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Barrow Entropy Cosmology: an observational approach with a hint of stability analysis

Genly Leon1    Juan Magaña2    A. Hernández-Almada3    Miguel A. García-Aspeitia4,5    Tomás Verdugo6    V. Motta7
Abstract

In this work, we use an observational approach and dynamical system analysis to study the cosmological model recently proposed by Saridakis (2020), which is based on the modification of the entropy-area black hole relation proposed by Barrow (2020). The Friedmann equations governing the dynamics of the Universe under this entropy modification can be calculated through the gravity-thermodynamics conjecture. We investigate two models, one considering only a matter component and the other including matter and radiation, which have new terms compared to the standard model sourcing the late cosmic acceleration. A Bayesian analysis is performed in which we use five cosmological observations (observational Hubble data, type Ia supernovae, HII galaxies, strong lensing systems, and baryon acoustic oscillations) to constrain the free parameters of both models. From a joint analysis, we obtain constraints that are consistent with the standard cosmological paradigm within 2σ2\sigma confidence level. In addition, a complementary dynamical system analysis using local and global variables is developed which allows obtaining a qualitative description of the cosmology. As expected, we found that the dynamical equations have a de Sitter solution at late times.

1 Introduction

In the last decades, one of the puzzles in Cosmology is the source of the accelerated expansion of the Universe at late times. The first observational evidence of such expansion comes from the high redshift type Ia supernovae (SNIa) [1], confirmed by the acoustic peaks of the Cosmic Microwave Background Radiation (CMB) [2], and recently tested with large scale structure measurements [3]. The evidence point out to the existence of a dark entity whose gravitational influence should be repulsive, being known in the community with the name of dark energy (DE). The first approach, and the most successful DE candidate to explain the Universe acceleration is the cosmological constant (CC) [4], whose introduction in the dynamical equations is simple and in agreement with the different cosmological data and can be deduced mathematically from the Lovelock theorem [5]. Despite that CC is a successful model, understanding its nature eludes us. Our best theoretical models break down under the assumption that it comes from quantum vacuum fluctuations, obtaining results that are in total disagreement with our observations (see for example [6, 7]). In this vein that we have been forced to propose other alternatives to explain the Universe acceleration, which is the reason behind the expression ’dark energy’. Another path to address the cosmic acceleration problem is modifying the General Theory of Relativity (GR) by assuming the DE is caused by either some geometrical effect (see the following compilation of models [8, 9, 10, 11, 12]) or a fluid with strange characteristics, such as the Equation of State (EoS) taking the form ω<1/3\omega<-1/3, which is nonstandard for baryonic matter or even for dark matter (DM) (see also the models [13, 14, 15]).

An interesting alternative to tackle the problem of the cosmic acceleration, comes from the seminal ideas on black hole physics by Hawking and Bekenstein [16], and hereafter applied to the cosmological context (see for instance [17, 18]). The formalism, known as gravity-thermodynamics [18], consist on deriving the Einstein equations from a thermodynamic approach by using the proportionality of entropy and horizon area, and the assumption of local equilibrium conditions. In a recent study inspired by the geometrical structure of the COVID-19 virus, [19] propose that the expected black hole surface can be increased at the quantum gravitational level if it has such an intricate structure that could cut-off down to small scale (for instance the Planck length). In this context, Barrow constructs a fractal horizon surface by increasing the black hole area (AA), hence modifying its entropy as SBAf(Δ)S_{B}\sim A^{f(\Delta)}, being Δ\Delta a constant exponent. By using the gravity-thermodynamics approach, [20] calculated the equations governing the cosmological evolution assuming the Barrow entropy SBS_{B}. The modified Friedmann equation contains extra terms encoded as an effective dark energy, which drives the late cosmic acceleration. An interesting feature of this scenario is that, although the effective dark energy can behave as quintessence-like or phantom-like at different epochs, the Universe dynamics converges to de Sitter solution at larger times. By applying the Holographic principle, [21] calculated the equation governing the cosmological dynamics under the assumption that holographic dark energy obey the Barrow entropy, showing that it can source the cosmic accelerated expansion. Ref. [22] provide observational constraints on the Barrow holographic dark energy using SNIa and measurements of the Hubble data. Later on, [23] investigate the evolution of an interacting holographic dark energy model component under the Barrow’s modified entropy. Recently, [24] showed that a non-flat Barrow interacting holographic dark energy can reproduce the thermal history of the Universe. In addition, the authors claim that an open Universe favors an phantom regime for the effective dark energy equation of state.

Our aim is to revisit the framework of the Barrow cosmological model proposed by [20] to investigate the viability of such scenario to explain the late cosmic acceleration without a dark energy fluid. We constrain this model with several cosmological data at different scales: observational Hubble data, type Ia supernovae, HII galaxies, strong lensing systems, and baryonic acoustic oscillations. We also perform a dynamical analysis of the system equations to identify and classify the critical points and their stability, considering that the Universe is composed just by dust matter and filled with matter and radiation.

The paper is organized as follow: Sec. 2 presents the theoretical framework for the Barrow background cosmology. In Section 3 we perform a Bayesian analysis to constrain the free parameters of the model using observational Hubble data, type Ia supernovae, HII galaxies, strong lensing systems and baryon acoustic oscillations. In Sec. 4 we perform the dynamical analysis and stability of the system around the critical points. Finally, we discuss and present a summary of our results in Sec.5. In what follows we use units in which =kB=c=1\hbar=k_{B}=c=1.

2 Cosmology with Barrow Entropy

The equations that govern the dynamics of the Universe can be obtained from the gravity-thermodynamics conjecture, particularly, the Friedmann equations are retrieved by applying the first law of thermodynamics (dE=TdS-dE=T\,dS) to the apparent horizon of a Friedmann-Lemaitre-Robertson-Walker (FLRW) universe [18]. Analogously to black holes whose temperature and entropy are related to its horizon area AA, one can assume that this principle holds for the apparent cosmological horizon, rAr_{A}, i.e. it has an associated temperature TT and entropy SS in the form T=1/2πrAT=1/2\pi r_{A} and S=A/4GS=A/4G, where GG is the Newton constant. The heat flow (energy flux) δQ\delta Q through the horizon is given by

δQ=dE=A(ρf+pf)HrAdt,\delta Q=-dE=A\left(\rho_{f}+p_{f}\right)\,H\,r_{A}dt, (2.1)

being ρf\rho_{f} and pfp_{f} the energy density and pressure of the fluid respectively, and the Hubble parameter at scale factor aa is defined as H=a˙/aH=\dot{a}/a . The radius of the apparent cosmological horizon rAr_{A} is defined as

rA=(H2+ka2)1/2,r_{A}=\left(H^{2}+\frac{k}{a^{2}}\right)^{-1/2}, (2.2)

where kk is the spatial Universe curvature.

