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institutetext: Department of Physics, Kobe University,
Kobe 657-8501, Japan
institutetext: International Center for Quantum-field Measurement Systems for Studies of the Universe and Particles (QUP),
KEK, Tsukuba 305-0801, Japan
institutetext: Particle Theory and Cosmology Group, Center for Theoretical Physics of the Universe,
Institute for Basic Science (IBS), Daejeon, 34126, Korea

Stochastic tunneling in de Sitter spacetime

Taiga Miyachi ♮,†    Jiro Soda    and Junsei Tokuda [email protected] [email protected] [email protected]
Abstract

Tunneling processes in de Sitter spacetime are studied by using the stochastic approach. We evaluate the the Martin–Siggia–Rose–Janssen–de Dominicis (MSRJD) functional integral by using the saddle-point approximation to obtain the tunneling rate. The applicability conditions of this method are clarified using the Schwinger-Keldysh formalism. In the case of a shallow potential barrier, we reproduce the Hawking-Moss (HM) tunneling rate. Remarkably, in contrast to the HM picture, the configuration derived from the MSRJD functional integral satisfies physically natural boundary conditions. We also discuss the case of a steep potential barrier and find an interesting Coleman-de Luccia (CDL) bubble-like configuration. Since the starting point of our analysis is the Schwinger-Keldysh path integral, which can be formulated in a more generic setup and incorporates quantum effects, our formalism sheds light on further studies of tunneling phenomena from a real-time perspective.

KOBE-COSMO-23-09   CTPU-PTC-23-33

1 Introduction

Tunneling is an important non-perturbative phenomenon in cosmology. Hence, it is crucial to understand tunneling processes in curved spacetime. In particular, tunneling in de Sitter spacetime is worth studying in detail. The reason is that de Sitter spacetime is the simplest non-trivial curved spacetime. Moreover, the results obtained there can be applicable to tunneling phenomena during inflation. Since both Minkowski and de Sitter spacetime have the maximal symmetry, there exist a similarity. Indeed, the Euclidean instanton method for evaluating the tunneling rate in Minkowski spacetime Coleman:1977py ; Callan:1977pt is applicable to tunneling processes in de Sitter spacetime Coleman:1980aw . However, the extension of Euclidean method to de Sitter spacetime has a difficulty in interpretation. In the case of de Sitter spacetime, there are two saddle solutions: Coleman-De Luccia (CDL) Coleman:1980aw and Hawking-Moss (HM) instantons Hawking:1981fz . The latter instanton is a homogeneous solution. Therefore, it is not straightforward to interpret the tunneling rate as that for the tunneling process from a false vacuum to a true vacuum Rubakov:1999ir ; Brown:2007sd .

To circumvent the difficulty, a real time formalism might be useful. In the case of de Sitter spacetime in the flat chart, the stochastic formalism has been used for investigating time evolution of fluctuations during inflation Starobinsky:1986fx ; Starobinsky:1994bd . In this formalism, Langevin equations describe the dynamics of long wavelength modes. Stochastic noises stem from short wavelength quantum modes. The stochastic formalism has been also used to analyze the tunneling processes in de Sitter spacetime Goncharov:1987ir ; Linde:1991sk ; Tolley:2008qv ; Noorbala:2018zlv ; Hashiba:2020rsi ; Camargo-Molina:2022ord ; Camargo-Molina:2022paw . However, most of the previous works treated only the HM transition by utilizing the Fokker-Plank (FP) equation for a homogeneous scalar field, which can be derived from the Langevin equation. Obviously, the HM transition cannot describe the bubble nucleation in contrast to CDL tunneling. To describe the bubble, we have to include the spatial gradient term and the FP equation becomes the functional differential equation instead of the partial differential equation. Hence, at first glance, it seems difficult to treat the CDL bubble by the stochastic approach. However, we make an observation that there exists a path integral representation to solutions of the FP equation. In condensed matter physics, it is called Martin–Siggia–Rose–Janssen–de Dominicis (MSRJD) functional integral Martin:1973zz ; DeDominicis:1975gjb ; Janssen:1976aa ; DeDominicis:1977fw .

Refer to caption
Figure 1: The schematic picture of the potential V(ϕ)V(\phi) which has a false vacuum at ϕ=ϕfalse\phi=\phi_{\text{false}}, true vacuum at ϕ=ϕtrue\phi=\phi_{\text{true}} and the top of the potential at ϕ=ϕtop\phi=\phi_{\text{top}}.

In this paper, we use the MSRJD path integral formula to study the tunneling processes on the fixed de Sitter background. The applicability conditions of this method are clarified based on the Schwinger-Keldysh formalism. We consider a potential V(ϕ)V(\phi) which has a local minimum at ϕ=ϕfalse\phi=\phi_{\text{false}}, a true minimum at ϕtrue\phi_{\text{true}}, and a local maximum at ϕtop\phi_{\text{top}} as shown in FIG. 1. We use the saddle point method and evaluate the tunneling rate by computing the action for the tunneling configurations PhysRevE.70.041106 . We investigate both HM and CDL tunneling processes. In the case of a shallow potential barrier, the conventional HM tunneling rate is reproduced. Remarkably, the tunneling configuration in the MSRJD functional integral method has physically natural boundary conditions in contrast to the Euclidean method. We then clarify that the HM tunneling rate is the tunneling rate of a (roughly Hubble-sized) coarse-grained patch transitioning from ϕfalse\phi_{\text{false}} to ϕtop\phi_{\text{top}}. In the case of a steep potential barrier, we find an interesting CDL bubble-like configuration which is obtained by solving the solution of a scalar field equation in Euclidean anti-de Sitter space even though we do not work in the imaginary time. Our results show how the bubble nucleation process could be described in the stochastic approach.

This paper is organized as follows. In sec. 2, we present the setup and review the stochastic approach. In sec. 3, the MSRJD functional integral is constructed from the Langevin equations. We also outline the derivation of MSRJD functional integral starting from the Schwinger-Keldysh formalism. In sec. 4, we apply the MSRJD functional integral to the case of the shallow potential barrier and study the HM tunneling process. In sec. 5, we consider the case of the steep potential barrier and find the CDL bubble-like configuration. We derive the tunneling rate using the configuration and compare it with the one obtained in sec. 4. We also compare our results with those in the Euclidean method. Sec. 6 is devoted to the conclusion. Some technical details are presented in appendices.

2 Stochastic approach

In this section, we review the stochastic approach Starobinsky:1986fx ; Starobinsky:1994bd .

2.1 Setup

We consider a real scalar field ϕ\phi in (3+1) dimensional de Sitter background. The background geometry is described by the metric

ds2=dt2+a(t)2d𝒙2=a(η2)(dη2+d𝒙2),\displaystyle\mathrm{d}s^{2}=-\mathrm{d}t^{2}+a(t)^{2}\mathrm{d}\bm{x}^{2}=a(\eta^{2})(-\mathrm{d}\eta^{2}+\mathrm{d}\bm{x}^{2}), (1)

with the scale factor

a(t)=eHt=1Hη,a(t)=e^{Ht}=-\frac{1}{H\eta}, (2)

where HH is the Hubble constant. The action is given by

S=dtd3xa3[12ϕ˙212a2(ϕ)2V(ϕ)],S=\int\mathrm{d}t\mathrm{d}^{3}x\,a^{3}\bigg{[}\frac{1}{2}\dot{\phi}^{2}-\frac{1}{2}a^{-2}(\nabla\phi)^{2}-V(\phi)\bigg{]}, (3)

where a dot denotes a derivative respect to tt and V(ϕ)V(\phi) is a potential function. From this action, the canonical conjugate momentum Π\Pi is defined as Π:=a3ϕ˙\Pi:=a^{3}\dot{\phi} and the Hamilton’s equations of motion are given by

ϕ˙=a3Π,Π˙=a2ϕa3V(ϕ).\dot{\phi}=a^{-3}\Pi\ ,\qquad\dot{\Pi}=a\nabla^{2}\phi-a^{3}V^{\prime}(\phi)\,. (4)

2.2 Langevin equation

First, we divide the quantum fields ϕ\phi and Π\Pi into an infrared (IR) part and an ultraviolet (UV) part respectively as

ϕ=ϕIR+ϕUV,Π=ΠIR+ΠUV.\phi=\phi_{\text{IR}}+\phi_{\text{UV}}\ ,\qquad\Pi=\Pi_{\text{IR}}+\Pi_{\text{UV}}\ . (5)

The UV part is defined as

ϕUV\displaystyle\phi_{\text{UV}} :=d3k(2π)3θ(kkc(t))[a𝒌u𝒌(t)ei𝒌𝒙+a𝒌u𝒌(t)ei𝒌𝒙],\displaystyle:=\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\theta(k-k_{c}(t))\bigg{[}a_{\bm{k}}u_{\bm{k}}(t)e^{i\bm{k}\cdot\bm{x}}+a_{\bm{k}}^{\dagger}u_{\bm{k}}^{*}(t)e^{-i\bm{k}\cdot\bm{x}}\bigg{]},
ΠUV\displaystyle\Pi_{\text{UV}} :=d3k(2π)3θ(kkc(t))a(t)3[a𝒌u˙𝒌(t)ei𝒌𝒙+a𝒌u˙𝒌(t)ei𝒌𝒙],\displaystyle:=\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\theta(k-k_{c}(t))a(t)^{3}\,\bigg{[}a_{\bm{k}}\dot{u}_{\bm{k}}(t)e^{i\bm{k}\cdot\bm{x}}+a_{\bm{k}}^{\dagger}\dot{u}_{\bm{k}}^{*}(t)e^{-i\bm{k}\cdot\bm{x}}\bigg{]}, (6)

where u𝒌u_{\bm{k}} is a mode function that will be specified later, and a𝒌a_{\bm{k}} and a𝒌a^{\dagger}_{\bm{k}} are annihilation and creation operators, respectively. Here, θ(kkc(t))\theta(k-k_{c}(t)) is a step function and kc(t)k_{c}(t) is the cutoff scale defined as

kc(t):=εa(t)H,k_{c}(t):=\varepsilon a(t)H, (7)

where ε\varepsilon is a constant. The value of ε\varepsilon will be discussed later. Substituting Eqs.(6) into Hamilton’s equations (4), we obtain the following equations;

ϕ˙IR=a3ΠIR+ξϕ,Π˙IR=a2ϕIRa3V(ϕIR)+ξΠ,\dot{\phi}_{\text{IR}}=a^{-3}\Pi_{\text{IR}}+\xi^{\phi}\ ,\qquad\dot{\Pi}_{\text{IR}}=a\nabla^{2}\phi_{\text{IR}}-a^{3}V^{\prime}(\phi_{\text{IR}})+\xi^{\Pi}\ , (8)

where ξϕ\xi^{\phi} and ξΠ\xi^{\Pi} are defined as

ξϕ\displaystyle\xi^{\phi} :=k˙c(t)d3k(2π)3δ(kkc(t))[a𝒌u𝒌(t)ei𝒌𝒙+a𝒌u𝒌(t)ei𝒌𝒙],\displaystyle:=\dot{k}_{c}(t)\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\delta(k-k_{c}(t))\bigg{[}a_{\bm{k}}u_{\bm{k}}(t)e^{i\bm{k}\cdot\bm{x}}+a_{\bm{k}}^{\dagger}u_{\bm{k}}^{*}(t)e^{-i\bm{k}\cdot\bm{x}}\bigg{]},
ξΠ\displaystyle\xi^{\Pi} :=k˙c(t)d3k(2π)3δ(kkc(t))[a𝒌a(t)3u˙𝒌(t)ei𝒌𝒙+a𝒌a(t)3u˙𝒌(t)ei𝒌𝒙].\displaystyle:=\dot{k}_{c}(t)\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\delta(k-k_{c}(t))\bigg{[}a_{\bm{k}}a(t)^{3}\dot{u}_{\bm{k}}(t)e^{i\bm{k}\cdot\bm{x}}+a_{\bm{k}}^{\dagger}a(t)^{3}\dot{u}_{\bm{k}}^{*}(t)e^{-i\bm{k}\cdot\bm{x}}\bigg{]}. (9)

To derive Eqs.(8) and (9), we assumed that the time evolution of UV modes can be well approximated by the free theory that is defined around the false vacuum. The mode function u𝒌(t)u_{\bm{k}}(t) introduced in (9) then satisfies the following equation

u¨𝒌+3Hu˙𝒌+a2k2u𝒌+V′′(ϕfalse)u𝒌=0.\displaystyle\ddot{u}_{\bm{k}}+3H\dot{u}_{\bm{k}}+a^{-2}k^{2}u_{\bm{k}}+V^{\prime\prime}(\phi_{\text{false}})u_{\bm{k}}=0. (10)

From this equation, we see the mode function only depends on k:=|𝒌|k:=|\bm{k}|. Hence, we simply denote the mode function as uku_{k}. Note that this mode function is used for UV modes k>kc(t)k>k_{c}(t).

Let us consider statistical properties of ξϕ\xi^{\phi} and ξΠ\xi^{\Pi}. The annihilation and creation operators a𝒌a_{\bm{k}} and a𝒌a^{\dagger}_{\bm{k}} satisfy following commutation relations:

[a𝒌,a𝒌]=(2π)3δ(3)(𝒌𝒌),[a𝒌,a𝒌]=[a𝒌,a𝒌]=0.\displaystyle[a_{\bm{k}},a^{\dagger}_{\bm{k}^{\prime}}]=(2\pi)^{3}\delta^{(3)}(\bm{k}-\bm{k}^{\prime})\ ,\qquad[a_{\bm{k}},a_{\bm{k}^{\prime}}]=[a^{\dagger}_{\bm{k}},a^{\dagger}_{\bm{k}^{\prime}}]=0. (11)

Defining the vacuum state |0\ket{0} as

a𝒌|0=0,𝒌,\displaystyle a_{\bm{k}}\ket{0}=0,\quad\forall\bm{k}, (12)

we can calculate the one point and two point correlation functions of ξϕ\xi^{\phi} and ξΠ\xi^{\Pi} as

0|ξα(t,𝒙)|0=0,(α,β=ϕ,Π),\displaystyle\braket{0}{\xi^{\alpha}(t,\bm{x})}{0}=0,\quad(\alpha,\beta=\phi,\Pi),
0|ξα(t,𝒙)ξβ(t,𝒙)|0=12π2k˙c(t)kc(t)2sin(kc(t)r)kc(t)rgαβ(t)δ(tt),\displaystyle\braket{0}{\xi^{\alpha}(t,\bm{x})\xi^{\beta}(t^{\prime},\bm{x}^{\prime})}{0}=\frac{1}{2\pi^{2}}\dot{k}_{c}(t)k_{c}(t)^{2}\,\frac{\sin(k_{c}(t)r)}{k_{c}(t)r}g^{\alpha\beta}(t)\delta(t-t^{\prime}), (13)

where r:=|𝒙𝒙|r:=|\bm{x}-\bm{x}^{\prime}| and

{gϕϕ(t):=|ukc(t)|2gΠΠ(t):=a(t)6|u˙kc(t)|2gϕΠ(t)=(gΠϕ):=a(t)3ukc(t)u˙kc(t)..\displaystyle\begin{cases}g^{\phi\phi}(t)&:=|u_{k_{c}}(t)|^{2}\\ g^{\Pi\Pi}(t)&:=a(t)^{6}|\dot{u}_{k_{c}}(t)|^{2}\\ g^{\phi\Pi}(t)&=(g^{\Pi\phi})^{*}:=a(t)^{3}u_{k_{c}}(t)\dot{u}_{k_{c}}^{*}(t).\end{cases}. (14)

Because of the Wick theorem, all higher correlation functions can be decomposed into two point functions. In the stochastic approach, we replace the operator ξα\xi^{\alpha} by the real random field which has the following statistical properties

ξα(t,𝒙)ξ=0,(α,β=ϕ,Π),\displaystyle\braket{\xi^{\alpha}(t,\bm{x})}_{\xi}=0,\quad(\alpha,\beta=\phi,\Pi),
ξα(t,𝒙)ξβ(t,𝒙)ξ=12π2k˙c(t)kc(t)2sin(kc(t)r)kc(t)rRe[gαβ(t)]δ(tt),\displaystyle\braket{\xi^{\alpha}(t,\bm{x})\xi^{\beta}(t^{\prime},\bm{x}^{\prime})}_{\xi}=\frac{1}{2\pi^{2}}\dot{k}_{c}(t)k_{c}(t)^{2}\,\frac{\sin(k_{c}(t)r)}{k_{c}(t)r}\text{Re}[g^{\alpha\beta}(t)]\delta(t-t^{\prime}), (15)

where ξ\braket{\cdots}_{\xi} represents an expectation value with the distribution function of ξα\xi^{\alpha}. With this prescription, Eqs.(8) can be interpreted as the Langevin equations with the noise ξα\xi^{\alpha} stemming from quantum fluctuations. Since ξα\xi^{\alpha} are now regarded as classical variables, we ignored the imaginary parts of gϕΠg^{\phi\Pi} and gΠϕg^{\Pi\phi} which come from non-commutativity. Accordingly, IR variables ϕIR\phi_{\text{IR}} and ΠIR\Pi_{\text{IR}} are also regarded as classical stochastic variables in this prescription. The validity of this classical approximation will be discussed in the next section.

2.3 Bunch-Davies vacuum

Now we define the vacuum state |0\ket{0} by specifying the mode function uku_{k}. Eq.(10) is the equation for the mode k>kck>k_{c}. Let us assume that we can ignore the term V′′V^{\prime\prime} in solving (10). This can be justified when |V′′||V^{\prime\prime}| is sufficiently small to satisfy max[(kc/a)2,H2]|V′′|\max\left[(k_{c}/a)^{2},H^{2}\right]\gg|V^{\prime\prime}|. Under this approximation, (10) can be solved as

uk=(kη)32[C1H32(1)(kη)+C2H32(2)(kη)],\displaystyle u_{k}=(-k\eta)^{\frac{3}{2}}\bigg{[}C_{1}H^{(1)}_{\frac{3}{2}}(-k\eta)+C_{2}H^{(2)}_{\frac{3}{2}}(-k\eta)\bigg{]}, (16)

where C1,C2C_{1},C_{2} are constants of integration and Hν(1)(z),Hν(2)(z)H^{(1)}_{\nu}(z),H^{(2)}_{\nu}(z) are Hankel functions. We choose the Bunch-Davies vacuum, i.e., the vacuum coincides with Minkowski vacuum at past infinity (η\eta\to-\infty) so that

ukHη2keikη,(kη).\displaystyle u_{k}\to\frac{-H\eta}{\sqrt{2k}}e^{-ik\eta},\quad(-k\eta\to\infty). (17)

This determines C1,C2C_{1},C_{2} as

C1=π4kHk,C2=0.\displaystyle C_{1}=-\sqrt{\frac{\pi}{4k}}\frac{H}{k}\ ,\qquad C_{2}=0\ . (18)

Thus, we obtain the mode function

uk=Hη2k(1ikη1)eikη.\displaystyle u_{k}=\frac{H\eta}{\sqrt{2k}}\bigg{(}\frac{1}{-ik\eta}-1\bigg{)}e^{-ik\eta}. (19)

To check (17), we used the following formulae

H32(1)(z)=2πz(1iz1)eiz,H32(2)(z)=2πz(1iz1)eiz.\displaystyle H^{(1)}_{\frac{3}{2}}(z)=\sqrt{\frac{2}{\pi z}}\bigg{(}\frac{1}{iz}-1\bigg{)}e^{iz}\ ,\qquad H^{(2)}_{\frac{3}{2}}(z)=\sqrt{\frac{2}{\pi z}}\bigg{(}\frac{1}{-iz}-1\bigg{)}e^{-iz}. (20)

Substituting (19) into (14) and using (7), we obtain

{gϕϕ=H2η22kc(1kc2η2+1)=12Ha3(ε3+ε1)gΠΠ=kc2H2η2=Ha32εgϕΠ=gΠϕ=12(1kcη+i)=12ε1+i2.\displaystyle\begin{cases}g^{\phi\phi}&=\frac{H^{2}\eta^{2}}{2k_{c}}\bigg{(}\frac{1}{k_{c}^{2}\eta^{2}}+1\bigg{)}=\frac{1}{2Ha^{3}}\bigg{(}\varepsilon^{-3}+\varepsilon^{-1}\bigg{)}\\ g^{\Pi\Pi}&=\frac{k_{c}}{2H^{2}\eta^{2}}=\frac{Ha^{3}}{2}\varepsilon\\ g^{\phi\Pi}&=g^{\Pi\phi*}=\frac{1}{2}\bigg{(}\frac{1}{k_{c}\eta}+i\bigg{)}=-\frac{1}{2}\varepsilon^{-1}+\frac{i}{2}\end{cases}. (21)

From (8), we have to scale gαβg^{\alpha\beta} like as gϕϕgϕϕg^{\phi\phi}\to g^{\phi\phi}, gΠΠgΠΠ/(H2a6)g^{\Pi\Pi}\to g^{\Pi\Pi}/(H^{2}a^{6}) and gϕΠgϕΠ/(Ha3)g^{\phi\Pi}\to g^{\phi\Pi}/(Ha^{3}) in order to compare these quantities. Then, gϕϕg^{\phi\phi} and gΠΠg^{\Pi\Pi} become dominant for the case ε1\varepsilon\ll 1 and ε1\varepsilon\gg 1, respectively.

2.4 Reduced Langevin equation

Let us focus on physics at the super-horizon scales by taking ε1\varepsilon\ll 1 and assume a shallow potential so that we can use the massless approximation to evaluate the noise correlations. In this setup, we can use (21) from which we find that gϕϕg^{\phi\phi} becomes dominant. We then ignore the noise for momentum ξΠ\xi^{\Pi}. We also ignore the gradient term in (8) because we focus on the physics at super-horizon scales. Since the potential is assumed to be shallow, the time variation of ϕIR(t)\phi_{\text{IR}}(t) will be then very small. Therefore, we may integrate the second equation of (8) as

ΠIRa33HV(ϕIR).\displaystyle\Pi_{\text{IR}}\simeq-\frac{a^{3}}{3H}V^{\prime}(\phi_{\text{IR}}). (22)

Substituting this relation into the first equation of (8), we obtain

ϕ˙IR=V(ϕIR)3H+ξϕ,\displaystyle\dot{\phi}_{\text{IR}}=-\frac{V^{\prime}(\phi_{\text{IR}})}{3H}+\xi^{\phi}, (23)

where the two point correlation function of ξϕ\xi^{\phi} is given at the leading order by

ξϕ(t,𝒙)ξϕ(t,𝒙)ξ=H34π2j0(kcr)δ(tt),j0(kcr):=sin(kcr)kcr.\displaystyle\braket{\xi^{\phi}(t,\bm{x})\xi^{\phi}(t^{\prime},\bm{x}^{\prime})}_{\xi}=\frac{H^{3}}{4\pi^{2}}j_{0}(k_{c}r)\delta(t-t^{\prime})\,,\quad j_{0}(k_{c}r):=\frac{\sin(k_{c}r)}{k_{c}r}\,. (24)

Eq.(23) is the Langevin equation with the noise correlation (24) derived in Starobinsky:1994bd .