Recently, [19] propose an interesting modification to the entropy-area black hole relation by considering that the black hole horizon surface has a fractal structure. If the surface varies proportional to the radius as r2+Δ\propto r^{2+\Delta}, it modifies its entropy as

SB=(AA0)1+Δ2S_{B}=\left(\frac{A}{A_{0}}\right)^{1+\frac{\Delta}{2}} (2.3)

where AA is the standard horizon area, A0A_{0} is the Planck area, and Δ\Delta is an exponent in the range 0<Δ<10<\Delta<1. This exponent quantifies quantum deformations, when Δ=1\Delta=1 the deformation is maximum and the Bekenstein entropy is recovered when Δ=0\Delta=0.

Following the gravity-thermodynamics approach and assuming the Barrow entropy SBS_{B} (Eq. 2.3), it is possible to obtain the Friedmann equations governing the cosmic dynamics (see further details in [25, 20]). We investigate the background Cosmology in two cases: when the Universe is filled just by matter (Model I) and by matter plus radiation (Model II). In the following, we introduce the Friedmann equation in both scenarios.

2.1 Model I: Matter and an effective dark energy

For a flat Universe (k=0k=0) filled by matter, the Friedmann and Raychaudhuri equations [20] are

H2=8πG3(ρm+ρDE),\displaystyle H^{2}=\frac{8\pi G}{3}\left(\rho_{m}+\rho_{DE}\right), (2.4)
H˙=4πG(ρm+pm+ρDE+pDE),\displaystyle\dot{H}=-4\pi G\left(\rho_{m}+p_{m}+\rho_{DE}+p_{DE}\right), (2.5)

where ρm\rho_{m} denotes the energy density of matter (baryons plus dark matter) and we assume the equation of state pm=0p_{m}=0 corresponding to dust (pressureless) matter. The energy density and pressure of this effective dark energy are written in the form

ρDE=38πG{Λ3+H2[1β(Δ+2)2ΔHΔ]},\displaystyle\rho_{DE}=\frac{3}{8\pi G}\left\{\frac{\Lambda}{3}+H^{2}\left[1-\frac{\beta(\Delta+2)}{2-\Delta}H^{-\Delta}\right]\right\}, (2.6)
pDE=18πG{Λ+2H˙[1β(1+Δ2)HΔ]+3H2[1β(2+Δ)2ΔHΔ]},\displaystyle p_{DE}=-\frac{1}{8\pi G}\Big{\{}\Lambda+2\dot{H}\Big{[}1-\beta\Big{(}1+\frac{\Delta}{2}\Big{)}H^{-\Delta}\Big{]}+3H^{2}\Big{[}1-\frac{\beta(2+\Delta)}{2-\Delta}H^{-\Delta}\Big{]}\Big{\}}, (2.7)

where Λ4CG(4π)Δ/2\Lambda\equiv 4{C}G(4\pi)^{\Delta/2}, CC is an appropriate integration constant and β4(4π)Δ/2G/A01+Δ/2\beta\equiv 4(4\pi)^{\Delta/2}G/A_{0}^{1+\Delta/2}. Firstly, we keep β\beta as a free parameter. Next, by setting A0=4GA_{0}=4G we have β(π/G)Δ/2\beta\equiv(\pi/G)^{\Delta/2}.

Although Eqs. (2.4)-(2.5) does not has a dark energy component, we have dubbed effective dark energy the extra-terms introduced by the Barrow entropy.

The equation of state (EoS) for the effective dark energy reads

wDEpDEρDE=12H˙[1β(1+Δ2)HΔ]Λ+3H2[1β(2+Δ)2ΔHΔ].\displaystyle w_{DE}\equiv\frac{p_{DE}}{\rho_{DE}}=-1-\frac{2\dot{H}\left[1-\beta\left(1+\frac{\Delta}{2}\right)H^{-\Delta}\right]}{\Lambda+3H^{2}\left[1-\frac{\beta(2+\Delta)}{2-\Delta}H^{-\Delta}\right]}. (2.8)

Combining (2.4) and (2.6), the dimensionless Friedmann equation takes the form

8πGρm3H2+Λ3H2=β(Δ+2)HΔ2Δ.\frac{8\pi G\rho_{m}}{3H^{2}}+\frac{\Lambda}{3H^{2}}=\frac{\beta(\Delta+2)H^{-\Delta}}{2-\Delta}. (2.9)

The standard model with cold dark matter and cosmological constant (Λ\LambdaCDM) is recovered with Δ=0,β=1\Delta=0,\beta=1, which implies

8πGρm3H2+Λ3H2=1.\frac{8\pi G\rho_{m}}{3H^{2}}+\frac{\Lambda}{3H^{2}}=1. (2.10)

Now, we define

Ωm8πGρm3H2,ΩΛΛ3H2,\displaystyle\Omega_{m}\equiv\frac{8\pi G\rho_{m}}{3H^{2}},\quad\Omega_{\Lambda}\equiv\frac{\Lambda}{3H^{2}},
ΩDE8πGρDE3H2=1+ΩΛβ(Δ+2)HΔ2Δ.\displaystyle\Omega_{DE}\equiv\frac{8\pi G\rho_{DE}}{3H^{2}}=1+\Omega_{\Lambda}-\frac{\beta(\Delta+2)H^{-\Delta}}{2-\Delta}. (2.11)

Then, from Eq. (2.9) it follows

Ωm+ΩDE=1+Ωm+ΩΛβ(Δ+2)HΔ2Δ=0=1.\Omega_{m}+\Omega_{DE}=1+\underbrace{\Omega_{m}+\Omega_{\Lambda}-\frac{\beta(\Delta+2)H^{-\Delta}}{2-\Delta}}_{=0}=1. (2.12)

By considering that the matter component evolves in the traditional way ρm=ρm0(z+1)3\rho_{m}=\rho_{m0}(z+1)^{3}, the dimensionless Friedmann equation can alternatively be written as

E(z)HH0={β¯2Δ2+Δ[Ωm0(z+1)3+ΩΛ0]}1/(2Δ),\displaystyle E(z)\equiv\frac{H}{H_{0}}=\Big{\{}\bar{\beta}\frac{2-\Delta}{2+\Delta}[\Omega_{m0}(z+1)^{3}+\Omega_{\Lambda 0}]\Big{\}}^{1/(2-\Delta)}, (2.13)

where a=(z+1)1a=(z+1)^{-1}, zz is the redshift, the subscripts 0 denote quantities at a=1(z=0)a=1(z=0), and we have defined the dimensionless parameter

β¯H0Δβ=H0ΔA01+Δ/24(4π)Δ/2G=H0Δ(G/π)Δ/2settingA0=4G,\displaystyle\bar{\beta}\equiv\frac{H_{0}^{\Delta}}{\beta}=\frac{H_{0}^{\Delta}A_{0}^{1+\Delta/2}}{4(4\pi)^{\Delta/2}G}\underbrace{={H_{0}^{\Delta}(G/\pi)^{\Delta/2}}}_{\text{setting}\;A_{0}=4G}, (2.14)

where we have set the Planck area A0=4GA_{0}=4G. Notice that when Δ=0\Delta=0, and β¯=1\bar{\beta}=1, the Λ\LambdaCDM model is recovered.