3 Path integral formalism for the stochastic approach

In this section, we introduce path integral approach for the Langevin equation following altland_simons_2010 . From now on, we replace the IR field and its conjugate momentum as (ϕIR,ΠIR)(ϕc,Πc)(\phi_{\text{IR}},\Pi_{\text{IR}})\to(\phi_{c},\Pi_{c}). As we see in section 3.2, this notation corresponds to the Keldysh basis. In section 3.2, we provide a first-principle derivation of the stochastic approach based on the Schwinger-Keldysh formalism following Tokuda:2017fdh ; Tokuda:2018eqs .111For earlier discussions of stochastic approach based on the Schwinger-Keldysh formalism, see e.g., Morikawa:1989xz ; Tolley:2008qv . We briefly show the sketch of the derivation in the main text, and details of derivations are given in appendix A.

3.1 MSRJD functional integral representation

3.1.1 0+1 dimensional theories

Eq.(23) can be regarded as the equation determining the position of a particle ϕ(t)\phi(t) with the white noise ξϕ\xi^{\phi} defined by Eq.(24). For kcr1k_{c}r\ll 1, we have sin(kcr)/(kcr)1\sin(k_{c}r)/(k_{c}r)\simeq 1 in a good approximation. Let us discretize the field and noise as ϕc(t)ϕi,ξϕ(t)ξiϕ,(i𝐙)\phi_{c}(t)\to\phi_{i},\,\xi^{\phi}(t)\to\xi^{\phi}_{i},\,(i\in\mathbf{Z}). Then, Eq.(23) reads

Xi:=ϕiϕi1+Δt(V(ϕi)3Hξiϕ)=0,\displaystyle X_{i}:=\phi_{i}-\phi_{i-1}+\Delta t\bigg{(}\frac{V^{\prime}(\phi_{i})}{3H}-\xi^{\phi}_{i}\bigg{)}=0, (25)

where Δt\Delta t is the temporal discretization interval. Note that the discretization (25) is called Ito discretization.222Generally, we can choose other discretization like as Stratonovich discretization. This ambiguity does not affect the result since the amplitudes of the noise do not depend on fields within the range of our approximation. Denoting a solution of (23) by ϕc[ξ]\phi_{c}[\xi], the expectation value of an observable 𝒪ξ\braket{\mathcal{O}}_{\xi} can be formally expressed as

𝒪[ϕc(t)]ξ=𝒟ϕc𝒪[ϕc]δ(ϕcϕc[ξ])ξ=𝒟ϕc𝒪[ϕc]missing|δXδϕcmissing|δ(X)ξ.\displaystyle\braket{\mathcal{O}[\phi_{c}(t)]}_{\xi}=\int\mathcal{D}\phi_{c}\,\mathcal{O}[\phi_{c}]\braket{\delta(\phi_{c}-\phi_{c}[\xi])}_{\xi}=\int\mathcal{D}\phi_{c}\,\mathcal{O}[\phi_{c}]\Braket{\bigg{missing}}{\frac{\delta X}{\delta\phi_{c}}\bigg{missing}}{\,\delta(X)}_{\xi}. (26)

where 𝒟ϕc:=idϕi\mathcal{D}\phi_{c}:=\prod_{i}d\phi_{i} is the functional measure, δ(ϕcϕc[ξ]):=iδ(ϕiϕi[ξ])\delta(\phi_{c}-\phi_{c}[\xi]):=\prod_{i}\delta(\phi_{i}-\phi_{i}[\xi]), and |δX/δϕc||\delta X/\delta\phi_{c}| is the determinant of {δXi/δϕj}\{\delta X_{i}/\delta\phi_{j}\}. When we choose the above discretization (25), δX/δϕc\delta X/\delta\phi_{c} becomes triangular matrix with a unit in the diagonal components, i.e., the functional determinant is unity. Thus, substituting (25) into (26), we obtain

𝒪[ϕc(t)]ξ=𝒟ϕc𝒪[ϕc]iδ(ϕiϕi1+Δt(V(ϕi)3Hξiϕ))ξ.\displaystyle\braket{\mathcal{O}[\phi_{c}(t)]}_{\xi}=\int\mathcal{D}\phi_{c}\,\mathcal{O}[\phi_{c}]\Braket{\prod_{i}\delta\bigg{(}\phi_{i}-\phi_{i-1}+\Delta t\bigg{(}\frac{V^{\prime}(\phi_{i})}{3H}-\xi^{\phi}_{i}\bigg{)}\bigg{)}}_{\xi}. (27)

Representing the delta functions in terms of a Fourier integral and taking the continuum limit, we obtain the following path integral representation

𝒪[ϕc(t)]ξ=𝒟(ϕc,ϕ~)𝒪[ϕc]exp[idtϕ~(ϕ˙c+V(ϕc)3Hξϕ)]ξ.\displaystyle\braket{\mathcal{O}[\phi_{c}(t)]}_{\xi}=\int\mathcal{D}(\phi_{c},\tilde{\phi})\,\mathcal{O}[\phi_{c}]\Braket{\exp\bigg{[}i\int\mathrm{d}t\tilde{\phi}\bigg{(}\dot{\phi}_{c}+\frac{V^{\prime}(\phi_{c})}{3H}-\xi^{\phi}\bigg{)}\bigg{]}}_{\xi}. (28)

After averaging over the noise assuming Gaussian statistics, we obtain the Martin–Siggia–Rose –Janssen–de Dominicis (MSRJD) functional integral

𝒪[ϕc(t)]ξ=𝒟(ϕc,ϕ~)𝒪[ϕc]exp[dt(iϕ~(ϕ˙c+V(ϕc)3H)H38π2ϕ~2)].\displaystyle\braket{\mathcal{O}[\phi_{c}(t)]}_{\xi}=\int\mathcal{D}(\phi_{c},\tilde{\phi})\,\mathcal{O}[\phi_{c}]\exp\bigg{[}\int\mathrm{d}t\bigg{(}i\tilde{\phi}\bigg{(}\dot{\phi}_{c}+\frac{V^{\prime}(\phi_{c})}{3H}\bigg{)}-\frac{H^{3}}{8\pi^{2}}\tilde{\phi}^{2}\bigg{)}\bigg{]}. (29)

Putting 𝒪[ϕc]=δ(ϕcϕc(t))\mathcal{O}[\phi_{c}]=\delta(\phi_{c}-\phi_{c}(t)) and taking the boundary conditions ϕc(t)=ϕc\phi_{c}(t^{\prime})=\phi_{c}^{\prime} and ϕc(t)=ϕc\phi_{c}(t)=\phi_{c}, we obtain the transition probability p(ϕc,t|ϕc,t)p(\phi_{c},t|\phi_{c}^{\prime},t^{\prime})

p(ϕc,t|ϕc,t)=ϕc(t)=ϕcϕc(t)=ϕc𝒟(ϕc,ϕ~)exp[dt(iϕ~(ϕ˙c+V(ϕc)3H)H38π2ϕ~2)].\displaystyle p(\phi_{c},t|\phi_{c}^{\prime},t^{\prime})=\int_{\phi_{c}(t^{\prime})=\phi_{c}^{\prime}}^{\phi_{c}(t)=\phi_{c}}\mathcal{D}(\phi_{c},\tilde{\phi})\,\exp\bigg{[}\int\mathrm{d}t\bigg{(}i\tilde{\phi}\bigg{(}\dot{\phi}_{c}+\frac{V^{\prime}(\phi_{c})}{3H}\bigg{)}-\frac{H^{3}}{8\pi^{2}}\tilde{\phi}^{2}\bigg{)}\bigg{]}\,. (30)

Finally, introducing new variables ΠΔ:=iϕ~\Pi_{\Delta}:=i\tilde{\phi}, we obtain the ”phase space” path integral

p(ϕc,t|ϕc,t)=ϕc(t)=ϕcϕc(t)=ϕc𝒟(ϕc,ΠΔ)exp[dt(ΠΔϕ˙cH(ϕc,ΠΔ))],\displaystyle p(\phi_{c},t|\phi_{c}^{\prime},t^{\prime})=\int_{\phi_{c}(t^{\prime})=\phi_{c}^{\prime}}^{\phi_{c}(t)=\phi_{c}}\mathcal{D}(\phi_{c},\Pi_{\Delta})\,\exp\bigg{[}\int\mathrm{d}t(\Pi_{\Delta}\dot{\phi}_{c}-H(\phi_{c},\Pi_{\Delta}))\bigg{]}\ , (31)

where we defined the Hamiltonian as

H(ϕc,ΠΔ):=V(ϕc)3HΠΔH38π2ΠΔ2.\displaystyle H(\phi_{c},\Pi_{\Delta}):=-\frac{V^{\prime}(\phi_{c})}{3H}\Pi_{\Delta}-\frac{H^{3}}{8\pi^{2}}\Pi_{\Delta}^{2}\ . (32)

We emphasize that this is just a change of integration variable, not the Wick rotation. A set of saddle point equations is defined as the Hamilton’s equations for the Hamiltonian defined above.

3.1.2 3+1 dimensional theories

Let us consider the case of the full Langevin Eqs. (8), (13) and (21). When the space is discretized, (8) can be seen as the dynamics of many body particles. Thus, the procedure in the previous subsection can be utilized. Taking the continuum limit, we obtain the following expression which is analogous to (30),

p(ϕc(𝒙),t|ϕc(𝒙),t)\displaystyle p(\phi_{c}(\bm{x}),t|\phi_{c}^{\prime}(\bm{x}),t^{\prime}) =ϕc(t,𝒙)=ϕc(𝒙)ϕc(t,𝒙)=ϕc(𝒙)𝒟(ϕc,Πc,ϕΔ,ΠΔ)\displaystyle=\int_{\phi_{c}(t^{\prime},\bm{x})=\phi_{c}^{\prime}(\bm{x})}^{\phi_{c}(t,\bm{x})=\phi_{c}(\bm{x})}\mathcal{D}(\phi_{c},\Pi_{c},\phi_{\Delta},\Pi_{\Delta})
×exp[id4x(ΠΔϕ˙cϕΔΠ˙cH(ϕc,Πc,ϕΔ,ΠΔ))].\displaystyle\times\exp\bigg{[}i\int\mathrm{d}^{4}x\bigg{(}\Pi_{\Delta}\dot{\phi}_{c}-\phi_{\Delta}\dot{\Pi}_{c}-H(\phi_{c},\Pi_{c},\phi_{\Delta},\Pi_{\Delta})\bigg{)}\bigg{]}\ .\quad

We defined the Hamiltonian H(ϕc,Πc,ϕΔ,ΠΔ)H(\phi_{c},\Pi_{c},\phi_{\Delta},\Pi_{\Delta}) as

H(ϕc,Πc,ϕΔ,ΠΔ)=\displaystyle H(\phi_{c},\Pi_{c},\phi_{\Delta},\Pi_{\Delta})= ΠcΠΔa3(a2ϕca3V(ϕc))ϕΔ\displaystyle\frac{\Pi_{c}\Pi_{\Delta}}{a^{3}}-(a\nabla^{2}\phi_{c}-a^{3}V^{\prime}(\phi_{c}))\phi_{\Delta}
i2α,βd4xXα(x)Gαβ(x,x)Xβ(x),\displaystyle-\frac{i}{2}\sum_{\alpha,\beta}\int\mathrm{d}^{4}x^{\prime}X_{\alpha}(x)G^{\alpha\beta}(x,x^{\prime})X_{\beta}(x^{\prime})\,, (34)

where the Greek indices α,β=(ϕ,Π)\alpha,\beta=(\phi,\Pi) label the Δ\Delta fields as (Xϕ,XΠ)=(ΠΔ,ϕΔ)(X_{\phi},X_{\Pi})=(\Pi_{\Delta},-\phi_{\Delta}) and GαβG^{\alpha\beta} denotes the correlations of noises:

Gαβ(x,x):=ξα(x)ξβ(x)ξ,G^{\alpha\beta}(x,x^{\prime}):=\langle\xi^{\alpha}(x)\xi^{\beta}(x^{\prime})\rangle_{\xi}\,, (35)

where the RHS is given in (15). We use the formula (LABEL:eq:ConditionalFull) in sections 4.2 and 5. Note that we have not changed the integration variables as (ϕΔ,ΠΔ)(iϕΔ,iΠΔ)(\phi_{\Delta},\Pi_{\Delta})\to(-i\phi_{\Delta},-i\Pi_{\Delta}).

In sections 4 and 5, we take the initial state and the final state to be the false vacuum and the field configurations after tunneling (true vacuum or bubble), respectively.

3.2 Transition probability from the Schwinger-Keldysh formalism

In the above prescription, we treat IR fields (ϕIR,ΠIR)(\phi_{\text{IR}},\Pi_{\text{IR}}) as classical stochastic variables. To quantify the validity of this approximation, we derive the stochastic approach from the first principles based on the Schwinger-Keldysh formalism. Note that we recover the label “IR” for IR fields in this subsection following the notation adopted in appendix A.

Suppose that the system is in the false vacuum |Ψfalse\ket{\Psi_{\text{false}}} at the past infinity t=t=-\infty and it evolves into a certain quantum state |{ϕIR(T,𝒙)}𝒙𝒟|\{\phi^{\text{IR}}(T,\bm{x})\}_{\bm{x}\in\mathcal{D}}\rangle at the final time t=Tt=T, where |{ϕIR(T,𝒙)}𝒙𝒟|\{\phi^{\text{IR}}(T,\bm{x})\}_{\bm{x}\in\mathcal{D}}\rangle is an eigenstate of an IR field ϕ^IR(𝒙)\hat{\phi}^{\text{IR}}(\bm{x}) at spatial points 𝒙\bm{x} in the domain 𝒟\mathcal{D} with an eigenvalue ϕIR(T,𝒙)\phi^{\text{IR}}(T,\bm{x}). Here, ϕ^IR(𝒙)\hat{\phi}^{\text{IR}}(\bm{x}) is an IR field in the Schrödinger picture.333Precisely, ϕ^IR(𝒙)\hat{\phi}^{\text{IR}}(\bm{x}) is defined in terms of the the Schrödinger picture field ϕ^(𝒌)\hat{\phi}({\bm{k}}) in momentum space as ϕ^IR(𝒙):=d3k(2π)3ϕ^(𝒌)ei𝒌.𝒙θ(kc(t)k)\hat{\phi}^{\text{IR}}(\bm{x}):=\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\,\hat{\phi}({\bm{k}})\,e^{i\bm{k}.\bm{x}}\theta(k_{c}(t)-k). We suppressed the trivial time dependence stemming from the step function. The transition probability pp for this process is given by

p({ϕIR(T,𝒙)}𝒙𝒟)=|{ϕIR(T,𝒙)}𝒙𝒟|U^(t,)|Ψfalse|2,p(\{\phi^{\text{IR}}(T,\bm{x})\}_{\bm{x}\in\mathcal{D}})=\left|\langle\{\phi^{\text{IR}}(T,\bm{x})\}_{\bm{x}\in\mathcal{D}}|\hat{U}(t,-\infty)|\Psi_{\text{false}}\rangle\right|^{2}\,, (36)

where U^(t,t)\hat{U}(t,t^{\prime}) describes the unitary time evolution from tt^{\prime} to tt. The RHS is the Fourier component of the generating functional Z[JIR]Z[J^{\text{IR}}] for IR fields, and we have

p({ϕIR(T,𝒙)}𝒙𝒟)=𝒙𝒟dJIR(T,𝒙)Z[JIR(T)]eiJIR(T,𝒙)ϕIR(T,𝒙)|{JIR(T,𝒚)=0}𝒚𝒟,\displaystyle p(\{\phi^{\text{IR}}(T,\bm{x})\}_{\bm{x}\in\mathcal{D}})=\left.\prod_{\bm{x}\in\mathcal{D}}\int\mathrm{d}J^{\text{IR}}(T,\bm{x})Z[J^{\text{IR}}(T)]e^{-iJ^{\text{IR}}(T,\bm{x})\phi^{\text{IR}}(T,\bm{x})}\right|_{\{J^{\text{IR}}(T,\bm{y})=0\}_{\bm{y}\notin\mathcal{D}}}\,, (37)

where the generating functional Z[JIR(T)]Z[J^{\text{IR}}(T)] is defined by

Z[JIR(T)]:=Tr[U^(T,)|ΨfalseΨfalse|U^(T,)𝒙eiJIR(T,𝒙)ϕIR(T,𝒙)].\displaystyle Z[J^{\text{IR}}(T)]:=\text{Tr}\left[\hat{U}(T,-\infty)\ket{\Psi_{\text{false}}}\bra{\Psi_{\text{false}}}\hat{U}^{\dagger}(T,-\infty)\prod_{\bm{x}}e^{iJ^{\text{IR}}(T,\bm{x})\phi^{\text{IR}}(T,\bm{x})}\right]\,. (38)

We can evaluate Z[JIR(T)]Z[J^{\text{IR}}(T)] non-perturbatively in the IR sector based on the method developed in Tokuda:2017fdh ; Tokuda:2018eqs . Our strategy is that we integrate out UV sector k>kc(t)k>k_{c}(t) perturbatively in nonlinear couplings to obtain Z[JIR(T)]Z[J^{\text{IR}}(T)]. This is analogous to tracing out environmental degrees of freedom to evaluate the reduced density matrix for the system under considerations. Each step we take can be summarized as follows:

  1. 1.

    First, we derive a path integral representation of Z[JIR(T)]Z[J^{\text{IR}}(T)]. We then split the integration variables into UV fields and IR fields such that the integration contour of UV variables of ϕ\phi is closed: see discussions around Eq.(94) for more details.444There is a subtlety that modes satisfying kkc(T)k\geq k_{c}(T) are initially regarded as the “UV” degrees of freedom (DoF) while they become “IR” DoFs due to the accelerating expansion of the spacetime. However, by adopting this splitting procedure, we can use the Schwinger-Keldysh (or closed-time-path) formalism to evaluate the integration over UV variables first as usual.

  2. 2.

    We perform the integration over UV variables and evaluate an IR effective action, the so-called Feynman-Vernon influence functional Feynman:1963fq perturbatively.

  3. 3.

    We substitute the obtained expression of Z[JIR(T)]Z[J^{\text{IR}}(T)] into (37), giving rise to the path integral expression for the transition probability pp.

Technical details are shown in appendix A. At the step 2, we assumed that the quantum state for non-zero modes is given by the Bunch-Davies vacuum state for a free field defined around the false vacuum, and that the exact zero mode provides a non-fluctuating classical background field configuration ϕ=ϕfalse\phi=\phi_{\text{false}}.

In this way, we can obtain the path integral expression for the probability pp as

p({ϕIR(T,𝒙)}𝒙𝒟)=\displaystyle p(\{\phi^{\text{IR}}(T,\bm{x})\}_{\bm{x}\in\mathcal{D}})= 𝒟(ϕcIR,ϕΔIR,ΠcIR,ΠΔIR)ei𝒮δ[𝒞fin]δ[𝒞ini].\displaystyle\int\mathcal{D}(\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{c},\Pi^{\text{IR}}_{\Delta})\,\,e^{i\mathcal{S}}\,\delta\left[\mathcal{C}_{\text{fin}}\right]\delta\left[\mathcal{C}_{\text{ini}}\right]\,. (39)

Here, δ[𝒞fin]\delta\left[\mathcal{C}_{\text{fin}}\right] and δ[𝒞ini]\delta\left[\mathcal{C}_{\text{ini}}\right] fix the boundary conditions of path integral at the final time and the initial time, respectively:

δ[𝒞fin]:=𝒙𝒟δ(ϕcIR(T,𝒙)ϕIR(T,𝒙))𝒚δ(ϕΔIR(T,𝒚)),\displaystyle\delta\left[\mathcal{C}_{\text{fin}}\right]:=\prod_{\bm{x}\in\mathcal{D}}\delta(\phi^{\text{IR}}_{c}(T,\bm{x})-\phi^{\text{IR}}(T,\bm{x}))\prod_{\bm{y}}\delta(\phi^{\text{IR}}_{\Delta}(T,\bm{y}))\,, (40a)
δ[𝒞ini]:=𝒙δ(ϕcIR(,𝒙)ϕfalse)δ(ΠcIR(,𝒙))δ[𝒞detail],\displaystyle\delta\left[\mathcal{C}_{\text{ini}}\right]:=\prod_{\bm{x}}\delta\left(\phi^{\text{IR}}_{c}(-\infty,\bm{x})-\phi_{\text{false}}\right)\delta\left(\Pi^{\text{IR}}_{c}(-\infty,\bm{x})\right)\delta[\mathcal{C_{\text{detail}}}]\,, (40b)

where δ[𝒞detail]\delta[\mathcal{C}_{\text{detail}}] is not relevant for the main points here, and we define it in appendix A. A term 𝒮\mathcal{S} may be understood as an IR effective action,

𝒮:=d4x[ΠΔIRϕ˙cIRϕΔIRΠ˙cIRH(ϕcIR,ΠcIR,ϕΔIR,ΠΔIR)δH],\displaystyle\mathcal{S}:=\int\mathrm{d}^{4}x\,\left[\Pi^{\text{IR}}_{\Delta}\dot{\phi}^{\text{IR}}_{c}-\phi^{\text{IR}}_{\Delta}\dot{\Pi}^{\text{IR}}_{c}-H(\phi^{\text{IR}}_{c},\Pi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{\Delta})-\delta H\right]\,, (41a)
δH:=a3(t)[V(ϕcIR+(ϕΔIR/2))V(ϕcIR(ϕΔIR/2))V(ϕcIR)ϕΔIR]+δHhigher,\displaystyle\delta H:=a^{3}(t)\left[V(\phi^{\text{IR}}_{c}+(\phi^{\text{IR}}_{\Delta}/2))-V(\phi^{\text{IR}}_{c}-(\phi^{\text{IR}}_{\Delta}/2))-V^{\prime}(\phi^{\text{IR}}_{c})\phi^{\text{IR}}_{\Delta}\right]+\delta H_{\text{higher}}\,, (41b)

where HH is given in (34). δHhigher\delta H_{\text{higher}} denotes the higher-order terms in the coupling constant. Note that eq (39) allows us to understand the transition probability pp in terms of the stochastic dynamics: this point is discussed in appendix A.3.

Validity of Eq.(LABEL:eq:ConditionalFull).