Furthermore, the flatness constraint E(0)=1E(0)=1, gives the equation

ΩΛ0=(2+Δ2Δ)1β¯Ωm0.\Omega_{\Lambda 0}=\left(\frac{2+\Delta}{2-\Delta}\right)\frac{1}{\bar{\beta}}-\Omega_{m0}. (2.15)

In addition, the deceleration parameter is defined as

q=1H˙H2.q=-1-\frac{\dot{H}}{H^{2}}. (2.16)

By substituting Eq. (2.13) and replacing Eqs. (2.6), (2.7) into (2.5), the q(z)q(z) results

q(z)=1+3Ωm0(z+1)3E(z)[β¯(2Δ)Δ1(2+Δ)]1/(2Δ)[Ωm0(z+1)3+ΩΛ0](Δ1)/(2Δ),\displaystyle q(z)=-1+\frac{3\Omega_{m0}(z+1)^{3}}{E(z)}\left[\frac{\bar{\beta}(2-\Delta)^{\Delta-1}}{(2+\Delta)}\right]^{1/(2-\Delta)}[\Omega_{m0}(z+1)^{3}+\Omega_{\Lambda 0}]^{(\Delta-1)/(2-\Delta)},

and the DE EoS in terms of Eqs. (2.13)-(2.14) is written as

wDE=1+2(z+1)E(z)E(z)[1(1+Δ/2)(Eβ¯)Δ]3ΩΛ+3E(z)2[1(2+Δ)2Δ(Eβ¯)Δ]\displaystyle w_{DE}=-1+\frac{2(z+1)E(z)E^{\prime}(z)[1-(1+\Delta/2)(E\bar{\beta})^{-\Delta}]}{3\Omega_{\Lambda}+3E(z)^{2}\left[1-\frac{(2+\Delta)}{2-\Delta}(E\bar{\beta})^{-\Delta}\right]} (2.18)

where

E(z)=3Ωm0β¯2+ΔE(z)(Δ1)(z+1)2.\displaystyle E^{\prime}(z)=3\Omega_{m0}\frac{\bar{\beta}}{2+\Delta}E(z)^{(\Delta-1)}(z+1)^{2}. (2.19)

It is worthy to note that for β¯=1\bar{\beta}=1, Δ=0\Delta=0 and z1z\to 1 the EoS for the cosmological constant is recovered, i.e. wDE=1w_{DE}=-1.

2.2 Model II: Matter, Radiation and Effective Dark Energy

By considering two fluids, matter and radiation, for a flat Universe, the Friedmann and Raychaudhuri equations in Barrow cosmology result as follows

H2=8πG3(ρm+ρr+ρDE),\displaystyle H^{2}=\frac{8\pi G}{3}\left(\rho_{m}+\rho_{r}+\rho_{DE}\right), (2.21)
H˙=4πG(ρm+pm+ρr+pr+ρDE+pDE),\displaystyle\dot{H}=-4\pi G\left(\rho_{m}+p_{m}+\rho_{r}+p_{r}+\rho_{DE}+p_{DE}\right),

where ρr\rho_{r} indicates the radiation energy density and the radiation pressure is pr=ρr/3p_{r}=\rho_{r}/3. We define

Ωr8πGρr3H2.\displaystyle\Omega_{r}\equiv\frac{8\pi G\rho_{r}}{3H^{2}}. (2.22)

Using the previous variable definitions (2.11), the dimensionless Friedmann equation becomes

ΩΛ+Ωm+Ωr=β(Δ+2)HΔ2Δ.\Omega_{\Lambda}+\Omega_{m}+\Omega_{r}=\frac{\beta(\Delta+2)H^{-\Delta}}{2-\Delta}. (2.23)

Finally, from Eq. (2.23) it follows

Ωm+Ωr+ΩDE=1+Ωm+Ωr+ΩΛβ(Δ+2)HΔ2Δ=0=1.\Omega_{m}+\Omega_{r}+\Omega_{DE}=1+\underbrace{\Omega_{m}+\Omega_{r}+\Omega_{\Lambda}-\frac{\beta(\Delta+2)H^{-\Delta}}{2-\Delta}}_{=0}=1. (2.24)

The dimensionless Friedmann equation can be written as

E(z)HH0={β¯2Δ2+Δ[Ωm0(z+1)3+Ωr0(z+1)4+ΩΛ0]}1/(2Δ),\displaystyle E(z)\equiv\frac{H}{H_{0}}=\Big{\{}\bar{\beta}\frac{2-\Delta}{2+\Delta}[\Omega_{m0}(z+1)^{3}+\Omega_{r0}(z+1)^{4}+\Omega_{\Lambda 0}]\Big{\}}^{1/(2-\Delta)}, (2.25)

where the radiation component evolves in the traditional way ρr=ρr0(z+1)4\rho_{r}=\rho_{r0}(z+1)^{4}, and Ωr0\Omega_{r0} is obtained from (2.22) evaluated at a=1a=1 (z=0z=0). This can be calculated as Ωr0=2.469×105h2(1+0.2271Neff)\Omega_{r0}=2.469\times 10^{-5}h^{-2}(1+0.2271N_{eff}), with Neff=3.04N_{eff}=3.04 as the number of relativistic species [26] and h=H0/100kms1Mpc1h=H_{0}/100\mathrm{kms}^{-1}\mathrm{Mpc}^{-1} as the current Hubble dimensionless parameter.

The flatness constriction E(0)=1E(0)=1, gives the equation

ΩΛ0=(2+Δ2Δ)1β¯Ωm0Ωr0.\Omega_{\Lambda 0}=\left(\frac{2+\Delta}{2-\Delta}\right)\frac{1}{\bar{\beta}}-\Omega_{m0}-\Omega_{r0}. (2.26)

In addition, the deceleration parameter reads

q(z)=1+[β¯(2Δ)Δ1(2+Δ)]1/(2Δ)×\displaystyle q(z)=-1+\left[\frac{\bar{\beta}(2-\Delta)^{\Delta-1}}{(2+\Delta)}\right]^{1/(2-\Delta)}\times
3Ωm0(z+1)3+4Ωr0(z+1)4E(z)[Ωm0(z+1)3+Ωr0(z+1)4+ΩΛ0](Δ1)/(2Δ).\displaystyle\frac{3\Omega_{m0}(z+1)^{3}+4\Omega_{r0}(z+1)^{4}}{E(z)}[\Omega_{m0}(z+1)^{3}+\Omega_{r0}(z+1)^{4}+\Omega_{\Lambda 0}]^{(\Delta-1)/(2-\Delta)}. (2.27)

The DE EoS can be calculated by substituting Eq. (2.25) into Eq. (2.18) and E(z)E^{\prime}(z) as

E(z)=β¯2+ΔE(z)(Δ1)[3Ωm0(z+1)2+4Ωr0(z+1)3].\displaystyle E^{\prime}(z)=\frac{\bar{\beta}}{2+\Delta}E(z)^{(\Delta-1)}[3\Omega_{m0}(z+1)^{2}+4\Omega_{r0}(z+1)^{3}]. (2.28)

Notice that for β¯=1\bar{\beta}=1, Δ=0\Delta=0 and z1z\to 1 the EoS for the cosmological constant is recovered.

3 Observational constraints

For both models under Barrow cosmology (Model I: universe filled by matter and Model II: universe filled by matter plus radiation), the free parameters of the model are: hh, Ωm0\Omega_{m0}, β¯\bar{\beta}, and Δ\Delta. To constrain these parameters we employ observational Hubble data (OHD) [27], Type Ia supernovaes (SNIa) [28], HII galaxies (HIIG) [29], strong lensing systems (SLS) [30], and baryon acoustic oscillations (BAO) [31]. In the following we briefly describe these samples.

3.1 Observational Hubble Data

A cosmological-independent measurement of the Hubble parameter is acquired through the differential age (DA) technique [32] in cosmic chronometers (i.e passive elliptic galaxies). In this paper, we consider the OHD compilation provided by [27] containing 3131 data points in the range 0.07<z<1.9650.07<z<1.965. Hence, the chi square function for OHD can be constructed through the following equation

χOHD2=i31(Hth(𝚯,zi)Hobs(zi)σobsi)2,\chi^{2}_{{\rm OHD}}=\sum_{i}^{31}\left(\frac{H_{th}({\bf\Theta},z_{i})-H_{obs}(z_{i})}{\sigma^{i}_{obs}}\right)^{2}, (3.1)

where Hth(𝚯,zi)H_{th}({\bf\Theta},z_{i}) and Hobs(zi)H_{obs}(z_{i}), are the theoretical and observational Hubble parameters respectively at the redshift ziz_{i}, and σobsi\sigma^{i}_{obs} is the observational error. Notice that 𝚯{\bf\Theta} is a vector related to the number of free parameters of the studied cosmological model.

3.2 Pantheon SNIa sample

The Pantheon sample [33] contains 10481048 SNIa data points in the redshift range 0.001<z<2.30.001<z<2.3. The observational distance modulus μPAN\mu_{\mathrm{PAN}} for Pantheon SNIa can be measured as

μPAN=mbMB+α×X1β×C+ΔM+ΔB,\mu_{\mathrm{PAN}}=m_{b}^{\star}-M_{B}+\alpha\times X_{1}-\beta\times C+\Delta_{M}+\Delta_{B}, (3.2)

where mbm_{b}^{\star} corresponds to the observed peak magnitude, MBM_{B} is the B-band absolute magnitude, α\alpha, and β\beta coefficients are nuisance parameters; X1X_{1} and CC are variables describing the time stretching of the light-curve and the Supernova color at maximum brightness, respectively. ΔM\Delta_{M} is a distance correction based on the host-galaxy mass of the SNIa and ΔB\Delta_{B} is a distance correction based on predicted biases from simulations.

The theoretical counterpart of the distance modulus for any cosmological model is given by μth(𝚯,z)=5log10(dL(𝚯,z)/10pc)\mu_{th}({\bf\Theta},z)=5\log_{10}\left(d_{L}({\bf\Theta},z)/10\mathrm{pc}\right), where dLd_{L} is the luminosity distance given by

dL(𝚯,z)=cH0(1+z)0zdzE(z),d_{L}({\bf\Theta},z)=\frac{c}{H_{0}}(1+z)\int^{z}_{0}\frac{\mathrm{dz}^{\prime}}{E(z^{\prime})}, (3.3)

where cc is the light speed velocity. Since that [33] provide μ~PAN=μPAN+MB\tilde{\mu}_{\mathrm{PAN}}=\mu_{\mathrm{PAN}}+M_{B}, we can marginalize over the MBM_{B} parameter to compare the data with the underlying cosmology. Thus, the marginalized figure-of-merit for the Pantheon sample is given by

χPanMmarg2=a+log(e2π)b2e,\chi_{Pan_{Mmarg}}^{2}=a+\log\left(\frac{e}{2\pi}\right)-\frac{b^{2}}{e}, (3.4)

where a=Δ𝝁~T𝐂𝐏𝟏Δ𝝁~,b=Δ𝝁~T𝐂𝐏𝟏Δ𝟏a=\Delta\boldsymbol{\tilde{\mu}}^{T}\cdot\mathbf{C_{P}^{-1}}\cdot\Delta\boldsymbol{\tilde{\mu}},\,b=\Delta\boldsymbol{\tilde{\mu}}^{T}\cdot\mathbf{C_{P}^{-1}}\cdot\Delta\mathbf{1},  e=Δ𝟏T𝐂𝐏𝟏Δ𝟏e=\Delta\mathbf{1}^{T}\cdot\mathbf{C_{P}^{-1}}\cdot\Delta\mathbf{1}, and Δ𝝁~\Delta\boldsymbol{\tilde{\mu}} is the vector of residuals between the model distance modulus and the observed μ~PAN\tilde{\mu}_{\mathrm{PAN}}. The covariance matrix 𝐂𝐏\mathbf{C_{P}} is constructed by adding the systematic and statistical matrices of μ~PAN\tilde{\mu}_{\mathrm{PAN}}. We refer the interested reader to [33] for a detailed description of how these matrices are constructed.

3.3 HII Galaxies

HIIG are galaxies with large HII regions, product of young and hot stars (O and/or B type stars) ionizing the medium. For these galaxies there is a correlation between the measured luminosity, LL, and the inferred velocity dispersion, σ\sigma, of the ionized gas. Several authors have shown that the correlation LσL-\sigma could be used as a cosmological tracer [34, 35, 36, 37, 38, and references therein]. A HIIG data sample was compiled by [38] containing 107107 low redshift (0.00880.0088 \leq zz \leq 0.164170.16417) galaxies, and 4646 high redshift (0.6364270.636427 \leq zz \leq 2.429352.42935) galaxies. [29] used such HIIG sample to constrain the cosmological parameters for six different cosmological models. Recently, [39] presented a new sample which contains 181181 local and high-z HIIG data points in the redshift range 0.01<z<2.60.01<z<2.6. In this paper, we use such HIIG sample, and follow their methodology [see 39].