Now we find that 𝒮\mathcal{S} coincides with the term in the exponent of (LABEL:eq:ConditionalFull) up to the term δH\delta H. Hence, (39) shows that the result (LABEL:eq:ConditionalFull) in the previous section can be justified from the first-principles when the term δH\delta H is negligible. Suppose that the potential V(ϕ)V(\phi) is sufficiently flat in the regime of our interest such that perturbation theory works when integrating out UV modes. In this case, we can systematically calculate δHhigher\delta H_{\text{higher}} perturbatively and we have δHhigher=0\delta H_{\text{higher}}=0 at the leading order. We set δHhigher=0\delta H_{\text{higher}}=0 in the present analysis. We should keep in mind however that the non-perturbative physics at UV scales k>kc(t)=εa(t)Hk>k_{c}(t)=\varepsilon a(t)H is lost by setting δHhigher=0\delta H_{\text{higher}}=0. From this viewpoint, we should choose ε\varepsilon as large as possible.

Even after setting δHhigher=0\delta H_{\text{higher}}=0, we have nonzero δH\delta H. In the classical approximation, we may regard the Δ\Delta-variables (ϕΔIR,ΠΔIR)(\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{\Delta}) as tiny quantities and keep only the terms which are linear in the Δ\Delta-variables in 𝒮\mathcal{S}, leading to δH0\delta H\simeq 0. In the case ε1\varepsilon\ll 1, this approximation would work thanks to the squeezing of quantum fluctuations at super-horizon scales. However, it is more subtle if we can set δH=0\delta H=0 in the case ε1\varepsilon\gtrsim 1. We will revisit this issue in section 5.

4 Hawking-Moss tunneling

In this section, we discuss the Hawking-Moss (HM) tunneling from the perspective of MSRJD functional integral. We calculate the tunneling rate defined by (31) and (LABEL:eq:ConditionalFull) in sections 4.1 and 4.2, respectively.

Refer to caption
Figure 2: The potential of (42) for various β\beta. From top to bottom, the curves correspond to β=0,0.25,0.5,0.75,1\beta=0,0.25,0.5,0.75,1.

Hereafter, for the numerical calculations, we consider the potential Weinberg:2012pjx in FIG. 2;

V(ϕ)=g24[(ϕ2α2)2+4β3(αϕ33α3ϕ2α4)],\displaystyle V(\phi)=\frac{g^{2}}{4}\bigg{[}(\phi^{2}-\alpha^{2})^{2}+\frac{4\beta}{3}(\alpha\phi^{3}-3\alpha^{3}\phi-2\alpha^{4})\bigg{]}, (42)

for which the derivative with respect to ϕ\phi is given by a simple form

V(ϕ)=g2(ϕα)(ϕ+α)(ϕ+αβ).\displaystyle V^{\prime}(\phi)=g^{2}(\phi-\alpha)(\phi+\alpha)(\phi+\alpha\beta)\,. (43)

For this potential, we have ϕfalse=α\phi_{\text{false}}=-\alpha, ϕtrue=α\phi_{\text{true}}=\alpha and ϕtop=βα\phi_{\text{top}}=-\beta\alpha. The dimensionless parameter β\beta must be 0<β<10<\beta<1, otherwise ϕ=α\phi=-\alpha is not a false vacuum. The potential at each point takes the following values:

V(α)=0,V(α)=4βg2α43,V(βα)=g2α412(1β)3(3+β).\displaystyle V(-\alpha)=0\,,\quad V(\alpha)=-\frac{4\beta g^{2}\alpha^{4}}{3}\,,\quad V(-\beta\alpha)=\frac{g^{2}\alpha^{4}}{12}(1-\beta)^{3}(3+\beta)\,. (44)

The height of potential barrier ΔV\Delta V between the false vacuum and the true vacuum is

ΔV:=V(βα)V(α)=g2α412(1β)3(3+β).\displaystyle\Delta V:=V(-\beta\alpha)-V(-\alpha)=\frac{g^{2}\alpha^{4}}{12}(1-\beta)^{3}(3+\beta)\,. (45)

The mass of fluctuations around a given point ϕ\phi is

V′′(ϕ)=α2g2[3(ϕ/α)2+2β(ϕ/α)1].\displaystyle V^{\prime\prime}(\phi)=\alpha^{2}g^{2}\left[3(\phi/\alpha)^{2}+2\beta(\phi/\alpha)-1\right]\,. (46)

In our analysis, we work in the quantum field theory on the fixed de Sitter background. This assumption will be valid when the condition max[|V(α)|,|V(βα)|,|V(α)|]3Mpl2H2\max\bigl{[}|V(-\alpha)|,|V(-\beta\alpha)|,|V(\alpha)|\bigr{]}\ll 3M_{\text{pl}}^{2}H^{2} is satisfied. This is always satisfied when the following condition is imposed,

H3gMpl2(Hgα)22.9×1012GeV(g1.12×104)(140gα/H)2,H\ll\frac{3gM_{\text{pl}}}{2}\left(\frac{H}{g\alpha}\right)^{2}\approx 2.9\times 10^{12}\,\text{GeV}\left(\frac{g}{1.12\times 10^{-4}}\right)\left(\frac{\sqrt{140}}{g\alpha/H}\right)^{2}\,, (47)

where we use 0<β<10<\beta<1 and choose parameters (g,gα/H)=(1.12×104,140)(g,g\alpha/H)=(1.12\times 10^{-4},\sqrt{140}) as a benchmark point for later convenience. This shows that we can ignore the backreaction consistently with the weak coupling g1g\ll 1 provided that HH is well below the Planck scale Mpl2.44×1018M_{\text{pl}}\approx 2.44\times 10^{18} GeV. Note that under this condition, our discussion below is also applicable in the case of a quasi de Sitter background. However, it is non-trivial to generalize our analysis to the case when a non-negligible backreaction on HH exists. This is because it is necessary to extend the first-principles derivation of the stochastic approach to account for the backreaction. This is in itself an interesting issue which we leave for future work.

4.1 The case for the reduced Langevin equation

Let us start from the simpler formula (31). The Hamilton’s equations for the Hamiltonian H(ϕc,ΠΔ)H(\phi_{c},\Pi_{\Delta}) defined in (32) are given as

ϕ˙c\displaystyle\dot{\phi}_{c} =V(ϕc)3HH34π2ΠΔ\displaystyle=-\frac{V^{\prime}(\phi_{c})}{3H}-\frac{H^{3}}{4\pi^{2}}\Pi_{\Delta}
Π˙Δ\displaystyle\dot{\Pi}_{\Delta} =V′′(ϕc)3HΠΔ.\displaystyle=\frac{V^{\prime\prime}(\phi_{c})}{3H}\Pi_{\Delta}. (48)

There exist many Hamiltonian flow lines in phase space (ϕc,ΠΔ)(\phi_{c},\Pi_{\Delta}) that represent the solution of Hamilton’s equations as shown in FIG.3. Each flow line can be specified by the value of Hamiltonian since it is conserved on the given flow line. In the FIG.3, there are two important flow lines corresponding to H(ϕc,ΠΔ)=0H(\phi_{c},\Pi_{\Delta})=0. Since the Hamiltonian is the quadratic polynomial of ΠΔ\Pi_{\Delta}, there are two ΠΔ\Pi_{\Delta} satisfying H(ϕc,ΠΔ)=0H(\phi_{c},\Pi_{\Delta})=0:

ΠΔ=0,8π23H4V.\displaystyle\Pi_{\Delta}=0,\,-\frac{8\pi^{2}}{3H^{4}}V^{\prime}\ . (49)

In the case of ΠΔ=0\Pi_{\Delta}=0, the equations (48) reduce to

ϕ˙c\displaystyle\dot{\phi}_{c} =V(ϕc)3H.\displaystyle=-\frac{V^{\prime}(\phi_{c})}{3H}\ . (50)

Similarly, in the case of ΠΔ=8π23H4V(ϕc)\Pi_{\Delta}=-\frac{8\pi^{2}}{3H^{4}}V^{\prime}(\phi_{c}), the equations (48) reduce to

ϕ˙c=V(ϕc)3H.\displaystyle\dot{\phi}_{c}=\frac{V^{\prime}(\phi_{c})}{3H}\ . (51)

These two flow lines have three intersections which correspond to the false vacuum, the top of potential hill and the true vacuum from left to right. On the flow line with ΠΔ=0\Pi_{\Delta}=0, the false and true vacuum are stable and the top of potential is unstable. While on the flow line with ΠΔ0\Pi_{\Delta}\neq 0, the stability is reversed. The different signs of the potential forces account for the reverse of the stability at the intersections. We see that the tunneling configuration exists; starting from the false vacuum (ϕc,ΠΔ)=(α,0)(\phi_{c},\Pi_{\Delta})=(-\alpha,0), going to the top of the potential (ϕc,ΠΔ)=(βα,0)(\phi_{c},\Pi_{\Delta})=(-\beta\alpha,0) through the flow line with ΠΔ0\Pi_{\Delta}\neq 0 and finally going to the true vacuum through the flow line with ΠΔ=0\Pi_{\Delta}=0.

Refer to caption
Figure 3: The Hamilton flow for (48) where we take α=H\alpha=H, g=0.4g=0.4 and β=0.1\beta=0.1. The solid lines correspond to H(ϕc,ΠΔ)=0H(\phi_{c},\Pi_{\Delta})=0. From left to right, the intersections of the solid lines correspond to the false vacuum, the top of potential hill and the true vacuum.

We numerically solve the second equation with the initial conditions ϕc(t)=α\phi_{c}(t^{\prime})=-\alpha and switch to the first equation when the field reaches the top of potential ϕc(t)=βα\phi_{c}(t)=-\beta\alpha. Thus, we obtain the tunneling configuration in FIG.4.

Refer to caption
Figure 4: The tunneling configuration for the homogeneous fields is plotted for β=0.1\beta=0.1 and αg/H=10\alpha g/H=\sqrt{10}. We choose the initial condition as ϕc(1015)/α=1+105\phi_{c}(10^{-15})/\alpha=-1+10^{-5} and solve the second equation of (50). When ϕc/α\phi_{c}/\alpha reached the top of potential ϕc/α=β\phi_{c}/\alpha=-\beta, we switch to the first equation of (50) with the initial condition ϕc/α=β+105\phi_{c}/\alpha=-\beta+10^{-5}.

Now, we evaluate the transition probability (31) by substituting the above tunneling configurations. The action in (31) can be calculated without the concrete solutions for ϕc\phi_{c};

I=ttdt[ΠΔϕ˙cH(ϕc,ΠΔ)]=8π23H4ttdtϕ˙cV(ϕc)=8π23H4ΔV,\displaystyle I=\int_{t^{\prime}}^{t}\mathrm{d}t\left[\Pi_{\Delta}\dot{\phi}_{c}-H(\phi_{c},\Pi_{\Delta})\right]=-\frac{8\pi^{2}}{3H^{4}}\int_{t^{\prime}}^{t_{*}}\mathrm{d}t\dot{\phi}_{c}V^{\prime}(\phi_{c})=-\frac{8\pi^{2}}{3H^{4}}\Delta V, (52)

where tt_{*} is the time that ϕc\phi_{c} reaches the top of potential and ΔV\Delta V is the difference of energy density between the top of the potential and the false vacuum. The trajectory from the top of the potential to the true vacuum does not contribute to the transition probability because H(ϕc,ΠΔ)=0H(\phi_{c},\Pi_{\Delta})=0 and ΠΔ=0\Pi_{\Delta}=0 on its trajectory. Thus, the transition probability of the tunneling can be evaluated as

p(α,t|α,t)exp(8π23H4ΔV).p(\alpha,t|-\alpha,t^{\prime})\sim\exp\bigg{(}-\frac{8\pi^{2}}{3H^{4}}\Delta V\bigg{)}. (53)

This shows a complete agreement with the result of the HM instanton on the fixed background Weinberg:2006pc .

Comments on this result are in order. It is pointed out in Weinberg:2006pc that when the potential V(ϕ)V(\phi) has several degenerate local maxima, all of them yield the same tunneling action in the Euclidean method, despite differing distances from the false vacuum. In our formalism, however, a transition to a distant maximum is described by a saddle-point solution that passes through all the intermediate maxima, and the transition probability is given by the product of the factors on the RHS of (53) for each maximum. The aforementioned subtlety is absent in our formalism.

Since the analysis in sec. 4.1 is based on (23) describing the stochastic dynamics of the IR field ϕc\phi_{c} at a single spatial point, eq. (53) calculates the tunneling probability at a single spatial point, not at the whole universe.555This is consistent with the observation made in Brown:2007sd that HM solution corresponds to the transition over a region of a Hubble horizon volume. Hence, physically speaking, (53) provides the tunneling probability of a coarse-grained patch with a physical radius (εH)1(\varepsilon H)^{-1}. This point becomes manifest also in sec. 4.2.

4.2 The case for the full Langevin equation

Next, we evaluate the tunneling rate based on the formula (LABEL:eq:ConditionalFull). An advantage of (LABEL:eq:ConditionalFull) is that one can discuss various non-trivial dynamics in the whole universe covered by the flat chart in principle.

In the previous section, we focused on the dynamics at a single spatial point and found the HM tunneling process as a non-trivial solution of the Hamilton’s equations. In this section, we discuss the corresponding process in the global picture based on (LABEL:eq:ConditionalFull) by identifying a non-trivial configuration that satisfies the Hamilton’s equations in a good approximation. We then reproduce the result (52). We also estimate the characteristic time scale of the tunneling. In sec. 4.2.1, we remark some technical complications that arise in the global picture.

We start with simplifying the expression (LABEL:eq:ConditionalFull). As discussed in section 2, GϕϕG^{\phi\phi} becomes dominant and the others can be neglected for ε1\varepsilon\ll 1 in (34). Under this approximation, the exponent of the integrand of (LABEL:eq:ConditionalFull) is linear in ϕΔ\phi_{\Delta}. We can then perform the path integral 𝒟ϕΔ\int\mathcal{D}\phi_{\Delta} in (LABEL:eq:ConditionalFull), yielding the product of delta functions 𝒙δ(Π˙ca2ϕc+a3V(ϕc))\prod_{\bm{x}}\delta\bigl{(}\dot{\Pi}_{c}-a\nabla^{2}\phi_{c}+a^{3}V^{\prime}(\phi_{c})\bigr{)}. These delta functions give an equation of motion for Πc\Pi_{c} and eliminate the path integral 𝒟Πc\int\mathcal{D}\Pi_{c}. We solve this equation as Πca3V(ϕc)/3H\Pi_{c}\simeq-a^{3}V^{\prime}(\phi_{c})/3H, ignoring the spatial gradient and the time variation of ϕc\phi_{c}. Furthermore, we change the integration variable as ΠΔiΠΔ\Pi_{\Delta}\to-i\Pi_{\Delta} in (LABEL:eq:ConditionalFull). Consequently, (LABEL:eq:ConditionalFull) reduces to

p(ϕc(𝒙),t|ϕc(𝒙),t)ϕc(t,𝒙)=ϕc(𝒙)ϕc(t,𝒙)=ϕc(𝒙)𝒟(ϕc,ΠΔ)exp[d4x(ΠΔϕ˙cHHM(ϕc,ΠΔ))],p(\phi_{c}(\bm{x}),t|\phi_{c}^{\prime}(\bm{x}),t^{\prime})\simeq\int_{\phi_{c}(t^{\prime},\bm{x})=\phi_{c}^{\prime}(\bm{x})}^{\phi_{c}(t,\bm{x})=\phi_{c}(\bm{x})}\mathcal{D}(\phi_{c},\Pi_{\Delta})\exp\left[\int\mathrm{d}^{4}x\left(\Pi_{\Delta}\dot{\phi}_{c}-H_{\text{HM}}(\phi_{c},\Pi_{\Delta})\right)\right]\,, (54)

where the Hamiltonian HHMH_{\text{HM}} is defined as

HHM(ϕc,ΠΔ)\displaystyle H_{\text{HM}}(\phi_{c},\Pi_{\Delta}) :=13HV(ϕc)ΠΔH38π2ΠΔΠ¯Δ,\displaystyle:=-\frac{1}{3H}V^{\prime}(\phi_{c})\Pi_{\Delta}-\frac{H^{3}}{8\pi^{2}}\Pi_{\Delta}\overline{\Pi}_{\Delta}\,, (55)

and Π¯Δ\overline{\Pi}_{\Delta} is given by

Π¯Δ(t,𝒙)\displaystyle\overline{\Pi}_{\Delta}(t,\bm{x}) :=d3xj0(kc(t)|𝒙𝒙|)ΠΔ(t,𝒙)=d3k(2π)34π2H3H22k3δ(ttk)ΠΔ(t,𝒌)ei𝒌𝒙.\displaystyle:=\int\mathrm{d}^{3}x^{\prime}\,j_{0}\left(k_{c}(t)|\bm{x}-\bm{x}^{\prime}|\right)\Pi_{\Delta}(t,\bm{x}^{\prime})=\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\,\frac{4\pi^{2}}{H^{3}}\frac{H^{2}}{2k^{3}}\delta(t-t_{k})\Pi_{\Delta}(t,\bm{k})e^{i\bm{k}\cdot\bm{x}}\,. (56)

Here we define tkt_{k} by the condition kc(tk)=kk_{c}(t_{k})=k. The Hamilton’s equations are

ϕ˙c=13HV(ϕc)H34π2Π¯Δ,\displaystyle\dot{\phi}_{c}=-\frac{1}{3H}V^{\prime}(\phi_{c})-\frac{H^{3}}{4\pi^{2}}\overline{\Pi}_{\Delta}\,, (57a)
Π˙Δ=13HV′′(ϕc)ΠΔ.\displaystyle\dot{\Pi}_{\Delta}=\frac{1}{3H}V^{\prime\prime}(\phi_{c})\Pi_{\Delta}\,. (57b)

Here, the term Π˙Δ(t,𝒙)\dot{\Pi}_{\Delta}(t,\bm{x}) on the LHS of (57b) is defined as the Fourier transform of Π˙Δ(t,𝒌)\dot{\Pi}_{\Delta}(t,\bm{k}) i.e., Π˙Δ(t,𝒙):=(2π)3d3kΠ˙Δ(t,𝒌)ei𝒌𝒙\dot{\Pi}_{\Delta}(t,\bm{x}):=(2\pi)^{-3}\int\mathrm{d}^{3}k\,\dot{\Pi}_{\Delta}(t,\bm{k})e^{i\bm{k}\cdot\bm{x}}. The same rule applies to other IR variables in the real space as in eq. (115). Intuitively, this is because the stochastic formalism is formulated in the momentum space and its Fourier transform provides the stochastic formalism in the real-space: see appendix A for more details.

Eqs. (57) admit a trivial configuration ΠΔ(t,𝒌)=0\Pi_{\Delta}(t,\bm{k})=0 under which we have HHM=0H_{\text{HM}}=0 and (57a) becomes ϕ˙c=V(ϕc)/(3H)\dot{\phi}_{c}=-V^{\prime}(\phi_{c})/(3H) describing the standard classical time evolution. Now we are interested in the non-trivial configuration which satisfies (57). In the previous section, we focus on the non-trivial dynamics at the single spatial point 𝒙=𝒙0\bm{x}=\bm{x}_{0} and it is found that the tunneling configuration is obtained by ΠΔ(t,𝒙0)=8π23H4V(ϕc(t,𝒙0))\Pi_{\Delta}(t,\bm{x}_{0})=-\frac{8\pi^{2}}{3H^{4}}V^{\prime}(\phi_{c}(t,\bm{x}_{0})). This configuration can be naturally extended to the one in the global picture by considering the following configuration

ΠΔ(t,𝒌)=8π23H4V(ϕc(t,𝒙0))ei𝒌𝒙0.\displaystyle\Pi_{\Delta}(t,\bm{k})=-\frac{8\pi^{2}}{3H^{4}}V^{\prime}(\phi_{c}(t,\bm{x}_{0}))e^{-i\bm{k}\cdot\bm{x}_{0}}\,. (58)

From now on, we show that this configuration satisfies a set of Hamilton equations (57) in a good approximation. For this configuration, we have

ΠΔ(t,𝒙)=8π23H4V(ϕc(t,𝒙0))f(r;t),\displaystyle\Pi_{\Delta}(t,\bm{x})=-\frac{8\pi^{2}}{3H^{4}}V^{\prime}(\phi_{c}(t,\bm{x}_{0}))f(r;t)\,,\quad (59a)
Π˙Δ(t,𝒙)=8π23H4V′′(ϕc(t,𝒙0))ϕ˙c(t,𝒙0)f(r;t),\displaystyle\dot{\Pi}_{\Delta}(t,\bm{x})=-\frac{8\pi^{2}}{3H^{4}}V^{\prime\prime}(\phi_{c}(t,\bm{x}_{0}))\dot{\phi}_{c}(t,\bm{x}_{0})f(r;t)\,, (59b)
Π¯Δ(t,𝒙)=8π23H4V(ϕc(t,𝒙0))j0(kc(t)r),\displaystyle\overline{\Pi}_{\Delta}(t,\bm{x})=-\frac{8\pi^{2}}{3H^{4}}V^{\prime}(\phi_{c}(t,\bm{x}_{0}))j_{0}\left(k_{c}(t)r\right)\,, (59c)

where r:=|𝒙𝒙0|r:=|\bm{x}-\bm{x}_{0}| and f(r;t):=(2π)3d3kθ(kc(t)k)ei𝒌(𝒙𝒙0)f(r;t):=(2\pi)^{-3}\int\mathrm{d}^{3}k\,\theta(k_{c}(t)-k)\,e^{i\bm{k}\cdot(\bm{x}-\bm{x}_{0})}. The functions j0(kc(t)r)j_{0}(k_{c}(t)r) and f(r;t)f(r;t) rapidly oscillate for rkc1(t)r\gg k_{c}^{-1}(t). Hence, they exponentially decay to zero after they are smeared over the Hubble time: for instance, j0j_{0} and ff becomes the smooth function after the suitable coarse-graining as 666 Note that this behavior may motivate one to replace the term j0(kc(t)r)j_{0}(k_{c}(t)r) in (55) by the step function j0(kc(t)r)θ(1kc(t)r).\displaystyle j_{0}(k_{c}(t)r)\rightarrow\theta(1-k_{c}(t)r)\,. (60) This is the approximation adopted in Starobinsky:1994bd .

j0(kc(t)r)\displaystyle j_{0}(k_{c}(t)r) time c.g.W(r;t):=dtw(t,t)j0(kc(t)r){1(rkc1(t))0(rkc1(t)),\displaystyle\xrightarrow{\text{time c.g.}}W(r;t):=\int\mathrm{d}t^{\prime}w(t^{\prime},t)j_{0}\left(k_{c}(t^{\prime})r\right)\approx\begin{cases}1&(r\ll k_{c}^{-1}(t))\\ 0\quad&(r\gg k_{c}^{-1}(t))\end{cases}\,,
f(r;t)\displaystyle f(r;t) time c.g.Wf(r;t):=dtw(t,t)f(r;t){kc3(t)/(6π2)(rkc1(t))0(rkc1(t)).\displaystyle\xrightarrow{\text{time c.g.}}W_{f}(r;t):=\int\mathrm{d}t^{\prime}\,w(t^{\prime},t)f(r;t^{\prime})\approx\begin{cases}k_{c}^{3}(t)/(6\pi^{2})&(r\ll k_{c}^{-1}(t))\\ 0\quad&(r\gg k_{c}^{-1}(t))\end{cases}\,. (61)

Here, we perform the smearing by using a window function w(t,t)w(t^{\prime},t) which is approximately constant in the domain |tt|H1|t-t^{\prime}|\ll H^{-1} while it exponentially decays to zero at |tt|H1|t-t^{\prime}|\gg H^{-1}. We also impose the normalization condition dtw(t,t)=1\int\mathrm{d}t^{\prime}w(t^{\prime},t)=1. We can choose w(t,t)=Hπ1/2exp[H2(tt)2]w(t^{\prime},t)=H\pi^{-1/2}\exp[-H^{2}(t-t^{\prime})^{2}] for example. Note that the property (61) is based on the behavior j0(kcr)1j_{0}(k_{c}r)\simeq 1 and f(r;t)kc3/(6π2)f(r;t)\simeq k_{c}^{3}/(6\pi^{2}) for rkc1r\ll k_{c}^{-1} and the rapid oscillations of j0(kcr)j_{0}(k_{c}r) and f0(r;t)f_{0}(r;t) for rkc1r\gg k_{c}^{-1}. Hence, the property (61) will be robust against the choice of w(t,t)w(t^{\prime},t).