The correlation between LL and σ\sigma can be written as

logL=βIIlogσ+γ,\log L=\beta_{II}\log\sigma+\gamma, (3.5)

where γ\gamma and βII\beta_{II} are the intercept and slope functions, respectively. Following [29, 38, 39], we set βII\beta_{II} = 5.022, and γ\gamma = 33.268. Therefore, the distance modulus takes the form

μobs=2.5logL2.5logf100.2,\mu_{obs}=2.5\log L-2.5\log f-100.2, (3.6)

where ff is the flux emitted by the HIIG. Moreover, the theoretical distance modulus is

μth(𝚯,z)=5logdL(𝚯,z)+25,\mu_{th}({\bf\Theta},z)=5\log d_{L}({\bf\Theta},z)+25, (3.7)

being dL(𝚯,z)d_{L}({\bf\Theta},z) the luminosity distance (in Mpc).

The figure-of-merit is given by the following equation

χHIIG2=i18[μth(𝚯,zi)μobs(zi)]ϵi2,\chi^{2}_{{\rm HIIG}}=\sum_{i}^{18}\frac{[\mu_{th}({\bf\Theta},z_{i})-\mu_{obs}(z_{i})]}{\epsilon_{i}^{2}}, (3.8)

where ϵi\epsilon_{i} is the uncertainty of the ithi_{th} measurement and it can be calculated propagating the errors of Eq. 3.6 [see further details in 39].

3.4 Strong lensing systems

Several authors have shown that strong lensing systems can be used as cosmological tool to constrain cosmological parameters [30]. The method consists in comparing a theoretical distance ratio of angular diameter distances in the lens geometry with its observational counterpart. It can be obtained from the Einstein radius of a lens (modeled with a singular isothermal sphere) given by

θE=4πσl2Dlsc2Ds,\theta_{E}=4\pi\frac{\sigma_{l}^{2}D_{ls}}{c^{2}D_{s}}, (3.9)

where σl\sigma_{l} is the observed velocity dispersion of the lens galaxy, DsD_{s} is the angular diameter distance to the source at redshift zsz_{s}, and DlsD_{ls} is the angular diameter distance from the lens (at redshift zlz_{l}) to the source. Then, the observational distance ratio of angular diameter distances is defined as

Dobsc2θE/4πσ2.D^{obs}\equiv c^{2}\theta_{E}/4\pi\sigma^{2}. (3.10)

To measure the theoretical distance ratio Dth(𝚯,zl,zs)Dls/DsD^{th}({\bf\Theta},z_{l},z_{s})\equiv D_{ls}/D_{s}, we calculate DsD_{s} using the definition of angular diameter distance of a source at redshift zz

DA(𝚯,z)=cH0(1+z)0zdzE(z),D_{A}({\bf\Theta},z)=\frac{c}{H_{0}(1+z)}\int_{0}^{z}\frac{dz^{\prime}}{E(z^{\prime})}, (3.11)

and DlsD_{ls} through the definition of the angular diameter distance between two objects at redshift z1z_{1} and z2z_{2}

D12(𝚯,z)=cH0(1+z2)z1z2dzE(z).D_{12}({\bf\Theta},z)=\frac{c}{H_{0}(1+z_{2})}\int_{z_{1}}^{z_{2}}\frac{dz^{\prime}}{E(z^{\prime})}. (3.12)

The most recent compilation of Strong-Lensing Systems (SLS) given by [30] consists of 204 SLS spanning the redshift region 0.0625<zl<0.9580.0625<z_{l}<0.958 for the lens and 0.196<zs<3.5950.196<z_{s}<3.595 for the source. To avoid convergence problems and discarding (unphysical) systems with Dls>DsD_{ls}>D_{s}, the authors provided a fiducial sample with an observational lens equation (DobsD^{obs}) within the region 0.5Dobs10.5\leq D^{obs}\leq 1.

In this work, we use such a fiducial sample consisting of 143 SLS, and the chi-square function takes the form

χSLS2=i143[Dth(𝚯,zl,zs)Dobs(θE,σ2)]2(δDobs)2,\chi^{2}_{\rm SLS}=\sum_{i}^{143}\frac{[D^{th}({\bf\Theta},z_{l},z_{s})-D^{obs}(\theta_{E},\sigma^{2})]^{2}}{(\delta D^{obs})^{2}}, (3.13)

where

δDobs=Dobs[(δθEθE)2+4(δσσ)2]1/2,\delta D^{obs}=D^{obs}\left[\left(\frac{\delta\theta_{E}}{\theta_{E}}\right)^{2}+4\left(\frac{\delta\sigma}{\sigma}\right)^{2}\right]^{1/2}, (3.14)

being δθE\delta\theta_{E} and δσ\delta\sigma the uncertainties of the Einstein radius and velocity dispersion, respectively.

3.5 Baryon Acoustic Oscillations

BAO are considered as standard rulers, being primordial signatures of the interaction of baryons and photons in a hot plasma on the matter power spectrum in the pre-recombination epoch. Authors in [40] collected 6 correlated data points measured by [41, 42, 43]. To confront cosmological models to these data, it is useful to build the χ2\chi^{2}-function in the form

χBAO2=ΔXTCov1ΔX,\chi^{2}_{\rm BAO}=\Delta\vec{X}^{T}\rm{Cov}^{-1}\Delta\vec{X}\,, (3.15)

where ΔX\Delta\vec{X} is the difference between the theoretical and observational values of dA(zdrag)/DV(zi)d_{A}(z_{drag})/D_{V}(z_{i}) where zdragz_{drag} is defined by the sound horizon at baryon drag epoch measured at the redshift ziz_{i}, and Cov1\rm{Cov}^{-1} is the inverse of covariance matrix, the dilation scale (DVD_{V}) is defined as [44]

DV(𝚯,z)=[dA2(𝚯,z)czH0E(z)]1/3D_{V}({\bf\Theta},z)=\left[\frac{d_{A}^{2}({\bf\Theta},z)\,c\,z}{H_{0}E(z)}\right]^{1/3} (3.16)

where dA(𝚯,z)=(1+z)DA(𝚯,z)d_{A}({\bf\Theta},z)=(1+z)D_{A}({\bf\Theta},z) is the comoving angular-diameter distance and DAD_{A} is the angular diameter distance at zz presented in Eq. (3.11). Additionally, rdragr_{drag} is the sound horizon at baryon drag epoch. We use rdrag=147.21±0.23r_{drag}=147.21\pm 0.23 reported in [2].

3.6 Results from Observational constraints

The inference of the cosmological parameters under Barrow cosmology, for both model I (Eq. 2.13) and II (Eq. 2.25), is performed using a Bayesian Markov Chain Monte Carlo (MCMC) approach using the emcee Python module [45]. We set 30003000 chains with 250250 steps each one. The burn-in phase is stopped up to obtain convergence according to the auto-correlation time criteria. We build a Gaussian log-likelihood as the merit-of-function to minimize through the equation 2log(data)χdata2-2\log(\mathcal{L}_{\rm data})\varpropto\chi^{2}_{\rm data} for each dataset, and consider Gaussian priors on hh and Ωm0\Omega_{m0} centered at 0.6766±0.00420.6766\pm 0.0042 and 0.3111±0.00560.3111\pm 0.0056 [2], respectively, and a flat prior for Δ\Delta in the ranges: Δ:[0,2]\Delta:\,[0,2]. The parameter β¯\bar{\beta} is calculated using Eq. (2.14), where we have set A0=4GA_{0}=4G. Additionally, a joint analysis can be constructed through the sum of their function-of-merits, i.e.,

χJoint2=χSNIa2+χBAO2+χOHD2+χSLS2+χHIIG2,\chi^{2}_{\rm Joint}=\chi^{2}_{\rm SNIa}+\chi^{2}_{\rm BAO}+\chi^{2}_{\rm OHD}+\chi^{2}_{\rm SLS}+\chi^{2}_{\rm HIIG}, (3.17)

where subscripts indicate the observational measurements under consideration.

Figure 1 shows the 2D confidence contours at 68%68\% (1σ1\sigma) and 99.7%99.7\% (3σ3\sigma) confidence level (CL) respectively, and 1D posterior distribution of the parameters in Barrow cosmology with a matter component (top panel) and matter plus radiation. In the case of the Δ\Delta parameter, although the contours for most of the samples are consistent with each other, the ones obtained using SLS data are in tension with those estimated with the other samples. However, this is not surprising inasmuch as reported by [30], the use of their fiduciary sample of 143 strong lensing systems while performs better constraining the cosmological models tested in such work (compared with other lensing samples), the parameters are not tightly constraint. Indeed, they reported that the range on the studied cosmological parameters were in agreement with those expected from other astrophysical observations, but they also discussed that the method needs improvement, in particular to take into account systematic biases (e.g. not fully confirmed lenses, multiple arcs, uncertain redshifts, complex lens substructure).

Table 1 presents the chi-square and mean values of the parameters obtained from the different data set and their uncertainties at 1σ1\sigma for both Barrow cosmologies. We obtain Δ=(5.9123.112+3.353)×104\Delta=(5.912^{+3.353}_{-3.112})\times 10^{-4}, β¯=0.9200.042+0.042\bar{\beta}=0.920^{+0.042}_{-0.042}, and Δ=(6.2453.164+3.377)×104\Delta=(6.245^{+3.377}_{-3.164})\times 10^{-4}, β¯=0.9150.043+0.043\bar{\beta}=0.915^{+0.043}_{-0.043} for model I and II, respectively. Both models are consistent at 2σ2\sigma with the standard cosmological model, i.e. Δ=0\Delta=0 and β¯=1\bar{\beta}=1. Moreover, the Δ\Delta bounds suggest the entropy-area relation is consistent with the Bekenstein entropy. From now on, we focus our discussion on the model II ( matter and radiation components) since it is a more realistic model.

The top panel of the Figure 2 shows that the expansion rate estimated from the mean values of the Barrow cosmology parameters are consistent with the OHD. In addition, the reconstruction of the deceleration parameter as function of redshift is shown in the middle panel of Fig. 2. The q(z)q(z) behavior is similar to the standard one, i.e. there is a transition at zt0.7110.034+0.035z_{t}\simeq 0.711^{+0.035}_{-0.034} from a decelerated stage to an accelerated stage with q0=0.5730.019+0.019q_{0}=-0.573^{+0.019}_{-0.019}, suggesting a de Sitter solution. However, in the Barrow scenario the late cosmic acceleration is driven by the new terms in the dynamical equations. Finally, the bottom panel of Fig. 2 illustrates the reconstruction of the equation of state of the effective dark energy as function of redshift. It is worth noting that it has a transition at zwde1.0700.104+0.114z_{wde}\simeq 1.070^{+0.114}_{-0.104} from a quintessence-like regime to a phantom-like one, yielding wDE(0)1.0001340.000068+0.000069w_{DE}(0)\simeq-1.000134^{+0.000069}_{-0.000068} at current times, which is consistent with the cosmological constant at 1σ1\sigma. This behavior of wDE(z)w_{DE}(z) has been also discussed by [20], the effective dark energy can undergo the phantom-divide crossing but it tends asymptotically to a de Sitter solution at late times.

Furthermore, the age of the Universe can be estimated by solving the integral t0=01da/aH(a)t_{0}=\int_{0}^{1}{\text{d}a}/aH(a). Considering the constraints from the joint analysis, we obtain t014.0620.170+0.179t_{0}\simeq 14.062^{+0.179}_{-0.170} (14.0450.167+0.17914.045^{+0.179}_{-0.167}) Gyr for matter+radiation (matter) model, consistent with 2σ2\sigma confidence level with the measurements of Planck [2]. Thus, the constraints obtained from several data at different scales indicate that, by modifying the entropy-area relation, Barrow cosmology is a plausible scenario to explain the late cosmic acceleration without the need to include an exotic component.

In the following sections, we perform a dynamical system analysis of the Barrow cosmology.