Therefore, substituting Eqs. (59c) and (61) into Eq. (57a) and performing the smearing in time, we obtain

ϕ˙c(t,𝒙)=\displaystyle\dot{\phi}_{c}(t,\bm{x})= 13H[V(ϕc(t,𝒙))2V(ϕc(t,𝒙0))j0(kc(t)r)]\displaystyle-\frac{1}{3H}\left[V^{\prime}(\phi_{c}(t,\bm{x}))-2V^{\prime}(\phi_{c}(t,\bm{x}_{0}))j_{0}\left(k_{c}(t)r\right)\right] (62a)
time c.g.{V(ϕc(t,𝒙))/(3H)(rkc1(t))V(ϕc(t,𝒙0))/(3H)(rkc1(t)).\displaystyle\xrightarrow{\text{time c.g.}}\begin{cases}-V^{\prime}(\phi_{c}(t,\bm{x}))/(3H)&(r\gg k_{c}^{-1}(t))\\ V^{\prime}(\phi_{c}(t,\bm{x}_{0}))/(3H)&(r\ll k_{c}^{-1}(t))\end{cases}\,. (62b)

This exhibits the non-trivial dynamics only in the domain rkc1r\lesssim k_{c}^{-1}, i.e., a coarse-grained patch centered at a point 𝒙0\bm{x}_{0} with a physical radius (εH)1(\varepsilon H)^{-1}. Here, we used ϕc(t,𝒙)ϕc(t,𝒙0)\phi_{c}(t,\bm{x})\simeq\phi_{c}(t,\bm{x}_{0}) for rkc1(t)r\ll k_{c}^{-1}(t). In the second line, it is assumed that V(ϕc(t,𝒙0))V^{\prime}(\phi_{c}(t,\bm{x}_{0})) does not cancel the rapid oscillations of j0(kc(t)r)j_{0}(k_{c}(t)r) so that their product Vj0V^{\prime}j_{0} decays exponentially at rkc1r\gg k_{c}^{-1} after the suitable smearing. This assumption will be valid thanks to the approximate constancy of super-Horizon fluctuations ϕc(t,𝒌)\phi_{c}(t,\bm{k}) over the Hubble time: ϕc(t,𝒌)ϕc(t,𝒌)\phi_{c}(t,\bm{k})\simeq\phi_{c}(t^{\prime},\bm{k}) for |tt|H1|t-t^{\prime}|\lesssim H^{-1}. Adopting the same assumption, from (59a) and (59b) we also obtain the smeared expressions of ΠΔ\Pi_{\Delta} and Π˙Δ\dot{\Pi}_{\Delta} which turn out to satisfy (57b) under the condition (57a). Hence, we conclude that (59) describes a non-trivial saddle-point solution in a good approximation. Furthermore, after the smearing we can find HHM0H_{\text{HM}}\approx 0 for this configuration.

Now we use the configuration (58) or (59) to obtain the tunneling configuration shown in FIG.4 again. We can calculate the action for this tunneling configuration similarly to (52). By substituting the exact expressions (59) and (62a), we obtain 777Note that we can also estimate the action II by performing the coarse-graining in time suitably and substituting the smeared expression of ΠΔ\Pi_{\Delta} into the action: I\displaystyle I 8π23H4ttdtV(ϕc(t,𝒙0))d3xϕ˙c(t,𝒙)Wf(r;t)8π23H4ttdtϕ˙c(t,𝒙0)V(ϕc(t,𝒙0))=8π23H4ΔV,\displaystyle\simeq-\frac{8\pi^{2}}{3H^{4}}\int_{t^{\prime}}^{t_{*}}\mathrm{d}t\,V^{\prime}(\phi_{c}(t,\bm{x}_{0}))\int\mathrm{d}^{3}x\,\dot{\phi}_{c}(t,\bm{x})W_{f}(r;t)\simeq-\frac{8\pi^{2}}{3H^{4}}\int_{t^{\prime}}^{t_{*}}\mathrm{d}t\,\dot{\phi}_{c}(t,\bm{x}_{0})V^{\prime}(\phi_{c}(t,\bm{x}_{0}))=-\frac{8\pi^{2}}{3H^{4}}\Delta V\,, reproducing the previous result (52). In the first approximate equality, we used HHM=0H_{\text{HM}}=0 which is well satisfied after the smearing. In the second one, we use ϕc(t,𝒙)ϕc(t,𝒙0)\phi_{c}(t,\bm{x})\simeq\phi_{c}(t,\bm{x}_{0}) for rkc1(t)r\ll k_{c}^{-1}(t) and the condition d3xWf(r;t)=1\int\mathrm{d}^{3}x\,W_{f}(r;t)=1 which follows from the definition of WfW_{f}. This estimate may be more analogous to the calculation of the action in sec. 4.1 since the approximate locality of the dynamics is restored after the smearing.

I\displaystyle I =H38π2ttdtd3xΠΔ(t,𝒙)Π¯Δ(t,𝒙)\displaystyle=-\frac{H^{3}}{8\pi^{2}}\int_{t^{\prime}}^{t_{*}}\mathrm{d}t\,\int\mathrm{d}^{3}x\,\Pi_{\Delta}(t,\bm{x})\overline{\Pi}_{\Delta}(t,\bm{x})
=8π23H4ttdtV(ϕc(t,𝒙0))V(ϕc(t,𝒙0))3Hd3xj0(kc(t)r)f(r;t)\displaystyle=-\frac{8\pi^{2}}{3H^{4}}\int_{t^{\prime}}^{t_{*}}\mathrm{d}t\,V^{\prime}(\phi_{c}(t,\bm{x}_{0}))\frac{V^{\prime}(\phi_{c}(t,\bm{x}_{0}))}{3H}\int\mathrm{d}^{3}x\,j_{0}\left(k_{c}(t)r\right)f(r;t)
=8π23H4ttdtϕ˙c(t,𝒙0)V(ϕc(t,𝒙0))=8π23H4ΔV.\displaystyle=-\frac{8\pi^{2}}{3H^{4}}\int_{t^{\prime}}^{t_{*}}\mathrm{d}t\,\dot{\phi}_{c}(t,\bm{x}_{0})V^{\prime}(\phi_{c}(t,\bm{x}_{0}))=-\frac{8\pi^{2}}{3H^{4}}\Delta V\,. (63)

In the first line, we used (57a) to eliminate ϕ˙c\dot{\phi}_{c} from the integrand. In the second line, we substituted the concrete configurations (59). In the third line, we used (62a) and performed the spatial integral as d3xj0(kc(t)r)f(r;t)=1\int\mathrm{d}^{3}x\,j_{0}\left(k_{c}(t)r\right)f(r;t)=1. Thus, we reproduce the previous result (52). Our analysis confirms that (63) gives the tunneling probability of a coarse-grained patch with a physical radius (εH)1(\varepsilon H)^{-1}.

It is worth mentioning the time scale of the HM tunneling. We may naively calculate the typical time scale of the HM tunneling as tt=ϕfalseϕtopdϕc3HV(ϕc)t_{*}-t^{\prime}=\int^{\phi_{\text{top}}}_{\phi_{\text{false}}}\mathrm{d}\phi_{c}\,\frac{3H}{V^{\prime}(\phi_{c})}. Here, the space-time argument of the field is suppressed. However, this integral is in general divergent since V=0V^{\prime}=0 at the both ends of the integral. In the vicinity of the domain where V=0V^{\prime}=0, we expect that the quantum fluctuations of the field would play an important role. Since the typical size of quantum fluctuations accumulated over the Hubble time is H/(2π)H/(2\pi), we may define the regulated quantity tHMt_{\text{HM}} as

tHM:=ϕfalse+H2πϕtopH2πdϕc3HV(ϕc),\displaystyle t_{\text{HM}}:=\int^{\phi_{\text{top}}-\frac{H}{2\pi}}_{\phi_{\text{false}}+\frac{H}{2\pi}}\mathrm{d}\phi_{c}\,\frac{3H}{V^{\prime}(\phi_{c})}\,, (64)

and we expect that tHMt_{\text{HM}} would correctly characterize the typical time scale of the HM tunneling. In particular, for our potential (42) we have

tHM\displaystyle t_{\text{HM}} =3H2g2α2(1+β)[(3+β1β)log|11βH/2πα|log|12H/2πα1+1+βH/2πα|]1H𝒪((H/gα)2).\displaystyle=\frac{3H}{2g^{2}\alpha^{2}\left(1+\beta\right)}\left[\left(\frac{3+\beta}{1-\beta}\right)\log\left|1-\frac{1-\beta}{H/2\pi\alpha}\right|-\log\left|\frac{1-\frac{2}{H/2\pi\alpha}}{1+\frac{1+\beta}{H/2\pi\alpha}}\right|\right]\sim\frac{1}{H}\cdot\mathcal{O}\left((H/g\alpha)^{2}\right)\,. (65)

Since we have (H/gα)2(H2/V′′)ϕfalseϕcϕtop1(H/g\alpha)^{2}\sim(H^{2}/V^{\prime\prime})_{\phi_{\text{false}}\lesssim\phi_{c}\lesssim\phi_{\text{top}}}\gg 1 for the shallow potential, we conclude that the time scale of HM tunneling is much longer than the Hubble time.

4.2.1 Remark

So far it is found that, starting from (LABEL:eq:ConditionalFull), the configuration (58) approximately solves the Hamilton’s equations (57) and reproduce the previous result (52) when it is substituted into the action. There is actually an important reason behind why we should choose the configuration (58) to evaluate the HM tunneling process.

To see this, it is important to realize an important difference between the current Hamilton’s equations (57) and the previous one (48); the equation for ϕc\phi_{c} now contains Π¯Δ\overline{\Pi}_{\Delta} rather than ΠΔ\Pi_{\Delta}. Due to this difference, the structures of Hamilton’s equations (57) are understood as follows;

  • the equation for ϕc\phi_{c} (57a) is determined once Π¯Δ\overline{\Pi}_{\Delta} is specified,

  • Π¯Δ(t,𝒙)\overline{\Pi}_{\Delta}(t,\bm{x}) is understood as initial conditions for (57b) since Π¯Δ(t,𝒙)\overline{\Pi}_{\Delta}(t,\bm{x}) contains only the boundary modes satisfying k=kc(t)k=k_{c}(t). Hence, ΠΔ(t,𝒙)\Pi_{\Delta}(t,\bm{x}) is obtained by solving (57b) for given Π¯Δ\overline{\Pi}_{\Delta} under the condition (57a).

On top of that, substituting the Hamilton’s equation for ϕc\phi_{c} into the action, we have the first line of (63) which can be rewritten as

I=12ttdtd3k(2π)3ΠΔ(t,𝒌)ΠΔ(t,𝒌)H22k3δ(ttk).\displaystyle I=-\frac{1}{2}\int^{t_{*}}_{t^{\prime}}\mathrm{d}t\,\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\,\Pi_{\Delta}(t,\bm{k})\Pi_{\Delta}(t,-\bm{k})\frac{H^{2}}{2k^{3}}\delta(t-t_{k})\,. (66)

The RHS depends only on the value of ΠΔ(t,𝒌)|k=kc(t)\Pi_{\Delta}(t,\bm{k})|_{k=k_{c}(t)}. Hence, we can evaluate the tunneling action once Π¯Δ\overline{\Pi}_{\Delta} is specified, provided that (66) or equivalently (LABEL:eq:ConditionalFull) is reliable.

We claim that (LABEL:eq:ConditionalFull) will be valid when Π¯Δ\overline{\Pi}_{\Delta} is chosen so that ΠΔ(t>tk,𝒌)\Pi_{\Delta}(t>t_{k},\bm{k}) becomes a smooth function in time. Otherwise, it will not be justified to ignore the higher-order corrections δHhigher\delta H_{\text{higher}} which are neglected in (LABEL:eq:ConditionalFull). Intuitively, this states that perturbation theory tend to be broken down around exotic configurations. When ΠΔ\Pi_{\Delta} is a smooth function, we can relate Π¯Δ\overline{\Pi}_{\Delta} to ΠΔ\Pi_{\Delta} after the suitable smearing in time:

Π¯Δ(t,𝒙)time c.g.d3xΠΔ(t,𝒙)W(|𝒙𝒙|;t)𝒱ΠΔ(t,𝒙).\displaystyle\overline{\Pi}_{\Delta}(t,\bm{x})\xrightarrow{\text{time c.g.}}\int\mathrm{d}^{3}x^{\prime}\Pi_{\Delta}(t,\bm{x}^{\prime})W(|\bm{x}-\bm{x}^{\prime}|;t)\sim\mathcal{V}\Pi_{\Delta}(t,\bm{x})\,. (67)

Here, we also used ΠΔ(t,𝒙)ΠΔ(t,𝒙)\Pi_{\Delta}(t,\bm{x})\sim\Pi_{\Delta}(t,\bm{x}^{\prime}) for |𝒙𝒙|kc1|\bm{x}-\bm{x}^{\prime}|\lesssim k_{c}^{-1} and defined 𝒱:=(4π/3)kc3(t)d3xW(|𝒙𝒙|;t)\mathcal{V}:=(4\pi/3)k_{c}^{-3}(t)\sim\int\mathrm{d}^{3}x^{\prime}\,W(|\bm{x}-\bm{x}^{\prime}|;t). We then require that the Hamilton’s equation for ΠΔ\Pi_{\Delta} (57b) is satisfied in a good approximation to ensure the validity of (LABEL:eq:ConditionalFull). This constrains the choice of Π¯Δ\overline{\Pi}_{\Delta}. Indeed, the configuration (58) approximately solves (57b) and satisfies the smoothness and henceforth (67) after the smearing. This would be the reason why our analysis with (58) based on (LABEL:eq:ConditionalFull) can reproduce the correct result.

4.3 On the ε\varepsilon-independence of the Hawking-Moss tunneling

In sections 4.1 and 4.2, the tunneling probability of a coarse-grained patch with a physical radius (εH)1(\varepsilon H)^{-1} is calculated. Our results coincide with the HM tunneling and are independent of ε\varepsilon.

The ε\varepsilon-independence of the results would be a consequence of the scale-independence of the dynamics of light scalar fields at super-horizon scales. To see this, it is useful to notice that a coarse-grained patch of physical radius (ε1H)1(\varepsilon_{1}H)^{-1} at a time t=Tt=T expands to a patch of larger physical radius (ε2H)1(\varepsilon_{2}H)^{-1} at a later time t=T+δt>Tt=T+\delta t>T with ε2=ε1exp[Hδt]<ε11\varepsilon_{2}=\varepsilon_{1}\exp[-H\delta t]<\varepsilon_{1}\ll 1. The value of IR field does not evolve from t=Tt=T to T+δtT+\delta t because the fluctuations of light scalar field at super-horizon scales are approximately time-independent,

d3k(2π)3ϕc(t,𝒌)ei𝒌.𝒙θ(kc(t)k)d3k(2π)3ϕc(t+δt,𝒌)ei𝒌.𝒙θ(kc(t)k),\displaystyle\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\,\phi_{c}(t,\bm{k})e^{i\bm{k}.\bm{x}}\theta(k_{c}(t)-k)\simeq\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\,\phi_{c}(t+\delta t,\bm{k})e^{i\bm{k}.\bm{x}}\theta(k_{c}(t)-k)\,, (68)

unless δt\delta t is much longer than H1H^{-1}. Hence, we can relate the coarse-grained dynamics of different ε1\varepsilon\ll 1 by considering the time shift tt+δtt\to t+\delta t with the value of IR field being kept fixed. This means that the tunneling probability from ϕ=ϕfalse\phi=\phi_{\text{false}} to ϕtrue\phi_{\text{true}} of a patch with physical radius (εH)1(\varepsilon H)^{-1} should be independent of ε\varepsilon.

5 Coleman-de Luccia tunneling

In the previous section, the result of the HM instanton is reproduced by using (LABEL:eq:ConditionalFull). We expect that the formula (LABEL:eq:ConditionalFull) can describe not only the HM tunneling but also the CDL tunneling. In other words, we expect that there will be a flow line starting from the false vacuum to the bubble configurations as illustrated in FIG. 5. In this section, we concretely show an interesting configuration by following the prescription in the previous section.

Refer to caption
Figure 5: A schematic picture of Hamiltonian flows in the ”field” phase space. We expect that there is a flow line which starts from the false vacuum (left intersection) and reaches the bubble configuration (right intersection) through a non-zero ϕΔ(𝒙)\phi_{\Delta}(\bm{x}) path.

5.1 Coleman-de Luccia bubble solution

In Euclidean method, the CDL instanton is dominant rather than the HM instanton when the potential barrier is steep Jensen:1983ac ; Jensen:1988zx ; Hackworth:2004xb ; Batra:2006rz . By taking ε1\varepsilon\gg 1, we can study nonperturbative physics at sub-horizon scales such as the formation of bubble. In this case, GΠΠG^{\Pi\Pi} becomes dominant and the other noises can be ignored in (34). Under this approximation, the exponent of the integrand of (LABEL:eq:ConditionalFull) is linear in ΠΔ\Pi_{\Delta}. We can then perform the path integral 𝒟ΠΔ\int\mathcal{D}\Pi_{\Delta} in (LABEL:eq:ConditionalFull), yielding the product of delta functions 𝒙δ(ϕ˙ca3Πc)\prod_{\bm{x}}\delta\bigl{(}\dot{\phi}_{c}-a^{-3}\Pi_{c}\bigr{)}. These delta functions eliminate the path integral 𝒟Πc\int\mathcal{D}\Pi_{c}.888This is the reason why we illustrate flow lines in the (ϕc,ϕΔ)(\phi_{c},\phi_{\Delta})-plane in FIG. 5. Furthermore, we change the integration variable as ϕΔiϕΔ\phi_{\Delta}\to-i\phi_{\Delta} in (LABEL:eq:ConditionalFull), leading to

p𝒟(ϕc,ϕΔ)exp[d4x(a3ϕ˙Δϕ˙cHCDL(ϕc,ϕΔ))]p\simeq\int\mathcal{D}(\phi_{c},\phi_{\Delta})\exp\left[\int\mathrm{d}^{4}x\,\left(a^{3}\dot{\phi}_{\Delta}\dot{\phi}_{c}-H_{\text{CDL}}(\phi_{c},\phi_{\Delta})\right)\right] (69)

with appropriate boundary conditions; we consider bubble configurations as boundary conditions later. Here, the Hamiltonian HCDLH_{\text{CDL}} is defined by

HCDL(ϕc,ϕΔ):=(a2ϕca3V(ϕc))ϕΔa32ϕΔ(x)ϕ¯Δ(x),H_{\text{CDL}}(\phi_{c},\phi_{\Delta}):=-\left(a\nabla^{2}\phi_{c}-a^{3}V^{\prime}(\phi_{c})\right)\phi_{\Delta}-\frac{a^{3}}{2}\phi_{\Delta}(x)\overline{\phi}_{\Delta}(x)\,, (70)

with

ϕ¯Δ(t,𝒙):=Hkc4(t)4π2a(t)d3xj0(kc(t)|𝒙𝒙|)ϕΔ(t,𝒙).\displaystyle\overline{\phi}_{\Delta}(t,\bm{x}):=\frac{Hk_{c}^{4}(t)}{4\pi^{2}a(t)}\int\mathrm{d}^{3}x^{\prime}\,j_{0}\left(k_{c}(t)|\bm{x}-\bm{x}^{\prime}|\right)\phi_{\Delta}(t,\bm{x}^{\prime})\,. (71)

We would like to find the appropriate configuration ϕ¯Δ\overline{\phi}_{\Delta} which describes the tunneling process. Following the choice made in sec. 4, let us suppose that the appropriate choice is given by the configuration for which the Hamiltonian (70) vanishes:

ϕ¯Δ(x)=0,2(a22ϕcV(ϕc)).\overline{\phi}_{\Delta}(x)=0\,,\,-2(a^{-2}\nabla^{2}\phi_{c}-V^{\prime}(\phi_{c}))\,. (72)

Note that this condition is imposed up to the suitable smearing in time because ϕ¯Δ(t,𝒙)\overline{\phi}_{\Delta}(t,\bm{x}) includes only the boundary Fourier mode k=kc(t)k=k_{c}(t). As discussed in sec. 4.2.1, ϕΔ\phi_{\Delta} becomes sufficiently smooth for the appropriate ϕ¯Δ\overline{\phi}_{\Delta}, and hence we also suppose

ϕ¯ΔH2ε3πϕΔ(x)\displaystyle\overline{\phi}_{\Delta}\sim\frac{H^{2}\varepsilon}{3\pi}\phi_{\Delta}(x) (73)

after the suitable averaging over the Hubble time, similarly to (67). We use the relation (73) to evaluate the action later. This would work at least for the purpose of estimating the action.

In principle, we do not need to use the estimate (73) in evaluating the action since it is determined once ϕ¯Δ\overline{\phi}_{\Delta} is specified based on the analogous logic discussed around (66). For this purpose, we need to specify the configurations {ϕΔ(t,𝒌)|k=kc(t)}\{\phi_{\Delta}(t,\bm{k})|_{k=k_{c}(t)}\} in momentum space which result in the sufficiently smooth ϕΔ\phi_{\Delta} that solves the Hamilton equations. It is not easy to find such appropriate configurations precisely, however. Hence, we leave more careful analysis on the choice of ϕ¯Δ\overline{\phi}_{\Delta} for future work. In this study, instead, we focus on how we can proceed the analysis for given configuration (72) with adopting the estimate (73) and how the bubble nucleation process could be described in the stochastic approach.

Using the relation (73), the Hamiltonian (70) and the configuration (72) become

HCDL(a2ϕca3V(ϕc))ϕΔH2ε6πa3ϕΔ2,\displaystyle H_{\text{CDL}}\sim-\left(a\nabla^{2}\phi_{c}-a^{3}V^{\prime}(\phi_{c})\right)\phi_{\Delta}-\frac{H^{2}\varepsilon}{6\pi}a^{3}\phi_{\Delta}^{2}\,, (74)
ϕΔ(x)=0,6πH2ε(a22ϕcV(ϕc)).\displaystyle\phi_{\Delta}(x)=0\,,\,-\frac{6\pi}{H^{2}\varepsilon}(a^{-2}\nabla^{2}\phi_{c}-V^{\prime}(\phi_{c}))\,. (75)

The Hamilton’s equations under the constraints (75) give the following equation of motions for ϕc\phi_{c}:

ϕ¨c+3Hϕ˙c\displaystyle\ddot{\phi}_{c}+3H\dot{\phi}_{c} =(V(ϕc)a22ϕc),(ϕΔ=0),\displaystyle=-(V^{\prime}(\phi_{c})-a^{-2}\nabla^{2}\phi_{c}),\quad(\phi_{\Delta}=0),
ϕ¨c+3Hϕ˙c\displaystyle\ddot{\phi}_{c}+3H\dot{\phi}_{c} =V(ϕc)a22ϕc,(ϕΔ=6πH2ε(a22ϕcV(ϕc))).\displaystyle=V^{\prime}(\phi_{c})-a^{-2}\nabla^{2}\phi_{c},\qquad\,\,\,(\phi_{\Delta}=-\frac{6\pi}{H^{2}\varepsilon}(a^{-2}\nabla^{2}\phi_{c}-V^{\prime}(\phi_{c}))). (76)

Similar to the previous case (50), the signs of the potential term and the gradient term are flipped in the equation of motion with the non-trivial ϕΔ0\phi_{\Delta}\neq 0. Hence, we can expect that the tunneling process is realized. From (69), we find that only the solutions satisfying ϕΔ0\phi_{\Delta}\neq 0 contribute to the action. Then we focus on the second equation in (76).

Interestingly, this equation is the classical equation of motion in the Euclidean anti-de Sitter (AdS) space which is defined by the embedding equation

X02+X12+X22+X32+X42=H2\displaystyle-X_{0}^{2}+X_{1}^{2}+X_{2}^{2}+X_{3}^{2}+X_{4}^{2}=-H^{-2} (77)

in five-dimensional Minkowski spacetime

ds2=dX02+dX12+dX22+dX32+dX42.\displaystyle\mathrm{d}s^{2}=-\mathrm{d}X_{0}^{2}+\mathrm{d}X_{1}^{2}+\mathrm{d}X_{2}^{2}+\mathrm{d}X_{3}^{2}+\mathrm{d}X_{4}^{2}\,. (78)

In fact, the d’Alembert operator t2+3Ht+a22\partial_{t}^{2}+3H\partial_{t}+a^{-2}\nabla^{2} can be obtained from the following induced metrics;

ds2=dt2+e2Htd𝒙2=1H2η2(dη2+d𝒙2)=H2(dρ2+sinh2ρdΩ2),\displaystyle\mathrm{d}s^{2}=\mathrm{d}t^{2}+e^{2Ht}\mathrm{d}\bm{x}^{2}=\frac{1}{H^{2}\eta^{2}}(\mathrm{d}\eta^{2}+\mathrm{d}\bm{x}^{2})=H^{-2}(\mathrm{d}\rho^{2}+\sinh^{2}\rho\,\mathrm{d}\Omega^{2})\ , (79)

where dΩ2:=dθ12+sin2θ1dθ22+sin2θ1sin2θ2dθ32\mathrm{d}\Omega^{2}:=\mathrm{d}\theta_{1}^{2}+\sin^{2}\theta_{1}\mathrm{d}\theta_{2}^{2}+\sin^{2}\theta_{1}\sin^{2}\theta_{2}\mathrm{d}\theta_{3}^{2} and 0<ρ<0<\rho<\infty, 0θ1π0\leq\theta_{1}\leq\pi, 0θ2π0\leq\theta_{2}\leq\pi and 0θ32π0\leq\theta_{3}\leq 2\pi. The second metric is that in the Poincaré coordinates and the third one is that in the global coordinates. The explicit coordinate transformations are given by

X0\displaystyle X_{0} =12η2+𝒙2+H2η=H1coshρ,\displaystyle=\frac{1}{2}\frac{\eta^{2}+\bm{x}^{2}+H^{-2}}{-\eta}=H^{-1}\cosh\rho,
X1\displaystyle X_{1} =x1Hη=H1sinhρsinθ1cosθ2,\displaystyle=\frac{x_{1}}{-H\eta}=H^{-1}\sinh\rho\sin\theta_{1}\cos\theta_{2},
X2\displaystyle X_{2} =x2Hη=H1sinhρsinθ1sinθ2cosθ3,\displaystyle=\frac{x_{2}}{-H\eta}=H^{-1}\sinh\rho\sin\theta_{1}\sin\theta_{2}\cos\theta_{3},
X3\displaystyle X_{3} =x3Hη=H1sinhρsinθ1sinθ2sinθ3,\displaystyle=\frac{x_{3}}{-H\eta}=H^{-1}\sinh\rho\sin\theta_{1}\sin\theta_{2}\sin\theta_{3},
X4\displaystyle X_{4} =12η2+𝒙2H2η=H1sinhρcosθ1.\displaystyle=\frac{1}{2}\frac{\eta^{2}+\bm{x}^{2}-H^{-2}}{-\eta}=H^{-1}\sinh\rho\cos\theta_{1}. (80)

For later convenience, we derive the relation between (η,r:=|𝒙|)(\eta,r:=|\bm{x}|) and (ρ,σ1)(\rho,\sigma_{1}) as

Hη=1coshρsinhρcosθ1,r=H1sinhρsinθ1coshρsinhρcosθ1.-H\eta=\frac{1}{\cosh\rho-\sinh\rho\cos\theta_{1}}\,,\qquad r=H^{-1}\frac{\sinh\rho\sin\theta_{1}}{\cosh\rho-\sinh\rho\cos\theta_{1}}\,. (81)

From this, we can check that a point (η,r)=(H1,0)(\eta,r)=(-H^{-1},0) is mapped to ρ=0\rho=0 for any θ1[0,π]\theta_{1}\in[0,\pi]. Except for this, there is one-to-one correspondence between points in the (η,r)(\eta,r)-plane with η0\eta\leq 0 and r0r\geq 0 and points in the (ρ,θ1)(\rho,\theta_{1})-plane with ρ>0\rho>0 and 0θ1π0\leq\theta_{1}\leq\pi. On a constant-η\eta slice in the (η,r)(\eta,r)-plane, the value of ρ\rho for given spatial point rr is given by

ρ=arccosh(12H2(η2+r2)+1Hη).\rho=\text{arccosh}\bigg{(}\frac{1}{2}\frac{H^{2}(\eta^{2}+r^{2})+1}{-H\eta}\bigg{)}. (82)

This function increases monotonically in rr for given η\eta in the region r>0r>0.

From the global coordinate (79), we see the Euclidean AdS spacetime has O(4)O(4) symmetry. Hence, we assume that the field ϕc\phi_{c} depends only on ρ\rho. Thus the second equation of (76) reads

d2ϕcdρ2+3tanhρdϕcdρ=V(ϕc)H2.\displaystyle\frac{\mathrm{d}^{2}\phi_{c}}{\mathrm{d}\rho^{2}}+\frac{3}{\tanh\rho}\frac{\mathrm{d}\phi_{c}}{\mathrm{d}\rho}=\frac{V^{\prime}(\phi_{c})}{H^{2}}. (83)

Note that this is the same equation utilized in the Euclidean method Coleman:1980aw ; Rubakov:1999ir . Imposing the boundary conditions Coleman:1977py ; Coleman:1980aw

limρϕc=α,dϕcdρ|ρ=0=0,\displaystyle\lim_{\rho\to\infty}\phi_{c}=-\alpha,\quad\frac{d\phi_{c}}{d\rho}\bigg{|}_{\rho=0}=0, (84)

we obtain the bubble solutions as is shown in FIG. 6. Note that the latter condition ensures the continuity of ηϕc(η,r)\partial_{\eta}\phi_{c}(\eta,r) and η2ϕc(η,r)\partial_{\eta}^{2}\phi_{c}(\eta,r) at (Hη,Hr)=(1,0)(H\eta,Hr)=(-1,0).

It is useful to fit the bubble configurations by the following fitting function (FIG. 6);

ϕc(ρ)=αtanhμ(ρρ¯),\displaystyle\phi_{c}(\rho)=-\alpha\tanh\mu(\rho-\bar{\rho}), (85)

where μ\mu and ρ¯\bar{\rho} represent the thickness and the position of the bubble wall, respectively. Note that, for β0.6\beta\gtrsim 0.6, the deviation from the true vacuum at the ρ=0\rho=0 becomes significant Weinberg:2012pjx and the fitting (85) becomes bad.

Refer to caption
Figure 6: The tunneling configuration for the inhomogeneous field is plotted. The solid curve is the numerical solution for β=0.5\beta=0.5 and αg/H=140\alpha g/H=\sqrt{140}. We take the initial conditions as ϕc(1015)/α=14.98284×102\phi_{c}(10^{-15})/\alpha=1-4.98284\times 10^{-2} and ϕc(1015)/α=0\phi_{c}^{\prime}(10^{-15})/\alpha=0. The dashed curve is the fitting function (85) where μ=7.32515\mu=7.32515 and ρ¯=0.34397\bar{\rho}=0.34397.

We also have to examine the boundary conditions in the Hamilton flow. As in the case of HM tunneling, we expect that there are several intersections where ϕΔ=0\phi_{\Delta}=0 (FIG. 5). Since we have the concrete ϕΔ\phi_{\Delta} (75) and the bubble configurations (85), it is possible to obtain the curves in (r,η)(r,\eta)-plane on which ϕΔ=0\phi_{\Delta}=0. Using (75) and (76), such curves are given as

F(η,r):=η2ϕc2ηηϕc=0.F(\eta,r):=\partial_{\eta}^{2}\phi_{c}-\frac{2}{\eta}\partial_{\eta}\phi_{c}=0. (86)

Note that this is equivalent to solve a22ϕcV(ϕc)=0a^{-2}\nabla^{2}\phi_{c}-V^{\prime}(\phi_{c})=0. Substituting (75) into (86) and using the fitting formula (85), we find four solutions which are expressed as four lines in the (η,r)(\eta,r)-plane; two of them are placed at η=\eta=-\infty with fixed rr and r=r=\infty with fixed η\eta. These correspond to ρ=\rho=\infty where ϕ=α\phi=-\alpha (FIG. 6). Also, we numerically find other two non-trivial hypersurfaces (FIG. 7(a)). It can be seen that one of the curves is totally spacelike but another is partially timelike. Thus, it seems natural to take η=\eta=-\infty curve as an initial time slice on which ϕ\phi is false vacuum and totally spacelike non-trivial curve as a final time slice on which the bubble is nucleated. We denote the region between the two spacelike curves as Σ\Sigma.

As a matter of fact, the configurations on the final time slice has a bubble. It can be checked as follows; the value of ϕc\phi_{c} at the origin exceeds the top of potential hill. In the case of FIG. 7(a) where we set (β,αg/H)=(0.5,140)(\beta,\alpha g/H)=(0.5,\sqrt{140}), we have ϕc/α0.1>0.5=β\phi_{c}/\alpha\sim-0.1>-0.5=-\beta at Hr=0,Hη0.7Hr=0,H\eta\sim-0.7.

Refer to caption
(a)
Refer to caption
(b)
Refer to caption
(c)
Refer to caption
(d)
Figure 7: (a): The two non-trivial curves on which (86) is satisfied. We insert the mesh to confirm whether the curves are spacelike or timelike. It can be seen that the upper line is spacelike but the lower one is partially timelike. (b): The integration region for (87). There are another spacelike curve at η=\eta=-\infty. (c): The two non-trivial curves in (ρ,θ1)(\rho,\theta_{1}) plane is plotted. (d): The integration region for (87) in (ρ,θ1)(\rho,\theta_{1}) plane. All plots are the case for β=0.5\beta=0.5 and αg/H=140.\alpha g/H=\sqrt{140}.

Now, we can evaluate the action for the bubble configurations for Σ\Sigma (FIG. 7(b) or (d)). We use the fitting function (85) for the numerical integration.

I\displaystyle I Σd4x[a3ϕΔ(ϕ¨c+3Hϕ˙c)HCDL]\displaystyle\simeq\int_{\Sigma}\mathrm{d}^{4}x\left[-a^{3}\phi_{\Delta}\left(\ddot{\phi}_{c}+3H\dot{\phi}_{c}\right)-H_{\text{CDL}}\right]
=6πH6εΣdρdθ1dθ2dθ3sin2θ1sinθ2sinh3ρ(coshρsinhρcosθ1)4(η2ϕc2ηηϕc)2\displaystyle=-\frac{6\pi}{H^{6}\varepsilon}\int_{\Sigma}\mathrm{d}\rho\mathrm{d}\theta_{1}\mathrm{d}\theta_{2}\mathrm{d}\theta_{3}\frac{\sin^{2}\theta_{1}\sin\theta_{2}\sinh^{3}\rho}{(\cosh\rho-\sinh\rho\cos\theta_{1})^{4}}\bigg{(}\partial_{\eta}^{2}\phi_{c}-\frac{2}{\eta}\partial_{\eta}\phi_{c}\bigg{)}^{2}
=24π2H2εΣdρdθ1sin2θ1sinh3ρ[(sinhρcoshρcosθ1)2(coshρsinhρcosθ1)22ϕcρ2\displaystyle=-\frac{24\pi^{2}}{H^{2}\varepsilon}\int_{\Sigma}\mathrm{d}\rho\mathrm{d}\theta_{1}\sin^{2}\theta_{1}\sinh^{3}\rho\bigg{[}\frac{(\sinh\rho-\cosh\rho\cos\theta_{1})^{2}}{(\cosh\rho-\sinh\rho\cos\theta_{1})^{2}}\frac{\partial^{2}\phi_{c}}{\partial\rho^{2}}
+{3sinhρcoshρcosθ1coshρsinhρcosθ1+sin2θ1tanhρ(coshρsinhρcosθ1)2}ϕcρ]2\displaystyle\quad\,+\bigg{\{}3\frac{\sinh\rho-\cosh\rho\cos\theta_{1}}{\cosh\rho-\sinh\rho\cos\theta_{1}}+\frac{\sin^{2}\theta_{1}}{\tanh\rho(\cosh\rho-\sinh\rho\cos\theta_{1})^{2}}\bigg{\}}\frac{\partial\phi_{c}}{\partial\rho}\bigg{]}^{2}
:=24π2α2H2εI~(μ,ρ¯).\displaystyle:=-\frac{24\pi^{2}\alpha^{2}}{H^{2}\varepsilon}\tilde{I}(\mu,\bar{\rho}). (87)

In the second line, we used HCDL=0H_{\text{CDL}}=0, (75) and (76). Also we performed a coordinate transformation (t,r)(ρ,θ1)(t,r)\to(\rho,\theta_{1}). In the third line, the following relations are used

2ηϕc(ρ)η=2ηρηϕc(ρ)ρ=2H2(coshρsinhρcosθ1)(sinhρcoshρcosθ1)ϕc(ρ)ρ,\displaystyle-\frac{2}{\eta}\frac{\partial\phi_{c}(\rho)}{\partial\eta}=-\frac{2}{\eta}\frac{\partial\rho}{\partial\eta}\frac{\partial\phi_{c}(\rho)}{\partial\rho}=2H^{2}(\cosh\rho-\sinh\rho\cos\theta_{1})(\sinh\rho-\cosh\rho\cos\theta_{1})\frac{\partial\phi_{c}(\rho)}{\partial\rho},

and

2ϕc(ρ)η2\displaystyle\frac{\partial^{2}\phi_{c}(\rho)}{\partial\eta^{2}} =\displaystyle= H2[(sinhρcoshρcosθ1)22ρ2\displaystyle H^{2}\bigg{[}(\sinh\rho-\cosh\rho\cos\theta_{1})^{2}\frac{\partial^{2}}{\partial\rho^{2}}
+{(sinhρcoshρcosθ1)(coshρsinhρcosθ1)+sin2θ1tanhρ}ρ]ϕc(ρ).\displaystyle+\bigg{\{}(\sinh\rho-\cosh\rho\cos\theta_{1})(\cosh\rho-\sinh\rho\cos\theta_{1})+\frac{\sin^{2}\theta_{1}}{\tanh\rho}\bigg{\}}\frac{\partial}{\partial\rho}\bigg{]}\phi_{c}(\rho).

Here, the partial differentiation with respect to η\eta is taken while keeping rr constant.

5.2 Discussions

5.2.1 Appropriate choice of ε\varepsilon

Since our results (87) depend on ε\varepsilon, we need to choose some specific value of ε\varepsilon to predict the tunneling rate. We emphasize that the ε\varepsilon dependence does not imply the pathology of our result. Rather our results should depend on ε\varepsilon because the non-perturbative effects from UV modes are missed in our formalism as discussed in section 3.2. We then choose ε\varepsilon as large as possible to evaluate the tunneling rate.

Our analysis will be valid only when the value of ε\varepsilon lies in a certain range. Below, we briefly discuss necessary conditions for ε\varepsilon to justify our analysis.

Lower bound on ε\varepsilon.

We need to choose sufficiently large ε\varepsilon so that IR fields can describe the bubble configuration. This imposes that (εH)1(\varepsilon H)^{-1} should be smaller than the typical physical size of the bubble or the bubble wall. This condition will be satisfied by taking εμ\varepsilon\gtrsim\mu for our parameter choices.

Upper bound on ε\varepsilon.

Our analysis is based on Eq.(LABEL:eq:ConditionalFull) which will be invalid when quantum fluctuations of IR fields are too large. This imposes an upper bound on ε\varepsilon because the size of fluctuations of ϕc\phi_{c} at the scale kkc(t)k\sim k_{c}(t) is proportional to ε\varepsilon:

δϕc|kkc:=[d3k(2π)3δ(ln(k/kc(t)))|ϕ^(t,𝒌)|2]1/2kc/a2π=εH2π,\delta\phi_{c}|_{k\sim k_{c}}:=\left[\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\,\delta\left(\ln(k/k_{c}(t))\right)\langle|\hat{\phi}(t,\bm{k})|^{2}\rangle\right]^{1/2}\approx\frac{k_{c}/a}{2\pi}=\frac{\varepsilon H}{2\pi}\,, (88)

where we assumed (kc/a)2V′′(ϕc)(k_{c}/a)^{2}\gg V^{\prime\prime}(\phi_{c}) 999This is compatible with the condition ε<α/H\varepsilon<\alpha/H when the weak coupling g1g\ll 1 is considered. and approximated ϕ\phi as a massless scalar field.

As discussed in section 3.2, (LABEL:eq:ConditionalFull) will be justified when the term δH\delta H is negligible. Then, we define the ratio 𝒬\mathcal{Q} of the term δH\delta H to the final term on the RHS of (74) as 101010We can also compare δH\delta H with the second and the third term on the RHS of (74). Such considerations do not change our estimate of εmax\varepsilon_{\text{max}} in (89).

𝒬:=|δHH2εa3ϕΔ2/(6π)|ϕΔ=6πH2ε(a22ϕcV(ϕc))=3π22ε2H4|V′′′(ϕc)(a22ϕcV(ϕc))|,\mathcal{Q}:=\left|\frac{\delta H}{H^{2}\varepsilon\,a^{3}\phi_{\Delta}^{2}/(6\pi)}\right|_{\phi_{\Delta}=-\frac{6\pi}{H^{2}\varepsilon}(a^{-2}\nabla^{2}\phi_{c}-V^{\prime}(\phi_{c}))}=\frac{3\pi^{2}}{2\varepsilon^{2}H^{4}}\left|V^{\prime\prime\prime}(\phi_{c})\left(a^{-2}\nabla^{2}\phi_{c}-V^{\prime}(\phi_{c})\right)\right|\,,

and we impose 𝒬<1\mathcal{Q}<1. In the second equality, we used δH=(a3/24)V′′′(ϕc)ϕΔ3\delta H=(a^{3}/24)V^{\prime\prime\prime}(\phi_{c})\phi_{\Delta}^{3}. Similarly to (88), we can estimate the size of quantum fluctuations of a22ϕa^{-2}\nabla^{2}\phi. Then, we estimate 𝒬\mathcal{Q} at large ε\varepsilon as 𝒬g2αε/H\mathcal{Q}\sim g^{2}\alpha\varepsilon/H where we also used |V′′′(ϕc)|g2α|V^{\prime\prime\prime}(\phi_{c})|\sim g^{2}\alpha for |ϕc|α|\phi_{c}|\lesssim\alpha. The condition ε<H/(g2α)\varepsilon<H/(g^{2}\alpha) follows from 𝒬<1\mathcal{Q}<1.

Summary.

In summary, it is necessary to choose ε\varepsilon satisfying the following condition to justify our analysis,

μεεmax:=H/(g2α)755×(1.12×104g)(140gα/H).\mu\lesssim\varepsilon\lesssim\varepsilon_{\text{max}}:=H/(g^{2}\alpha)\approx 755\times\left(\frac{1.12\times 10^{-4}}{g}\right)\left(\frac{\sqrt{140}}{g\alpha/H}\right)\,. (89)

This suggests that, at least when gg is sufficiently tiny, we can reliably choose large ε\varepsilon. Note that we cannot make the action II given in (87) arbitrarily small even if we take εmax\varepsilon_{\text{max}}\to\infty in the free-theory limit g0g\to 0; for ε=εmax\varepsilon=\varepsilon_{\text{max}}, we have I|ε=εmaxg1(gα/H)3I~(μ,ρ¯)I|_{\varepsilon=\varepsilon_{\text{max}}}\sim-g^{-1}(g\alpha/H)^{3}\tilde{I}(\mu,\bar{\rho}). Roughly speaking, the small gα/Hg\alpha/H corresponds to the bubble radius being larger than the Hubble radius. Since we are interested in the bubble smaller than the Hubble radius, gα/Hg\alpha/H cannot be taken small arbitrarily.