Refer to caption
Refer to caption
Figure 1: 2D contour at 68% and 99.7% CL and 1D posterior distribution of the free parameters in two models: universe filled by matter (top panel) and universe filled by matter plus radiation (bottom panel). Dashed lines represent best-fit values for Λ\LambdaCDM [2].
Refer to caption
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Figure 2: Top panel: H(z)H(z) function for the Barrow cosmological model using the mean values of the joint analysis. Middle panel: Reconstruction of the cosmological evolution of q(z)q(z) function using the mean values of the joint analysis. Bottom panel : Reconstruction of the equation-of-state of the effective dark energy. In all panels the shadow regions represent the 1σ1\sigma, and 3σ3\sigma (from darker to lighter color bands) confidence levels.
Table 1: Mean values of the free parameters for the Barrow cosmology in two scenarios: universe filled by matter (Model I) and by matter plus radiation (Model II).
Sample χ2\chi^{2} hh Ωm(0)\Omega_{m}^{(0)} Δ\Delta
Model I
SLS 217.28217.28 0.6770.004+0.0040.677^{+0.004}_{-0.004} 0.3110.006+0.0060.311^{+0.006}_{-0.006} 0.9630.700+0.7040.963^{+0.704}_{-0.700}
BAO 2.972.97 0.6770.004+0.0040.677^{+0.004}_{-0.004} 0.3120.005+0.0060.312^{+0.006}_{-0.005} (5.3703.550+4.713)×104(5.370^{+4.713}_{-3.550})\times 10^{-4}
DA OHD 15.6215.62 0.6780.004+0.0040.678^{+0.004}_{-0.004} 0.3120.006+0.0060.312^{+0.006}_{-0.006} (3.8132.752+4.774)×104(3.813^{+4.774}_{-2.752})\times 10^{-4}
HII 441.64441.64 0.6790.004+0.0040.679^{+0.004}_{-0.004} 0.3120.006+0.0050.312^{+0.005}_{-0.006} (7.5485.272+8.094)×104(7.548^{+8.094}_{-5.272})\times 10^{-4}
SNIa 1036.111036.11 0.6770.004+0.0040.677^{+0.004}_{-0.004} 0.3120.005+0.0050.312^{+0.005}_{-0.005} (5.0563.361+4.678)×104(5.056^{+4.678}_{-3.361})\times 10^{-4}
Joint 1749.081749.08 0.6800.004+0.0040.680^{+0.004}_{-0.004} 0.3110.005+0.0060.311^{+0.006}_{-0.005} (5.9123.112+3.353)×104(5.912^{+3.353}_{-3.112})\times 10^{-4}
Model II
SLS 217.28217.28 0.6770.004+0.0040.677^{+0.004}_{-0.004} 0.3110.006+0.0060.311^{+0.006}_{-0.006} 0.9630.708+0.7030.963^{+0.703}_{-0.708}
BAO 2.862.86 0.6770.004+0.0040.677^{+0.004}_{-0.004} 0.3120.006+0.0050.312^{+0.005}_{-0.006} (6.0083.880+4.949)×104(6.008^{+4.949}_{-3.880})\times 10^{-4}
DA OHD 15.6115.61 0.6780.004+0.0040.678^{+0.004}_{-0.004} 0.3120.006+0.0060.312^{+0.006}_{-0.006} (3.8092.740+4.855)×104(3.809^{+4.855}_{-2.740})\times 10^{-4}
HII 441.64441.64 0.6800.004+0.0040.680^{+0.004}_{-0.004} 0.3120.006+0.0060.312^{+0.006}_{-0.006} (7.5405.245+8.107)×104(7.540^{+8.107}_{-5.245})\times 10^{-4}
SNIa 1036.111036.11 0.6770.004+0.0040.677^{+0.004}_{-0.004} 0.3120.005+0.0060.312^{+0.006}_{-0.005} (5.1053.383+4.680)×104(5.105^{+4.680}_{-3.383})\times 10^{-4}
Joint 1748.891748.89 0.6800.004+0.0040.680^{+0.004}_{-0.004} 0.3110.006+0.0060.311^{+0.006}_{-0.006} (6.2453.164+3.377)×104(6.245^{+3.377}_{-3.164})\times 10^{-4}

4 Dynamical system and stability analysis

The phase-space and stability analysis is a complementary inspection that allows us to obtain a qualitative description of the local and global dynamics of cosmological scenarios independent of the initial conditions and the specific evolution of the universe. Furthermore, one can find asymptotic solutions and the corresponding theoretical values to compare with the observable ones. Examples of such quantities are the DE and total equation-of-state parameters, the deceleration parameter, the density parameters for the different species, etc. These observables allow to classify the cosmological solutions. In this regard, we can follow th reference [46], the first book related to modern dynamical systems theory to both cosmological models and observations.

In order to perform the stability analysis of a given cosmological scenario, one first transforms it to its autonomous form X=f(X)\textbf{X}^{\prime}=\textbf{f(X)} [46, 47, 48, 49, 50, 51, 52, 53, 54], where X is a column vector containing some auxiliary variables and primes denote derivative with respect to a time variable (conveniently chosen). Then, one extracts the critical points 𝐗𝐜\bf{X_{c}} by imposing the condition 𝐗=𝟎\bf{X}^{\prime}=0 and, in order to determine their stability properties, one expands around them with U the column vector of the perturbations of the variables. Therefore, for each critical point the perturbation equations are expanded to first order as U=𝐐U\textbf{U}^{\prime}={\bf{Q}}\cdot\textbf{U}, with the matrix 𝐐{\bf{Q}} containing the coefficients of the perturbation equations. The eigenvalues of 𝐐{\bf{Q}} determine the type and stability of the specific critical point.

4.1 Stability analysis of Model I

To start the dynamical analysis for the Barrow cosmology (§2), we use the dynamical variables (Ωm,ΩΛ)(\Omega_{m},\Omega_{\Lambda}) defined in (2.11), say,

Ωm=8πGρm3H2,ΩΛ=Λ3H2.\Omega_{m}=\frac{8\pi G\rho_{m}}{3H^{2}},\quad\Omega_{\Lambda}=\frac{\Lambda}{3H^{2}}. (4.1)

As we commented before, the normalized Friedmann equation (2.9) is then transformed to

ΩΛ+Ωm=β(Δ+2)HΔ2Δ.\Omega_{\Lambda}+\Omega_{m}=\frac{\beta(\Delta+2)H^{-\Delta}}{2-\Delta}. (4.2)

Notice that by substituting β=1,Δ=0\beta=1,\Delta=0, in Eq. (2.9), we obtain the usual relation in FRW cosmology. For β1,Δ0\beta\neq 1,\Delta\neq 0, by substituting Eqs. (2.6) and (2.7) into Eq. (2.5), we obtain

8πGρm+β(Δ+2)HΔH˙=0,\displaystyle 8\pi G\rho_{m}+\beta(\Delta+2)H^{-\Delta}\dot{H}=0, (4.3)
3H2Ωm+β(Δ+2)HΔH˙=0,\displaystyle\implies 3H^{2}\Omega_{m}+\beta(\Delta+2)H^{-\Delta}\dot{H}=0, (4.4)
3H2Ωm+(2Δ)(ΩΛ+Ωm)H˙=0.\displaystyle\implies 3H^{2}\Omega_{m}+(2-\Delta)\left(\Omega_{\Lambda}+\Omega_{m}\right)\dot{H}=0. (4.5)

Then, for H0H\neq 0, β1\beta\neq 1, and Δ0\Delta\neq 0, the deceleration parameter (Eq. (2.16)) results

q=1+3Ωm(2Δ)(ΩΛ+Ωm),q=-1+\frac{3\Omega_{m}}{(2-\Delta)(\Omega_{\Lambda}+\Omega_{m})}, (4.6)

for Λ\LambdaCDM (β=1,Δ=0\beta=1,\Delta=0) we obtain the usual relation q=1+32Ωmq=-1+\frac{3}{2}\Omega_{m}.