A few more comments on the ε\varepsilon-dependence of our results are in order. Our result (87) shows that the value of II becomes larger for smaller choice of ε\varepsilon. This is because the size of quantum fluctuations of modes kεa(t)Hk\sim\varepsilon a(t)H is proportional to ε\varepsilon, while the nonperturbative physics caused by UV modes k>εa(t)Hk>\varepsilon a(t)H is truncated in our formalism. This interpretation however implicitly assumes that the modes kεmaxa(t)Hk\sim\varepsilon_{\text{max}}a(t)H are relevant for the tunneling process. We expect that this is the case because a kinetic energy of fluctuations of modes kεmaxa(t)Hk\sim\varepsilon_{\text{max}}a(t)H is estimated as (εmaxH)4(\varepsilon_{\text{max}}H)^{4} which is much smaller than the height of potential barrier ΔVg2α4\Delta V\sim g^{2}\alpha^{4} for our parameter choices.

By contrast, very short-scale physics which is insensitive to the detailed structure of V(ϕ)V(\phi) near its origin might be irrelevant for the tunneling process. Hence, we expect that the tunneling rate would converge to some finite value in the limit ε\varepsilon\to\infty. It would be interesting to see whether the tunneling rate converges to a finite value as ε\varepsilon increases, and if so, from which value of ε\varepsilon this convergence begins.

5.2.2 Hawking-Moss vs. Coleman-de Luccia

From the formula (LABEL:eq:ConditionalFull), we derived the two configurations which describe the tunneling from the false vacuum to the true vacuum. One is HM configuration and the other is CDL-like configuration. Using these configurations, we evaluate the probability of the tunneling. Here, we compare these probabilities. Denoting the action (87) and (52) as IbubbleI_{\text{bubble}} and IHMI_{\text{HM}}, the ratio of the two actions is given by

γ:=IbubbleIHM=9α2H2ΔVεI~(μ,ρ¯)=1ε108(1β)3(β+3)H2α2g2I~(μ,ρ¯)\displaystyle\gamma:=\frac{I_{\text{bubble}}}{I_{\text{HM}}}=\frac{9\alpha^{2}H^{2}}{\Delta V\varepsilon}\tilde{I}(\mu,\bar{\rho})=\frac{1}{\varepsilon}\frac{108}{(1-\beta)^{3}(\beta+3)}\frac{H^{2}}{\alpha^{2}g^{2}}\tilde{I}(\mu,\bar{\rho}) (90)

For example, if we choose β=0.5\beta=0.5 and αg/H=140\alpha g/H=\sqrt{140} (see FIG. 6), the fitting parameters become μ=7.32515\mu=7.32515 and ρ¯=0.34397\bar{\rho}=0.34397 and the ratio becomes γ=12.9840/ε\gamma=12.9840/\varepsilon. For these parameters, the upper bound of ϵ\epsilon is given as (89) and then γ\gamma can be smaller than one for appropriately small g. This means that the CDL bubble configuration is dominant rather than HM configuration. Results for other parameters are also shown in Table 1.

5.2.3 Comparison with the Euclidean method

We also compute the CDL action in Euclidean method (Appendix B) and compare the ratios of the CDL action to the HM action (Table 1). For ε>ε\varepsilon>\varepsilon_{*}, our tunneling process becomes more probable than the one predicted by the Euclidean method. As discussed in section 5.2.1, we can consistently choose ε>ε\varepsilon>\varepsilon_{*} for certain choices of parameters (g,α,β)(g,\alpha,\beta). Perhaps, our results may indicate the presence of tunneling process which is more probable than the Euclidean method.

β\beta g2α2/H2g^{2}\alpha^{2}/H^{2} 1ϕc(1015)/α1-\phi_{c}(10^{-15})/\alpha μ\mu ρ¯\bar{\rho} εγ\varepsilon\gamma γE\gamma^{E} ϵ\epsilon_{*}
0.3 80 4.87210×\times 10510^{-5} 6.22563 1.05197 355.089 0.247004 1437.58
0.4 80 5.20273×\times 10310^{-3} 5.99645 0.65257 64.1185 0.0909796 704.758
0.5 80 3.89106×\times 10210^{-2} 5.63444 0.475247 33.9526 0.0599470 566.376
0.3 140 3.50945×\times 10410^{-4} 8.13990 0.673305 52.2515 0.0486678 1073.64
0.4 140 8.96003×\times 10310^{-3} 7.82419 0.459659 19.2912 0.0239903 804.123
0.5 140 4.98284×\times 10210^{-2} 7.32515 0.34397 12.9840 0.0172063 754.606
Table 1: The values of γ\gamma for several parameter sets. First and second ones are potential parameters. Third one is the initial condition for the equation of motion (83). Forth and fifth ones are fitting parameters for (85). Sixth and seventh ones are the numerical results of (90) and (139). The last one is the cut-off parameter ϵ\epsilon for which (90) coincides with (139).

5.2.4 Bubble nucleation hypersurface and the subsequent evolution

We find the non-trivial spacelike hypersurface on which the bubble is nucleated (FIG. 7(a)), where the hypersurface is given by the condition F(η,r)=0F(\eta,r)=0 or equivalently a22ϕcV(ϕc)=0a^{-2}\nabla^{2}\phi_{c}-V^{\prime}(\phi_{c})=0. The subsequent evolution is then described by the one shown in the first line of (76) which is the standard classical equation of motion. The configuration on the hypersurface gives the initial data for the classical dynamics after the bubble nucleation.

The field value on the spacelike hypersurface does not reach the true vacuum but rather it lies between the true vacuum and the top of the potential as mentioned in the subsection 5.1. This is possible because the location of hypersurface is defined by the condition a22ϕcV(ϕc)=0a^{-2}\nabla^{2}\phi_{c}-V^{\prime}(\phi_{c})=0 where the gradient force is balanced with the potential force. Though it is non-trivial to solve the evolution starting from the general spacelike hypersurfaces, it is desirable to solve it to fully understand the formation of the true-vacuum bubble in our scenario.

We conclude this section by pointing out that our formalism naturally predicts that the condition ϕ¯Δ=0\overline{\phi}_{\Delta}=0 (or ϕΔ=0\phi_{\Delta}=0 via (73)) defines the hypersurface on which the quantum dynamics is switched to the classical dynamics and the non-trivial field configuration is nucleated. This would be the generic prediction of our formalism that holds true once the appropriate configuration ϕ¯Δ\overline{\phi}_{\Delta} is specified.

6 Conclusion

We studied the tunneling processes on de Sitter background by using the stochastic approach. A novel point is that we applied the MSRJD functional integral to the problem. In this formalism, the tunneling rate is obtained by evaluating the functional integral with the saddle-point approximation. Using this method, we investigated both the HM and the CDL tunnelings.

For the HM case, we first analyzed (31) which is the MSRJD functional integral of the stochastic equation (23) on a single spatial point. We succeeded in deriving the tunneling solution in the “phase space” (FIG. 3) which represents the tunneling process from the false vacuum, through the top of the potential hill, and finally to the true vacuum (FIG. 4). This solution has natural tunneling boundary conditions which cannot be obtained from the Euclidean method. The tunneling rate for this configuration coincides with that of the HM instanton at the leading order. In sec. 4.2, we succeeded in re-deriving this result starting from (LABEL:eq:ConditionalFull) which describes the stochastic dynamics in the global region covered by the flat chart. We also estimated the time scale of the HM tunneling as (64) which becomes much longer than the Hubble time scale. Our analysis clarifies the physical picture of the HM instanton, i.e., the HM transition probability represents the transition probability of a coarse-grained patch with a physical radius (εH)1(\varepsilon H)^{-1}. Some technical complications that arise in dealing with (LABEL:eq:ConditionalFull) and the way of handling them are remarked in sec. 4.2.1. Physically, these complications are due to the spatial correlations of stochastic noises.

For the CDL case, we found the configurations which describe the bubble nucleation process. The tunneling rates for the bubble configurations depend on the cutoff scale dividing IR and UV fields. We argued that this dependence comes from the truncation of the non-perturbative effects from UV modes. We also discussed the valid choice of the cutoff scale for which the MSRJD functional integral will be reliable. This consideration is based on the first-principles derivation of stochastic approach from the Schwinger-Keldysh formalism. With an appropriate cutoff scale, it turned out that the CDL tunneling rate is larger than the HM one for the steep potential barrier. However, as mentioned above (74), it has not yet been investigated if our configuration can be really used for estimating the tunneling action. This aspect would be important for evaluating the tunneling action, being left for future work. Nonetheless, we believe that our study clarifies how we can proceed the analysis and how the bubble nucleation process could be described in the stochastic approach; for instance, our formalism can naturally define the location of hypersurface on which the quantum dynamics is switched to the classical dynamics and the non-trivial field configuration is nucleated.

It is interesting to understand the relation between the stochastic approach and the Euclidean method. We compared the CDL tunneling rate in our method with that in Euclidean method and found the former becomes larger than the latter for the potential considered with a certain cutoff scale. It would be worth investigating the meaning of this result. Especially, we need to know a precise relation between the CDL instanton and our configuration. Intriguingly, our method is also related to that discussed in Braden:2018tky ; Blanco-Pillado:2019xny ; Hertzberg:2020tqa ; Tranberg:2022noe ; Hertzberg:2019wgx , where the bubble accidentally appears from the initial quantum fluctuations. In our method, however, we assume that we can neglect the non-perturbative effects from UV modes, the quantum component of the potential of the form V′′′(ϕc)ϕΔ3V^{\prime\prime\prime}(\phi_{c})\phi_{\Delta}^{3}, and that the configuration (75) can be used to estimate the tunneling rate. The first two are summarized into the term δH\delta H. We also assume the fixed background spacetime. The relaxation of these assumptions would be important to seek the relations among the three methods. It would also be useful to apply our path-integral method to the tunneling in flat space and make a comparison with the Euclidean method.

Once this relaxation is achieved, it would also be interesting to apply our method to tunneling phenomena where the backreaction to the background geometry is non-negligible and make comparisons with recently-discussed methods. For instance, the formalism of the Wheeler-DeWitt equation Kristiano:2018oyv ; Cespedes:2020xpn ; Maniccia:2022iqa and the tunneling potential Espinosa:2018voj must be related to ours because the HM exponent is reproduced. The tunneling in the black hole spacetime Gregory:2020cvy ; Gregory:2020hia is also interesting. Especially, Gregory:2020hia discussed the HM transition with a black hole from the viewpoint of the stochastic approach.

Our method using the saddle-point approximation effectively amounts to solving real-time quantum dynamics, which reduces to Starobinsky’s stochastic approach Starobinsky:1986fx ; Starobinsky:1994bd at leading order when the super-horizon dynamics in de Sitter space is considered. However, since our starting point is the Schwinger-Keldysh path integral, which can be formulated in a more generic setup and incorporates all the quantum effects in principle, we believe that our formalism sheds light on further studies of tunneling phenomena from a real-time perspective.

One of the advantage of our method is that it is applicable to a dynamical setup. The application of our method to the inflation models such as the chain inflation Freese:2004vs and the warm inflation Berera:1995ie is also intriguing. Using our method, we can study the tunneling process in the inflationary background under dissipation and fluctuations coming from circumference. We leave these issues for future work.

Author Contributions:

Conceptualization, T.M., J.S. and J.T.; Methodology, T.M., J.S. and J.T.; Software, T.M.; Investigation, T.M., J.S. and J.T.; Writing – original draft, T.M., J.S. and J.T.; Visualization, T.M. All authors have read and agreed to the published version of the manuscript.

Funding:

T. M. was supported by JST SPRING, Grant Number JPMJSP2148 and JSPS KAKENHI Grant Number JP23KJ1543. J. S. was in part supported by JSPS KAKENHI Grant Numbers JP17H02894, JP17K18778, JP20H01902, JP22H01220. J.T. is supported by IBS under the project code, IBS-R018-D1.

Data Availability Statement:

Data are contained within the article.

Conflicts of Interest:

The authors declare no conflict of interest.

Appendix A Stochastic approach from the first principle

In this section, we evaluate the generating functional for IR fields Z[JIR(T)]Z[J^{\text{IR}}(T)] defined in Eq.(38) to obtain (39). Note that each step we need to take for evaluating Z[JIR(T)]Z[J^{\text{IR}}(T)] is summarized in section 3.2.

A.1 Path integral representation

A path integral representation of Z[JIR(T)]Z[J^{\text{IR}}(T)] takes the following standard form,

Z[JIR(T)]=\displaystyle Z[J^{\text{IR}}(T)]= 𝒟(ϕ+,ϕ,Π+,Π)ei𝑱IR(ϕ+IR+ϕIR)/2\displaystyle\int\mathcal{D}(\phi_{+},\phi_{-},\Pi_{+},\Pi_{-})\,e^{i\bm{J}^{\text{IR}}\cdot(\bm{\phi}^{\text{IR}}_{+}+\bm{\phi}^{\text{IR}}_{-})/2}
×ei(SH+SH)𝒙δ(ϕ+(T,𝒙)ϕ(T,𝒙))Ψ0[ϕ+]Ψ0[ϕ],\displaystyle\quad\times e^{i(S^{+}_{H}-S^{-}_{H})}\prod_{\bm{x}}\delta(\phi_{+}(T,\bm{x})-\phi_{-}(T,\bm{x}))\Psi_{0}[\phi_{+}]\Psi^{*}_{0}[\phi_{-}]\,, (91)

where Ψ0[ϕ]\Psi_{0}[\phi] is an initial wave functional. We specify it more concretely in section A.2.1. SH±=t=Td4x(Π±ϕ˙±H[ϕ±,Π±])S_{H}^{\pm}=\int^{t=T}\mathrm{d}^{4}x(\Pi^{\pm}\dot{\phi}^{\pm}-H[\phi^{\pm},\Pi^{\pm}]) is a Hamiltonian action. After the rotation of the basis (X+,X)(Xc,XΔ):=(X++X2,X+X)(X_{+},X_{-})\to(X_{c},X_{\Delta}):=(\frac{X_{+}+X_{-}}{2},X_{+}-X_{-}) with X=ϕ,ΠX=\phi,\Pi, (91) is written as

Z[JIR(T)]=\displaystyle Z[J^{\text{IR}}(T)]= 𝒟(ϕc,ϕΔ,Πc,ΠΔ)ei𝑱IRϕcIReiSH[ϕc,ϕΔ,Πc,ΠΔ]𝒙δ(ϕΔ(T,𝒙))ρ0[ϕc,ϕΔ].\displaystyle\int\mathcal{D}(\phi_{c},\phi_{\Delta},\Pi_{c},\Pi_{\Delta})\,e^{i\bm{J}^{\text{IR}}\cdot\bm{\phi}^{\text{IR}}_{c}}e^{iS_{H}[\phi_{c},\phi_{\Delta},\Pi_{c},\Pi_{\Delta}]}\prod_{\bm{x}}\delta(\phi_{\Delta}(T,\bm{x}))\rho_{0}[\phi_{c},\phi_{\Delta}]\,. (92)

Here, we defined SH[ϕc,ϕΔ,Πc,ΠΔ]:=(SH+SH)|(X+,X)(Xc,XΔ)S_{H}[\phi_{c},\phi_{\Delta},\Pi_{c},\Pi_{\Delta}]:=(S_{H}^{+}-S_{H}^{-})|_{(X_{+},X_{-})\to(X_{c},X_{\Delta})} with X=ϕ,ΠX=\phi,\Pi. We also defined ρ0[ϕc,ϕΔ]:=Ψ0[ϕc+(ϕΔ/2)]Ψ0[ϕc(ϕΔ/2)]\rho_{0}[\phi_{c},\phi_{\Delta}]:=\Psi_{0}[\phi_{c}+(\phi_{\Delta}/2)]\Psi^{*}_{0}[\phi_{c}-(\phi_{\Delta}/2)].

A.2 Nonperturbative generating functional for IR sector

Now we explain how to calculate Z[JIR(T)]Z[J^{\text{IR}}(T)] non-perturbatively in the IR sector. This allows us to capture the non-perturbative physics of the sector kkc(t)k\leq k_{c}(t). Our strategy is to split the integration variables into UV modes k>kc(t)k>k_{c}(t) and IR modes kkc(t)k\leq k_{c}(t) for each time step tt, and perform the integration over UV variables to get Z[JIR(T)]Z[J^{\text{IR}}(T)]. One may simply split the integration variables Xa(t,𝒌)X_{a}(t,\bm{k}),111111In the main text, we use the notation X𝒌(t)X_{\bm{k}}(t) to write variables in momentum space. We however adopt the notation X(t,𝒌)X(t,\bm{k}) in this appendix since we have many subscripts such as cc and Δ\Delta. where X=(ϕ,Π)X=(\phi,\Pi) and a=(c,Δ)a=(c,\Delta), by the following replacement in (92):

Xa(t,𝒌){XaIR(t,𝒌)(ttk)XaUV(t,𝒌)(t<tk),X_{a}(t,\bm{k})\to\begin{cases}X_{a}^{\text{IR}}(t,\bm{k})&(t\geq t_{k})\\ X_{a}^{\text{UV}}(t,\bm{k})&(t<t_{k})\,,\end{cases} (93)

where tkt_{k} is defined by the condition kc(tk)=kk_{c}(t_{k})=k. It is then tempted to perform the integration over UV variables XaUVX^{\text{UV}}_{a} by using the Schwinger-Keldysh (or closed-time-path) formalism. However, the expression obtained from (92) after the replacement (93) does not have the product of delta functions 𝒌δ(ϕΔUV(tk0+,𝒌))\prod_{\bm{k}}\delta(\phi^{\text{UV}}_{\Delta}(t_{k}-0^{+},\bm{k})) at the final time t=tk0+t=t_{k}-0^{+}.121212Here, 0+0^{+} is the infinitesimal time step which is introduced to obtain path integral representation of unitary time evolution as usual. That is, the time contour for each UV ϕ\phi-variable with modes 0<kkc(T)0<k\leq k_{c}(T) is not closed at the final time. Hence, the usual Schwinger-Keldysh formalism does not apply for evaluating the integration over UV variables. To resolve this issue, Refs.Tokuda:2017fdh ; Tokuda:2018eqs proposed a new way of splitting integration variables. The splitting is given by (93) for X=ΠX=\Pi, while for ϕ\phi-variable it is defined by the following rule rather than (93):

ϕc(t,𝒌){ϕcIR(t,𝒌)(t>tk)ϕcUV(t,𝒌)(ttk),ϕΔ(t,𝒌){ϕΔIR(t,𝒌)(ttk)ϕΔUV(t,𝒌)(t<tk).\begin{array}[]{lr}\phi_{c}(t,\bm{k})\to\begin{cases}\phi_{c}^{\text{IR}}(t,\bm{k})&(t>t_{k})\\ \phi_{c}^{\text{UV}}(t,\bm{k})&(t\leq t_{k})\,,\end{cases}&\quad\phi_{\Delta}(t,\bm{k})\rightarrow\begin{cases}\phi_{\Delta}^{\text{IR}}(t,\bm{k})&\quad(t\geq t_{k})\\ \phi_{\Delta}^{\text{UV}}(t,\bm{k})&\quad(t<t_{k})\,.\end{cases}\end{array} (94)

In this replacement (94), the variables ϕΔUV(tk,𝒌)\phi^{\text{UV}}_{\Delta}(t_{k},\bm{k}) are absent while the variables ϕcUV(tk,𝒌)\phi^{\text{UV}}_{c}(t_{k},\bm{k}) are present. Therefore, in the expression obtained from (92) after the new replacement, the time contour for every UV ϕ\phi-variable including those for modes 𝒌\bm{k} with 0<kkc(T)0<k\leq k_{c}(T) is closed. This allows us to perform the integration over UV variables based on the Schwinger-Keldysh formalism as we see below. Note that there is no subtlety in the replacement of integration variables Xa(t,𝒌)X_{a}(t,\bm{k}) for a zero mode k=0k=0 and those for deep UV modes k>kc(T)k>k_{c}(T): in both replacement rules mentioned above, they are simply replaced by IR variables XaIR(t,𝒌)X_{a}^{\text{IR}}(t,\bm{k}) and UV variables XaUV(t,𝒌)X_{a}^{\text{UV}}(t,\bm{k}), respectively. The time contours for them are closed thanks to the product of delta functions in the original expression (92).

After the new replacement, the term SH[ϕc,ϕΔ,Πc,ΠΔ]S_{H}[\phi_{c},\phi_{\Delta},\Pi_{c},\Pi_{\Delta}] in the exponent of (92) is decomposed into three pieces: purely IR terms SHIR:=SH[ϕcIR,ϕΔIR,ΠcIR,ΠΔIR]S_{H}^{\text{IR}}:=S_{H}[\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{c},\Pi^{\text{IR}}_{\Delta}], purely UV terms SHUV:=SH[ϕcUV,ϕΔUV,ΠcUV,ΠΔUV]S_{H}^{\text{UV}}:=S_{H}[\phi^{\text{UV}}_{c},\phi^{\text{UV}}_{\Delta},\Pi^{\text{UV}}_{c},\Pi^{\text{UV}}_{\Delta}], and the remaining IR-UV mixing terms SmixedS_{\text{mixed}}:

SH[ϕc,ϕΔ,Πc,ΠΔ]SHIR+SHUV+Smixed.S_{H}[\phi_{c},\phi_{\Delta},\Pi_{c},\Pi_{\Delta}]\to S_{H}^{\text{IR}}+S_{H}^{\text{UV}}+S_{\text{mixed}}\,. (95)

In terms of these quantities, Z[JIR(T)]Z[J^{\text{IR}}(T)] can be formally written as Tokuda:2017fdh ; Tokuda:2018eqs

Z[JIR(T)]=\displaystyle Z[J^{\text{IR}}(T)]= 𝒟(ϕcIR,ϕΔIR,ΠcIR,ΠΔIR)ei𝑱IRϕcIReiSHIReiΓ\displaystyle\int\mathcal{D}(\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{c},\Pi^{\text{IR}}_{\Delta})\,e^{i\bm{J}^{\text{IR}}\cdot\bm{\phi}^{\text{IR}}_{c}}e^{iS_{H}^{\text{IR}}}e^{i\Gamma}
×kkc(T)δ(ϕΔIR(T,𝒌))0<kkc(T)δ(ϕcIR(tk,𝒌)),\displaystyle\times\prod_{k\leq k_{c}(T)}\delta(\phi^{\text{IR}}_{\Delta}(T,\bm{k}))\prod_{0<k\leq k_{c}(T)}\delta(\phi^{\text{IR}}_{c}(t_{k},\bm{k})), (96)

where iΓi\Gamma is the effective action for IR fields,

eiΓ:=𝒟(ϕcUV,ϕΔUV,ΠcUV,ΠΔUV)ei(SHUV+Smixed)k>0δ(ϕΔIR(tf(k),𝒌))ρ0[ϕcUV,ϕΔUV;ϕcIR,ϕΔIR],e^{i\Gamma}:=\int\mathcal{D}(\phi^{\text{UV}}_{c},\phi^{\text{UV}}_{\Delta},\Pi^{\text{UV}}_{c},\Pi^{\text{UV}}_{\Delta})\,e^{i(S_{H}^{\text{UV}}+S_{\text{mixed}})}\prod_{k>0}\delta(\phi^{\text{IR}}_{\Delta}(t_{f}(k),\bm{k}))\rho_{0}[\phi^{\text{UV}}_{c},\phi^{\text{UV}}_{\Delta};\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta}]\,, (97)

with tf(k):=min[T,tk]t_{f}(k):=\min[T,t_{k}]. Here, ρ0[ϕc,ϕΔ]ρ0[ϕcUV,ϕΔUV;ϕcIR,ϕΔIR]\rho_{0}[\phi_{c},\phi_{\Delta}]\to\rho_{0}[\phi^{\text{UV}}_{c},\phi^{\text{UV}}_{\Delta};\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta}] due to the replacement of variables. The IR variables (ϕcIR,ϕΔIR)(\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta}) in the argument of ρ0\rho_{0} contain only a zero mode. Since the time path for each UV ϕ\phi-variable is closed in (97), we can calculate iΓi\Gamma perturbatively as usual by writing the connected diagrams with nn external IR fields that are connected by UV propagators. The diagramatic rules such as vertex factors and symmetry factors follow the standard rules of Scheinger-Keldysh formalism for given vertexes in SHUV+SmixedS_{H}^{\text{UV}}+S_{\text{mixed}}.

Interestingly, due to the non-trivial replacement rule (94), the Πϕ˙\Pi\dot{\phi} terms in SHS_{H} also contribute to SmixedS_{\text{mixed}} Morikawa:1989xz ; Tolley:2008qv ; Tokuda:2017fdh ; Tokuda:2018eqs . Referring to such contributions and the remaining terms in SmixedS_{\text{mixed}} as StrS_{\text{tr}} and Smix-intS_{\text{mix-int}}, respectively, we have Smixed=Str+Smix-intS_{\text{mixed}}=S_{\text{tr}}+S_{\text{mix-int}} with 131313Precisely speaking, we need to perform the UV-IR splitting in the path integral with infinitesimal discrete time step for deriving StrS_{\text{tr}} correctly. After taking the continuum limit, we obtain (99); see also Tokuda:2018eqs . Furthermore, the form of Smix-intS_{\text{mix-int}} depends on the model. In our case, we have Smix-int=d4x\displaystyle S_{\text{mix-int}}=\int\mathrm{d}^{4}x [V(ϕ+UV+ϕ+IR)V(ϕ+UV)V(ϕ+IR)\displaystyle\bigl{[}V(\phi^{\text{UV}}_{+}+\phi^{\text{IR}}_{+})-V(\phi^{\text{UV}}_{+})-V(\phi^{\text{IR}}_{+}) V(ϕUV+ϕIR)+V(ϕUV)+V(ϕIR)]ϕ±UV=ϕcUV±(ϕΔUV/2),ϕ±IR=ϕcIR±(ϕΔIR/2).\displaystyle-V(\phi^{\text{UV}}_{-}+\phi^{\text{IR}}_{-})+V(\phi^{\text{UV}}_{-})+V(\phi^{\text{IR}}_{-})\bigr{]}_{\phi^{\text{UV}}_{\pm}=\phi^{\text{UV}}_{c}\pm(\phi^{\text{UV}}_{\Delta}/2),\,\phi^{\text{IR}}_{\pm}=\phi^{\text{IR}}_{c}\pm(\phi^{\text{IR}}_{\Delta}/2)}\,. (98)

Str:=Tdtd3k(2π)3δ(ttk)[ϕΔIR(t,𝒌)ΠcUV(t,𝒌)ΠΔIR(𝒌,t)ϕcUV(t,𝒌)].\displaystyle S_{\text{tr}}:=\int^{T}_{-\infty}\mathrm{d}t\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\delta(t-t_{k})\left[\phi^{\text{IR}}_{\Delta}(t,-\bm{k})\Pi^{\text{UV}}_{c}(t,\bm{k})-\Pi^{\text{IR}}_{\Delta}(-\bm{k},t)\phi^{\text{UV}}_{c}(t,\bm{k})\right]\,. (99)

The bi-linear vertexes exist only at the UV\toIR transition time tkt_{k} for given modes with 0<kkc(T)0<k\leq k_{c}(T). Physically, these vertexes set the initial fluctuations for such modes in (96).

A.2.1 Integrate out short-wavelength modes

Now we calculate iΓi\Gamma perturbatively by specifying the setup more concretely. We organize the perturbation theory around the false vacuum state ρ0\rho_{0} for which the expectation value of the zero mode is ϕfalse\phi_{\text{false}}. We assume that the fluctuations of zero modes are tiny enough so that the couplings between zero-mode fluctuations and those of non-zero modes k>0k>0 are switched off in the past infinity t=t=-\infty. We then take the initial state of non-zero modes to be the Bunch-Davies vacuum state for a free field, where the time evolution of a free field is defined by the quadratic action expanded around the homogeneous background ϕfalse\phi_{\text{false}}. These assumptions can be implemented by writing the initial quantum state as

ρ0[ϕcUV,ϕΔUV;ϕcIR,ϕΔIR]=ρBD[ϕcUV,ϕΔUV;ϕfalse]ρ0[ϕcIRϕfalse,ϕΔIR]\rho_{0}[\phi^{\text{UV}}_{c},\phi^{\text{UV}}_{\Delta};\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta}]=\rho_{\text{BD}}[\phi^{\text{UV}}_{c},\phi^{\text{UV}}_{\Delta};\phi_{\text{false}}]\,\rho_{0}[\phi^{\text{IR}}_{c}-\phi_{\text{false}},\phi^{\text{IR}}_{\Delta}] (100)

which is properly normalized as

1\displaystyle 1 =k>0dϕcUV(,𝒌)dϕΔUV(,𝒌)ρBD[ϕcUV,ϕΔUV;ϕfalse]\displaystyle=\prod_{k>0}\int\mathrm{d}\phi^{\text{UV}}_{c}(-\infty,\bm{k})\int\mathrm{d}\phi^{\text{UV}}_{\Delta}(-\infty,\bm{k})\,\rho_{\text{BD}}[\phi^{\text{UV}}_{c},\phi^{\text{UV}}_{\Delta};\phi_{\text{false}}]
=dϕcIR(,𝟎)dϕΔIR(,𝟎)ρ0[ϕcIRϕfalse,ϕΔIR].\displaystyle=\int\mathrm{d}\phi^{\text{IR}}_{c}(-\infty,\bm{0})\int\mathrm{d}\phi^{\text{IR}}_{\Delta}(-\infty,\bm{0})\,\rho_{0}[\phi^{\text{IR}}_{c}-\phi_{\text{false}},\phi^{\text{IR}}_{\Delta}]\,. (101)

ρBD[ϕcUV,ϕΔUV;ϕfalse]\rho_{\text{BD}}[\phi^{\text{UV}}_{c},\phi^{\text{UV}}_{\Delta};\phi_{\text{false}}] is the density matrix for non-zero modes. An initial state for the zero mode is given by ρ0[ϕcIRϕfalse,ϕΔIR]\rho_{0}[\phi^{\text{IR}}_{c}-\phi_{\text{false}},\phi^{\text{IR}}_{\Delta}] for which we have

Ψ()|ϕ^(𝒌=𝟎)|Ψ()=dϕcIRρ0[ϕcIRϕfalse,ϕΔIR]ϕcIR=ϕfalse(2π)3δ(𝟎).\bra{\Psi(-\infty)}\hat{\phi}(\bm{k}=\bm{0})\ket{\Psi(-\infty)}=\int\mathrm{d}\phi^{\text{IR}}_{c}\rho_{0}[\phi^{\text{IR}}_{c}-\phi_{\text{false}},\phi^{\text{IR}}_{\Delta}]\phi^{\text{IR}}_{c}=\phi_{\text{false}}(2\pi)^{3}\delta(\bm{0})\,. (102)

Combining this with Ψ()|ϕ^(𝒌)|Ψ()=0\bra{\Psi(-\infty)}\hat{\phi}(\bm{k})\ket{\Psi(-\infty)}=0 for non-zero modes k>0k>0, we have

Ψ()|ϕ^(𝒌)|Ψ()=ϕfalse(2π)3δ(𝒌).\bra{\Psi(-\infty)}\hat{\phi}(\bm{k})\ket{\Psi(-\infty)}=\phi_{\text{false}}(2\pi)^{3}\delta(\bm{k})\,. (103)

Hence, the VEV of the IR field ϕ^IR(t,𝒙)\hat{\phi}^{\text{IR}}(t,\bm{x}) in the past infinity t=t=-\infty is given by ϕfalse\phi_{\text{false}}.

The interaction vertexes for calculating iΓi\Gamma are the bi-linear vertexes (99) and non-linear vertexes coming from interacting potential V(ϕ)V(\phi). We assume that the potential is sufficiently flat under the region we are interested in. It is then natural to separate iΓi\Gamma into the leading order pieces and higher-order terms in the coupling constant as follows,

eiΓ=ρ0[ϕcIRϕfalse,ϕΔIR]eiΓLOk>0eid4xδHhigher,\displaystyle e^{i\Gamma}=\rho_{0}[\phi^{\text{IR}}_{c}-\phi_{\text{false}},\phi^{\text{IR}}_{\Delta}]\,e^{i\Gamma_{\text{LO}}^{k>0}}e^{-i\int\mathrm{d}^{4}x\,\delta H_{\text{higher}}}\,,
eiΓLOk>0:=𝒟(ϕcUV,ϕΔUV,ΠcUV,ΠΔUV)eiSH,freeUV+Strk>0δ(ϕΔIR(tf(k),𝒌))ρBD[ϕcUV,ϕΔUV;ϕfalse].\displaystyle e^{i\Gamma^{k>0}_{\text{LO}}}:=\int\mathcal{D}(\phi^{\text{UV}}_{c},\phi^{\text{UV}}_{\Delta},\Pi^{\text{UV}}_{c},\Pi^{\text{UV}}_{\Delta})\,e^{iS^{\text{UV}}_{H,\text{free}}+S_{\text{tr}}}\prod_{k>0}\delta(\phi^{\text{IR}}_{\Delta}(t_{f}(k),\bm{k}))\rho_{\text{BD}}[\phi^{\text{UV}}_{c},\phi^{\text{UV}}_{\Delta};\phi_{\text{false}}]\,. (104)

Here, SH,freeUV[ϕcUV,ϕΔUV,ΠcUV,ΠΔUV;ϕfalse]S^{\text{UV}}_{H,\text{free}}[\phi^{\text{UV}}_{c},\phi^{\text{UV}}_{\Delta},\Pi^{\text{UV}}_{c},\Pi^{\text{UV}}_{\Delta};\phi_{\text{false}}] is the free part of the Hamiltonian action defined around the false vacuum as explained above. Higher-order corrections to Γ\Gamma in the coupling constant are represented by the term δHhigher\delta H_{\text{higher}} which can be evaluated perturbatively. We have δHhigher=0\delta H_{\text{higher}}=0 at the leading order.

To calculate iΓLOk>0i\Gamma^{k>0}_{\text{LO}} by writing down the connected diagrams with external IR fields, we only need to consider the bi-linear vertexes StrS_{\text{tr}} given in (99). The number of diagrams are only four, and iΓLOk>0i\Gamma_{\text{LO}}^{k>0} can be calculated as Tokuda:2017fdh ; Tokuda:2018eqs

iΓLOk>0\displaystyle i\Gamma_{\text{LO}}^{k>0} =12dtdtd3k(2π)3Xα(t,𝒌)gαβ(t,t,k)Xβ(t,𝒌)\displaystyle=\frac{-1}{2}\int\mathrm{d}t\int\mathrm{d}t^{\prime}\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\,X_{\alpha}(t,\bm{k})g^{\alpha\beta}(t,t^{\prime},k)X_{\beta}(t^{\prime},-\bm{k})
=12d4xd4xXα(x)Gαβ(x,x)Xβ(x).\displaystyle=\frac{-1}{2}\int\mathrm{d}^{4}x\int\mathrm{d}^{4}x^{\prime}\,X_{\alpha}(x)G^{\alpha\beta}(x,x^{\prime})X_{\beta}(x^{\prime})\,. (105)

Here, the Greek indices α,β=(ϕ,Π)\alpha,\beta=(\phi,\Pi) label the IR-Δ\Delta fields: (Xϕ,XΠ)=(ΠΔIR,ϕΔIR)(X_{\phi},X_{\Pi})=(\Pi^{\text{IR}}_{\Delta},-\phi^{\text{IR}}_{\Delta}). Substituting Eq.(104) into (96), we find

Z[JIR(T)]=\displaystyle Z[J^{\text{IR}}(T)]= 𝒟(ϕcIR,ϕΔIR,ΠcIR,ΠΔIR)ei𝑱IRϕcIRρ0[ϕcIRϕfalse,ϕΔIR]ei(SHIR+ΓLOk>0)eid4xδHhigher\displaystyle\int\mathcal{D}(\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{c},\Pi^{\text{IR}}_{\Delta})\,e^{i\bm{J}^{\text{IR}}\cdot\bm{\phi}^{\text{IR}}_{c}}\rho_{0}[\phi^{\text{IR}}_{c}-\phi_{\text{false}},\phi^{\text{IR}}_{\Delta}]\,e^{i(S_{H}^{\text{IR}}+\Gamma_{\text{LO}}^{k>0})}e^{-i\int\mathrm{d}^{4}x\,\delta H_{\text{higher}}}
×kkc(T)δ(ϕΔIR(T,𝒌))0<kkc(T)δ(ϕcIR(tk,𝒌)).\displaystyle\times\prod_{k\leq k_{c}(T)}\delta(\phi^{\text{IR}}_{\Delta}(T,\bm{k}))\prod_{0<k\leq k_{c}(T)}\delta(\phi^{\text{IR}}_{c}(t_{k},\bm{k}))\,. (106)

Now we introduce iΓk=0i\Gamma_{k=0} as

eiΓk=0[ϕΔIR,ΠΔIR]:=dϕcIRρ0[ϕcIRϕfalse,ϕΔIR]eiΠΔIR(ϕcIRϕfalse(2π)3δ(𝟎)).\displaystyle e^{i\Gamma_{k=0}[\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{\Delta}]}:=\int\mathrm{d}\phi^{\text{IR}}_{c}\rho_{0}[\phi^{\text{IR}}_{c}-\phi_{\text{false}},\phi^{\text{IR}}_{\Delta}]e^{-i\Pi^{\text{IR}}_{\Delta}(\phi^{\text{IR}}_{c}-\phi_{\text{false}}(2\pi)^{3}\delta(\bm{0}))}\,. (107)

By definition, we have

dϕcIRρ0[ϕcIRϕfalse,ϕΔIR]eiΠΔIR(ϕcIRϕfalse(2π)3δ(𝟎))\displaystyle\int\mathrm{d}\phi^{\text{IR}}_{c}\rho_{0}[\phi^{\text{IR}}_{c}-\phi_{\text{false}},\phi^{\text{IR}}_{\Delta}]\,e^{-i\Pi^{\text{IR}}_{\Delta}\left(\phi^{\text{IR}}_{c}-\phi_{\text{false}}(2\pi)^{3}\delta(\bm{0})\right)}
=dϕcIReiΠΔIRϕcIReiΓk=0[ϕΔIR,ΠΔIR]δ(ϕcIRϕfalse(2π)3δ(𝟎)).\displaystyle=\int\mathrm{d}\phi^{\text{IR}}_{c}\,e^{-i\Pi^{\text{IR}}_{\Delta}\phi^{\text{IR}}_{c}}e^{i\Gamma_{k=0}[\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{\Delta}]}\delta\left(\phi^{\text{IR}}_{c}-\phi_{\text{false}}(2\pi)^{3}\delta(\bm{0})\right)\,. (108)

Substituting (108) into (106), we find

Z[JIR(T)]=\displaystyle Z[J^{\text{IR}}(T)]= 𝒟(ϕcIR,ϕΔIR,ΠcIR,ΠΔIR)ei𝑱IRϕcIRei(SHIR+ΓLOk>0+Γk=0)eid4xδHhigher\displaystyle\int\mathcal{D}(\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{c},\Pi^{\text{IR}}_{\Delta})\,e^{i\bm{J}^{\text{IR}}\cdot\bm{\phi}^{\text{IR}}_{c}}\,e^{i(S_{H}^{\text{IR}}+\Gamma_{\text{LO}}^{k>0}+\Gamma_{k=0})}e^{-i\int\mathrm{d}^{4}x\,\delta H_{\text{higher}}}
×kkc(T)δ(ϕΔIR(T,𝒌))δ(ϕcIR(tk,𝒌)ϕfalse(2π)3δ(𝒌)),\displaystyle\times\prod_{k\leq k_{c}(T)}\delta(\phi^{\text{IR}}_{\Delta}(T,\bm{k}))\delta(\phi^{\text{IR}}_{c}(t_{k},\bm{k})-\phi_{\text{false}}(2\pi)^{3}\delta(\bm{k}))\,, (109)

with defining tk|k=0=t_{k}|_{k=0}=-\infty.

A.2.2 Long-wavelength sector

For later convenience, let us focus on the term dtΠcIR(t,𝒌)ϕ˙ΔIR(t,𝒌)\int\mathrm{d}t\,\Pi^{\text{IR}}_{c}(t,\bm{k})\dot{\phi}^{\text{IR}}_{\Delta}(t,-\bm{k}) in SHIRS_{H}^{\text{IR}}. We use the following trick to perform the integration by parts:

δ(ϕΔIR(T,𝒌))eitkTdtΠcIR(t,𝒌)ϕ˙ΔIR(t,𝒌)\displaystyle\delta(\phi^{\text{IR}}_{\Delta}(T,\bm{k}))\,e^{i\int^{T}_{t_{k}}\mathrm{d}t\,\Pi^{\text{IR}}_{c}(t,\bm{k})\dot{\phi}^{\text{IR}}_{\Delta}(t,-\bm{k})}
=δ(ϕΔIR(T,𝒌))dΠcIR(tk0+,𝒌)eitk0+TdtΠcIR(t,𝒌)ϕ˙ΔIR(t,𝒌)δ(ΠcIR(tk0+,𝒌))\displaystyle=\delta(\phi^{\text{IR}}_{\Delta}(T,\bm{k}))\int\mathrm{d}\Pi^{\text{IR}}_{c}(t_{k}-0^{+},\bm{k})\,e^{i\int^{T}_{t_{k}-0^{+}}\mathrm{d}t\,\Pi^{\text{IR}}_{c}(t,\bm{k})\dot{\phi}^{\text{IR}}_{\Delta}(t,-\bm{k})}\delta(\Pi^{\text{IR}}_{c}(t_{k}-0^{+},\bm{k}))
=δ(ϕΔIR(T,𝒌))dΠcIR(tk0+,𝒌)eitk0+TdtΠ˙cIR(t,𝒌)ϕΔIR(t,𝒌)δ(ΠcIR(tk0+,𝒌)).\displaystyle=\delta(\phi^{\text{IR}}_{\Delta}(T,\bm{k}))\int\mathrm{d}\Pi^{\text{IR}}_{c}(t_{k}-0^{+},\bm{k})\,e^{-i\int^{T}_{t_{k}-0^{+}}\mathrm{d}t\,\dot{\Pi}^{\text{IR}}_{c}(t,\bm{k})\phi^{\text{IR}}_{\Delta}(t,-\bm{k})}\delta(\Pi^{\text{IR}}_{c}(t_{k}-0^{+},\bm{k}))\,. (110)

Thanks to this trick, (109) can be written as

Z[JIR(T)]\displaystyle Z[J^{\text{IR}}(T)] =𝒟(ϕcIR,ϕΔIR,ΠcIR,ΠΔIR)𝒟~ΠcIRei𝑱IRϕcIRei(SH,(d)IR+SH,(s)IR+ΓLOk>0+Γk=0)eid4xδHhigher\displaystyle=\int\mathcal{D}(\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{c},\Pi^{\text{IR}}_{\Delta})\int\widetilde{\mathcal{D}}\Pi^{\text{IR}}_{c}\,e^{i\bm{J}^{\text{IR}}\cdot\bm{\phi}^{\text{IR}}_{c}}\,e^{i(S_{H,(d)}^{\text{IR}}+S_{H,(s)}^{\text{IR}}+\Gamma_{\text{LO}}^{k>0}+\Gamma_{k=0})}e^{-i\int\mathrm{d}^{4}x\,\delta H_{\text{higher}}}
×kkc(T)δ(ϕΔIR(T,𝒌))δ(ϕcIR(tk,𝒌)ϕfalse(2π)3δ(𝒌))δ(ΠcIR(tk0+,𝒌)),\displaystyle\quad\times\prod_{k\leq k_{c}(T)}\delta(\phi^{\text{IR}}_{\Delta}(T,\bm{k}))\delta(\phi^{\text{IR}}_{c}(t_{k},\bm{k})-\phi_{\text{false}}(2\pi)^{3}\delta(\bm{k}))\delta(\Pi^{\text{IR}}_{c}(t_{k}-0^{+},\bm{k}))\,, (111)

where, 𝒟~ΠcIR:=kkc(T)dΠcIR(tk0+,𝒌)\displaystyle\widetilde{\mathcal{D}}\Pi_{c}^{\text{IR}}:=\prod_{k\leq k_{c}(T)}\mathrm{d}\Pi^{\text{IR}}_{c}(t_{k}-0^{+},\bm{k}). Below, we simply omit this integration measure just for simplifying the notation. We also decomposed SHIRS_{H}^{\text{IR}} as SHIR=SH,(d)IR+SH,(s)IRS_{H}^{\text{IR}}=S_{H,(d)}^{\text{IR}}+S_{H,(s)}^{\text{IR}} up to boundary terms which vanish thanks to the trick (110) as

SH,(d)IR\displaystyle S^{\text{IR}}_{H,(d)} =d4x[ΠΔIR(ϕ˙cIRa3ΠcIR)ϕΔIR(Π˙cIRa(t)2ϕcIR+a3(t)V(ϕcIR))],\displaystyle=\int\mathrm{d}^{4}x\,\left[\Pi^{\text{IR}}_{\Delta}\left(\dot{\phi}^{\text{IR}}_{c}-a^{-3}\Pi^{\text{IR}}_{c}\right)-\phi^{\text{IR}}_{\Delta}\left(\dot{\Pi}^{\text{IR}}_{c}-a(t)\nabla^{2}\phi^{\text{IR}}_{c}+a^{3}(t)\,V^{\prime}(\phi^{\text{IR}}_{c})\right)\right]\,, (112)
SH,(s)IR\displaystyle S^{\text{IR}}_{H,(s)} =d4xa3(t)[V(ϕcIR+(ϕΔIR/2))V(ϕcIR(ϕΔIR/2))V(ϕcIR)ϕΔIR].\displaystyle=-\int\mathrm{d}^{4}x\,a^{3}(t)\,\left[V(\phi^{\text{IR}}_{c}+(\phi^{\text{IR}}_{\Delta}/2))-V(\phi^{\text{IR}}_{c}-(\phi^{\text{IR}}_{\Delta}/2))-V^{\prime}(\phi^{\text{IR}}_{c})\phi^{\text{IR}}_{\Delta}\right]\,. (113)

Here, the space-time argument of IR variables are omitted. We introduced the IR variables and their time derivatives as

XIR(t,𝒙):=d3k(2π)3θ(kc(t)k)XIR(t,𝒌)ei𝒌.𝒙,\displaystyle X^{\text{IR}}(t,\bm{x}):=\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\,\theta(k_{c}(t)-k)\,X^{\text{IR}}(t,\bm{k})\,e^{i\bm{k}.\bm{x}}\,, (114)
X˙IR(t,𝒙):=d3k(2π)3θ(kc(t)k)X˙IR(t,𝒌)ei𝒌.𝒙,\displaystyle\dot{X}^{\text{IR}}(t,\bm{x}):=\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\,\theta(k_{c}(t)-k)\,\dot{X}^{\text{IR}}(t,\bm{k})\,e^{i\bm{k}.\bm{x}}\,, (115)

where XIRX^{\text{IR}} represents the IR variables: XIR=(ϕcIR,ϕΔIR,ΠcIR,ΠΔIR)X^{\text{IR}}=(\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{c},\Pi^{\text{IR}}_{\Delta}). Precisely speaking, for XIR=ΠcIRX^{\text{IR}}=\Pi^{\text{IR}}_{c}, we should replace kc(t)k_{c}(t) by kc(t+0+)k_{c}(t+0^{+}) so that we have kc(t)=kk_{c}(t)=k at t=tk0+t=t_{k}-0^{+}. One may concern about the subtlety of the time derivatives ϕ˙cIR(t,𝒙)\dot{\phi}^{\text{IR}}_{c}(t,\bm{x}) and Π˙cIR(t,𝒙)\dot{\Pi}^{\text{IR}}_{c}(t,\bm{x}) in (112): We in general have X˙IR(t,𝒙)t(XIR(t,𝒙))\dot{X}^{\text{IR}}(t,\bm{x})\neq\frac{\partial}{\partial t}(X^{\text{IR}}(t,\bm{x})), where the LHS is defined by (115), due to the presence of time-dependent step function. However, there is no subtlety thanks to the initial conditions for all IR modes kkc(T)k\leq k_{c}(T) of the form

ϕcIR(tk,𝒌)=ϕfalse(2π)3δ(𝒌),ΠcIR(tk0+,𝒌)=0,\displaystyle\phi^{\text{IR}}_{c}(t_{k},\bm{k})=\phi_{\text{false}}(2\pi)^{3}\delta(\bm{k})\,,\qquad\Pi^{\text{IR}}_{c}(t_{k}-0^{+},\bm{k})=0\,, (116)

which are imposed by the delta functions in the final line in (111). The corresponding conditions in the real space for all 𝒙\bm{x} are

X˙IR(t,𝒙)=t(XIR(t,𝒙))forXIR=(ϕcIR,ΠcIR),\displaystyle\dot{X}^{\text{IR}}(t,\bm{x})=\partial_{t}(X^{\text{IR}}(t,\bm{x}))\quad\text{for}\quad X^{\text{IR}}=(\phi^{\text{IR}}_{c},\,\Pi^{\text{IR}}_{c})\,, (117a)
ϕcIR(,𝒙)=ϕfalse,ΠcIR(,𝒙)=0.\displaystyle\phi^{\text{IR}}_{c}(-\infty,\bm{x})=\phi_{\text{false}}\,,\quad\Pi^{\text{IR}}_{c}(-\infty,\bm{x})=0\,. (117b)

To implement these conditions in the path integral, we define δ[𝒞ini]\delta\left[\mathcal{C}_{\text{ini}}\right] by (40b) with

δ[𝒞detail]:=tTXIR=(ϕcIR,ΠcIR)𝒙δ(X˙IR(t,𝒙)t(XIR(t,𝒙))).\delta\left[\mathcal{C}_{\text{detail}}\right]:=\prod_{-\infty\leq t\leq T}\prod_{X^{\text{IR}}=(\phi^{\text{IR}}_{c},\Pi^{\text{IR}}_{c})}\prod_{\bm{x}}\delta\left(\dot{X}^{\text{IR}}(t,\bm{x})-\partial_{t}(X^{\text{IR}}(t,\bm{x}))\right)\,. (118)

We find from eqs. (37) and (111) that the transition probability can be written in terms of path integral as

p({ϕIR(T,𝒙)}T,𝒙𝒟)=\displaystyle p(\{\phi^{\text{IR}}(T,\bm{x})\}_{T,\bm{x}\in\mathcal{D}})= 𝒟(ϕcIR,ϕΔIR,ΠcIR,ΠΔIR)ei𝒮eiΓk=0δ[𝒞fin]δ[𝒞ini],\displaystyle\int\mathcal{D}(\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{c},\Pi^{\text{IR}}_{\Delta})\,\,e^{i\mathcal{S}}e^{i\Gamma_{k=0}}\delta\left[\mathcal{C}_{\text{fin}}\right]\delta\left[\mathcal{C}_{\text{ini}}\right]\,, (119)

where δ[𝒞fin]\delta\left[\mathcal{C}_{\text{fin}}\right] is defined in (40a), and the term 𝒮\mathcal{S} in the exponent is given by

𝒮=(SH,(d)IR+SH,(s)IR+ΓLOk>0)d4xδHhigher\mathcal{S}=(S_{H,(d)}^{\text{IR}}+S_{H,(s)}^{\text{IR}}+\Gamma_{\text{LO}}^{k>0})-\int\mathrm{d}^{4}x\,\delta H_{\text{higher}} (120)

which agrees with the definition of 𝒮\mathcal{S} given in (41). When fluctuations of zero mode are negligible, we can set Γk=0=0\Gamma_{k=0}=0. This is the setup adopted in the main text. Then, (119) coincides with (39).

A.3 Stochastic interpretation of the tunneling

It is useful to see how the stochastic equations emerge as a consequence of performing the path integral over IR variables non-perturbatively. This leads to the stochastic interpretation of the tunneling probability. A final result of this section is (130).

For simplicity, let us ignore higher-order corrections δHhigher\delta H_{\text{higher}} for a while. We start with introducing the auxiliary fields (ξϕ,ξΠ)(\xi_{\phi},\xi_{\Pi}) as

ei(ΓLOk>0+Γk=0+SH,(s)IR)=𝒟(ξϕ,ξΠ)P[ξϕ,ξΠ]eid4x(ξΠ(x)ϕΔIR(x)ξϕ(x)ΠΔIR(x)).\displaystyle e^{i\left(\Gamma^{k>0}_{\text{LO}}+\Gamma_{k=0}+S^{\text{IR}}_{H,(s)}\right)}=\int\mathcal{D}(\xi_{\phi},\xi_{\Pi})\,P[\xi_{\phi},\xi_{\Pi}]e^{i\int\mathrm{d}^{4}x\left(\xi_{\Pi}(x)\phi^{\text{IR}}_{\Delta}(x)-\xi_{\phi}(x)\Pi^{\text{IR}}_{\Delta}(x)\right)}\,. (121)

We substitute (121) into (111). Then the exponent becomes linear in ϕΔIR(t,𝒌)\phi^{\text{IR}}_{\Delta}(t,\bm{k}) or ΠΔIR(t,𝒌)\Pi^{\text{IR}}_{\Delta}(t,\bm{k}) with t0t<Tt_{0}\leq t<T:

Z[JIR(T)]\displaystyle Z[J^{\text{IR}}(T)] 𝒟(ϕcIR,ϕΔIR,ΠcIR,ΠΔIR)𝒟~ΠcIRei𝑱IRϕcIR𝒟(ξϕ,ξΠ)P[ξϕ,ξΠ]\displaystyle\simeq\int\mathcal{D}(\phi^{\text{IR}}_{c},\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{c},\Pi^{\text{IR}}_{\Delta})\int\widetilde{\mathcal{D}}\Pi^{\text{IR}}_{c}\,e^{i\bm{J}^{\text{IR}}\cdot\bm{\phi}^{\text{IR}}_{c}}\int\mathcal{D}(\xi_{\phi},\xi_{\Pi})\,P[\xi_{\phi},\xi_{\Pi}]
×exp{iTdtd3k(2π)3[ΠΔIR(t,𝒌)ϕ(t,𝒌)ϕΔIR(t,𝒌)Π(t,𝒌)]Θ(kc(t)k)}\displaystyle\times\exp\left\{i\int^{T}_{-\infty}\mathrm{d}t\int\frac{\mathrm{d}^{3}k}{(2\pi)^{3}}\,\left[\Pi^{\text{IR}}_{\Delta}(t,-\bm{k})\mathcal{L}_{\phi}(t,\bm{k})-\phi^{\text{IR}}_{\Delta}(t,-\bm{k})\mathcal{L}_{\Pi}(t,\bm{k})\right]\Theta(k_{c}(t)-k)\right\}
×kkc(T)δ(ϕΔIR(T,𝒌))δ(ϕcIR(tk,𝒌)ϕfalse(2π)3δ(𝒌))δ(ΠcIR(tk0+,𝒌)),\displaystyle\times\prod_{k\leq k_{c}(T)}\delta(\phi^{\text{IR}}_{\Delta}(T,\bm{k}))\delta(\phi^{\text{IR}}_{c}(t_{k},\bm{k})-\phi_{\text{false}}(2\pi)^{3}\delta(\bm{k}))\delta(\Pi^{\text{IR}}_{c}(t_{k}-0^{+},\bm{k}))\,, (122)

where

ϕ(t,𝒌):=ϕ˙cIR(t,𝒌)a3(t)ΠcIR(t,𝒌)ξϕ(t,𝒌),\displaystyle\mathcal{L}_{\phi}(t,\bm{k}):=\dot{\phi}^{\text{IR}}_{c}(t,\bm{k})-a^{-3}(t)\Pi^{\text{IR}}_{c}(t,\bm{k})-\xi_{\phi}(t,\bm{k})\,, (123a)
π(t,𝒌):=Π˙cIR(t,𝒌)+a(t)k2ϕcIR(t,𝒌)+a3(t)V(ϕcIR)(t,𝒌)ξΠ(t,𝒌).\displaystyle\mathcal{L}_{\pi}(t,\bm{k}):=\dot{\Pi}^{\text{IR}}_{c}(t,\bm{k})+a(t)k^{2}\phi^{\text{IR}}_{c}(t,\bm{k})+a^{3}(t)\,V^{\prime}(\phi^{\text{IR}}_{c})(t,\bm{k})-\xi_{\Pi}(t,\bm{k})\,. (123b)

Consequently, we can perform the path integral 𝒟(ϕΔIR,ΠΔIR)\int\mathcal{D}(\phi^{\text{IR}}_{\Delta},\Pi^{\text{IR}}_{\Delta}), leading to

Z[JIR(T)]kkc(T)dϕcIR(T,𝒌)ei𝑱IRϕcIR𝒟(ξϕ,ξΠ)P[ξϕ,ξΠ]|ϕ=Π=0 & (116).\displaystyle Z[J^{\text{IR}}(T)]\simeq\prod_{k\leq k_{c}(T)}\left.\int\mathrm{d}\phi^{\text{IR}}_{c}(T,\bm{k})\,e^{i\bm{J}^{\text{IR}}\cdot\bm{\phi}^{\text{IR}}_{c}}\int\mathcal{D}(\xi_{\phi},\xi_{\Pi})\,P[\xi_{\phi},\xi_{\Pi}]\right|_{\text{$\mathcal{L}_{\phi}=\mathcal{L}_{\Pi}=0$ \& \eqref{initial}}}\,. (124)

Now we regard auxiliary fields (ξϕ,ξΠ)(\xi_{\phi},\xi_{\Pi}) as noise variables whose correlations are given by

ξα(t,𝒌)ξβ(t,𝒌)\displaystyle\langle\xi_{\alpha}(t,\bm{k})\xi_{\beta}(t^{\prime},\bm{k}^{\prime})\rangle :=𝒟(ξϕ,ξΠ)P[ξϕ,ξΠ]ξα(t,𝒌)ξβ(t,𝒌)\displaystyle:=\int\mathcal{D}(\xi_{\phi},\xi_{\Pi})\,P[\xi_{\phi},\xi_{\Pi}]\,\xi_{\alpha}(t,\bm{k})\xi_{\beta}(t^{\prime},\bm{k}^{\prime})
=[iδδXα(t,𝒌)iδδXβ(t,𝒌)]ei(ΓLOk>0+Γk=0+SH,(s)IR)|ϕΔIR=ΠΔIR=0,\displaystyle=\left.\left[\frac{i\delta}{\delta X_{\alpha}(t,\bm{k})}\frac{i\delta}{\delta X_{\beta}(t^{\prime},\bm{k}^{\prime})}\right]e^{i\left(\Gamma^{k>0}_{\text{LO}}+\Gamma_{k=0}+S^{\text{IR}}_{H,(s)}\right)}\right|_{\phi^{\text{IR}}_{\Delta}=\Pi^{\text{IR}}_{\Delta}=0}\,, (125)

where α,β=(ϕ,Π)\alpha,\beta=(\phi,\Pi) and (Xϕ,XΠ)=(ΠΔIR,ϕΔIR)(X_{\phi},X_{\Pi})=(\Pi^{\text{IR}}_{\Delta},-\phi^{\text{IR}}_{\Delta}) following the notation in (105). We also have the corresponding expression in the momentum space. If we ignore SH,(s)S_{H,(s)} and iΓk=0i\Gamma_{k=0}, we have

ξα(t,𝒌)ξβ(t,𝒌)=(2π)3δ(𝒌+𝒌)Re[gαβ(t)]δ(tt)δ(ttk).\langle\xi_{\alpha}(t,\bm{k})\xi_{\beta}(t^{\prime},\bm{k}^{\prime})\rangle=(2\pi)^{3}\delta\left(\bm{k}+\bm{k}^{\prime}\right)\text{Re}\left[g^{\alpha\beta}(t)\right]\delta(t-t^{\prime})\delta(t-t_{k})\,. (126)

Eq.(124) shows that the effective dynamics of IR fields are described by the set of Langevin equations ϕ=Π=0\mathcal{L}_{\phi}=\mathcal{L}_{\Pi}=0 with the initial condition (116) and the noise correlations (126).

In the real space, the dynamics is described by the set of Langevin equations,

ϕ˙cIR(x)=a3(t)ΠcIR(x)+ξϕ(x),\displaystyle\dot{\phi}^{\text{IR}}_{c}(x)=a^{-3}(t)\Pi^{\text{IR}}_{c}(x)+\xi_{\phi}(x)\,, (127a)
Π˙cIR(x)=a(t)2ϕcIR(x)a3V(ϕcIR(x))+ξΠ(x),\displaystyle\dot{\Pi}^{\text{IR}}_{c}(x)=a(t)\nabla^{2}\phi^{\text{IR}}_{c}(x)-a^{3}V^{\prime}(\phi^{\text{IR}}_{c}(x))+\xi_{\Pi}(x)\,, (127b)

with the initial conditions (117) and the noise correlations

ξα(x)ξβ(y)=Gαβ(x,y).\langle\xi_{\alpha}(x)\xi_{\beta}(y)\rangle=G^{\alpha\beta}(x,y)\,. (128)

Eq.(124) takes the following form in the real space:

Z[JIR(T)]𝒙dϕcIR(T,𝒙)ei𝑱IRϕcIR𝒟(ξϕ,ξΠ)P[ξϕ,ξΠ]|(117) & (127).\displaystyle Z[J^{\text{IR}}(T)]\simeq\prod_{\bm{x}}\left.\int\mathrm{d}\phi^{\text{IR}}_{c}(T,\bm{x})\,e^{i\bm{J}^{\text{IR}}\cdot\bm{\phi}^{\text{IR}}_{c}}\int\mathcal{D}(\xi_{\phi},\xi_{\Pi})\,P[\xi_{\phi},\xi_{\Pi}]\right|_{\text{\eqref{initial_real} \& \eqref{langevin_real1}}}\,. (129)

Substituting (129) into (37), we have

p({ϕIR(T,𝒙)}T,𝒙𝒟)\displaystyle p(\{\phi^{\text{IR}}(T,\bm{x})\}_{T,\bm{x}\in\mathcal{D}})\simeq 𝒚dϕcIR(T,𝒚)𝒙𝒟δ(ϕcIR(T,𝒙)ϕIR(T,𝒙))\displaystyle\prod_{\bm{y}}\int\mathrm{d}\phi^{\text{IR}}_{c}(T,\bm{y})\,\prod_{\bm{x}\in\mathcal{D}}\delta(\phi^{\text{IR}}_{c}(T,\bm{x})-\phi^{\text{IR}}(T,\bm{x}))
×𝒟(ξϕ,ξΠ)P[ξϕ,ξΠ]|(117) & (127).\displaystyle\quad\times\left.\int\mathcal{D}(\xi_{\phi},\xi_{\Pi})\,P[\xi_{\phi},\xi_{\Pi}]\right|_{\text{\eqref{initial_real} \& \eqref{langevin_real1}}}\,. (130)

This expression provides a stochastic interpretation of the transition probability; the dynamics of ϕcIR\phi^{\text{IR}}_{c} is described by the set of Langevin equations and the transition probability is simply understood as the probability to realize the field configuration ϕcIR(T,𝒙)=ϕIR(T,𝒙)\phi^{\text{IR}}_{c}(T,\bm{x})=\phi^{\text{IR}}(T,\bm{x}) in the domain 𝒙𝒟\bm{x}\in\mathcal{D} at the final time TT starting from the initial configuration ϕcIR(,𝒙)=ϕfalse\phi^{\text{IR}}_{c}(-\infty,\bm{x})=\phi_{\text{false}}. In particular, the set of Langevin equations is given by (8) with the noise correlations (15) when we ignore the terms δHhigher\delta H_{\text{higher}}, SH,(s)IRS_{H,(s)}^{\text{IR}}, and Γk=0\Gamma_{k=0}. Note that such terms simply correct the Langevin equations141414For instance, leading-order corrections to the stochastic dynamics at the super-horizon scales are calculated in Tokuda:2017fdh . and do not invalidate the above stochastic interpretation.

Appendix B Coleman - de Luccia tunneling in Euclidean method

In this appendix, we provide the CDL action in de Sitter background with Euclidean method.

Generally, the ways of Euclideanization for de Sitter spacetime depend on the coordinates. In this paper, we discuss the field theory on the metric (1), and then we choose the following coordinate again 151515The analytic continuations of this coordinate is examined in Rubakov:1999ir .

ds2=1H2η2(dη2+d𝒙2).\displaystyle\mathrm{d}s^{2}=\frac{1}{H^{2}\eta^{2}}(-\mathrm{d}\eta^{2}+\mathrm{d}\bm{x}^{2}). (131)

By taking the wick rotation as ηiτ\eta\to-i\tau, the coordinate becomes

ds2=1H2τ2(dτ2+d𝒙2).\displaystyle-\mathrm{d}s^{2}=\frac{1}{H^{2}\tau^{2}}(\mathrm{d}\tau^{2}+\mathrm{d}\bm{x}^{2}). (132)

This is the Euclidean AdS space discussed in section 5 and we can take the global coordinate;

ds2=H2(dρ2+sinh2ρdΩ2).\displaystyle-\mathrm{d}s^{2}=H^{-2}(\mathrm{d}\rho^{2}+\sinh^{2}\rho\mathrm{d}\Omega^{2}). (133)

We also impose that the field ϕ\phi only depends on ρ\rho. Therefore, the Euclidean action IEI^{E} and the equation of motion becomes

IE=2π20dρsinh3ρ[12H2(ρϕ)2+V(ϕ)H4],\displaystyle I^{E}=2\pi^{2}\int_{0}^{\infty}\mathrm{d}\rho\sinh^{3}\rho\bigg{[}\frac{1}{2H^{2}}(\partial_{\rho}\phi)^{2}+\frac{V(\phi)}{H^{4}}\bigg{]}, (134)
d2ϕdρ2+3tanhρdϕdρ=V(ϕ)H2.\displaystyle\frac{\mathrm{d}^{2}\phi}{\mathrm{d}\rho^{2}}+\frac{3}{\tanh\rho}\frac{\mathrm{d}\phi}{\mathrm{d}\rho}=\frac{V^{\prime}(\phi)}{H^{2}}. (135)

The second equation is the same as (83) and we can obtain the same bounce solutions discussed in section 5. For numerical calculations, we consider the potential (42) and fitting function (85). Also we take the following non-dimensionalizations;

ϕ\displaystyle\phi =αϕ~,\displaystyle=\alpha\tilde{\phi}, (136)
V(ϕ)\displaystyle V(\phi) =g2α4V~(ϕ~).\displaystyle=g^{2}\alpha^{4}\tilde{V}(\tilde{\phi}). (137)

Therefore, the Euclidean action (134) becomes

IE\displaystyle I^{E} =2π2α2H20dρsinh3ρ[12(ρϕ~)2+g2α2H2V~(ϕ~)]\displaystyle=2\pi^{2}\frac{\alpha^{2}}{H^{2}}\int_{0}^{\infty}\mathrm{d}\rho\sinh^{3}\rho\bigg{[}\frac{1}{2}(\partial_{\rho}\tilde{\phi})^{2}+\frac{g^{2}\alpha^{2}}{H^{2}}\tilde{V}(\tilde{\phi})\bigg{]}
:=2π2α2H2I~E.\displaystyle:=2\pi^{2}\frac{\alpha^{2}}{H^{2}}\tilde{I}^{E}. (138)

The ratio of the Coleman-de Luccia Euclidean action IbounceEI^{E}_{\text{bounce}} to the Hawking-Moss action IHMI_{\text{HM}} is given as

γE=IbounceEIHM=H2g2α29I~bounceE(1β)3(β+3).\displaystyle\gamma_{E}=\frac{I^{E}_{\text{bounce}}}{I_{\text{HM}}}=\frac{H^{2}}{g^{2}\alpha^{2}}\frac{9\tilde{I}^{E}_{\text{bounce}}}{(1-\beta)^{3}(\beta+3)}. (139)

References