In general, H(t)H(t) satisfies the differential equation

H˙=ΛHΔβ(Δ+2)+3H2Δ2.\dot{H}=\frac{\Lambda H^{\Delta}}{\beta(\Delta+2)}+\frac{3H^{2}}{\Delta-2}. (4.7)

Furthermore, we have

ρm=3β(Δ+2)H2Δ8π(Δ2)GΛ8πG.\rho_{m}=-\frac{3\beta(\Delta+2)H^{2-\Delta}}{8\pi(\Delta-2)G}-\frac{\Lambda}{8\pi G}. (4.8)

Finally, we obtain the dynamical system

ΩΛ=2(q+1)ΩΛ,Ωm=(2q1)Ωm,\displaystyle\Omega_{\Lambda}^{\prime}=2(q+1)\Omega_{\Lambda},\quad\Omega_{m}^{\prime}=(2q-1)\Omega_{m}, (4.9)

where the prime means derivative with respect τ=ln(a)\tau=\ln(a), and qq is defined by (4.6). The main difference with the Λ\LambdaCDM model is that the term β(Δ+2)HΔ2Δ\frac{\beta(\Delta+2)H^{-\Delta}}{2-\Delta} in Eq. (4.2) is unbounded as H0H\rightarrow 0, resulting in unbounded ΩΛ,Ωm\Omega_{\Lambda},\Omega_{m}. The equilibrium points in the finite part of the phase space are

  1. 1.

    the line A(ΩΛ):A(\Omega_{\Lambda}): Ωm=0\Omega_{m}=0, ΩΛ=arbitrary\Omega_{\Lambda}=\text{arbitrary}, for Δ=arbitrary\Delta=\text{arbitrary}, with eigensystem (03{1,0}{2Δ2,1})\left(\begin{array}[]{cc}0&-3\\ \{1,0\}&\left\{\frac{2}{\Delta-2},1\right\}\\ \end{array}\right); and

  2. 2.

    the line B(Ωm):B(\Omega_{m}): Ωm=arbitrary,ΩΛ=0\Omega_{m}=\text{arbitrary},\Omega_{\Lambda}=0, for Δ=0\Delta=0, with eigensystem (30{1,1}{0,1})\left(\begin{array}[]{cc}3&0\\ \{-1,1\}&\{0,1\}\\ \end{array}\right).

The line of points B(Ωm)B(\Omega_{m}) exists only for Δ=0\Delta=0. All these lines of equilibrium points are normally hyperbolic because the tangent vector at a given point of each line is parallel to the corresponding eigenvector associated to the zero eigenvalue. This implies that the stability conditions can be inferred from the eigenvalues with non-zero real parts [55]. Therefore, the line A(ΩΛ)A(\Omega_{\Lambda}) is the attractor of the system, representing de Sitter solutions. For Δ=0\Delta=0, the line B(Ωm)B(\Omega_{m}) contains the past attractors, which represents matter dominated solutions.

4.1.1 Global dynamical systems formulation

In this section we define the compact variables (assuming H0,H0>0H\geq 0,H_{0}>0) based on the approach by [56]:

T=H0H0+H,T=\frac{H_{0}}{H_{0}+H}, (4.10)

along with the angular variable

θ=tan1(ΩmΩΛ)=tan1(8πGρmΛ),\theta=\tan^{-1}\left(\sqrt{\frac{\Omega_{m}}{\Omega_{\Lambda}}}\right)=\tan^{-1}\left(\sqrt{\frac{8\pi G\rho_{m}}{\Lambda}}\right), (4.11)

with inverse

H=H0(1T)T,ρm=Λtan2(θ)8πG.H=\frac{H_{0}(1-T)}{T},\quad\rho_{m}=\frac{\Lambda\tan^{2}(\theta)}{8\pi G}. (4.12)

We obtain the dynamical system

dTdτ¯=3(1T)2TΔ2ΛT3H0Δ2(1T1)Δβ(Δ+2),\displaystyle\frac{dT}{d\bar{\tau}}=-\frac{3(1-T)^{2}T}{\Delta-2}-\frac{\Lambda T^{3}{H_{0}}^{\Delta-2}\left(\frac{1}{T}-1\right)^{\Delta}}{\beta(\Delta+2)},
dθdτ¯=34(1T)sin(2θ),\displaystyle\frac{d\theta}{d\bar{\tau}}=-\frac{3}{4}(1-T)\sin(2\theta), (4.13)
Label Coordinates Eigenvalues Stability
dS+dS_{+} {θ=2nπ}\left\{\theta=2n\pi\right\} {32,0}\left\{-\frac{3}{2},0\right\} sink
dSdS_{-} {θ=(2n+1)π}\left\{\theta=(2n+1)\pi\right\} {32,0}\left\{-\frac{3}{2},0\right\} sink
M(0)M_{-}^{(0)} {T=0,θ=(4n1)π2}\left\{T=0,\theta=(4n-1)\frac{\pi}{2}\right\} {32Δ,32}\left\{\frac{3}{2-\Delta},\frac{3}{2}\right\} source
M+(0)M_{+}^{(0)} {T=0,θ=(4n+1)π2}\left\{T=0,\theta=(4n+1)\frac{\pi}{2}\right\} {32Δ,32}\left\{\frac{3}{2-\Delta},\frac{3}{2}\right\} source
M(1)M_{-}^{(1)} {T=1,θ=(4n1)π2}\left\{T=1,\theta=(4n-1)\frac{\pi}{2}\right\} {32Δ,32}\left\{-\frac{3}{2-\Delta},\frac{3}{2}\right\} saddle
M+(1)M_{+}^{(1)} {T=1,θ=(4n+1)π2}\left\{T=1,\theta=(4n+1)\frac{\pi}{2}\right\} {32Δ,32}\left\{-\frac{3}{2-\Delta},\frac{3}{2}\right\} saddle
Table 2: Equilibrium points/lines of system (4.16).

where for a function f{T,θ}f\in\{T,\theta\} we have introduced the new derivative

dfdτ¯=1(H0+H)dfdt,\frac{df}{d\bar{\tau}}=\frac{1}{(H_{0}+H)}\frac{df}{dt},

which allows for a global dynamical system analysis.

On the other hand, the equation (4.2) leads to

ΛT2sec2(θ)3H02(1T)2+β(Δ+2)(H0(1T1))ΔΔ2=0,\frac{\Lambda T^{2}\sec^{2}(\theta)}{3{H_{0}}^{2}(1-T)^{2}}+\frac{\beta(\Delta+2)\left(H_{0}\left(\frac{1}{T}-1\right)\right)^{-\Delta}}{\Delta-2}=0, (4.14)

that can be solved globally for β\beta, and we end up with the system

dTdτ¯=3(1T)2Tsin2(θ)2Δ,\displaystyle\frac{dT}{d\bar{\tau}}=\frac{3(1-T)^{2}T\sin^{2}(\theta)}{2-\Delta},
dθdτ¯=34(1T)sin(2θ),\displaystyle\frac{d\theta}{d\bar{\tau}}=-\frac{3}{4}(1-T)\sin(2\theta), (4.15)

defined in the finite cylinder 𝐒\mathbf{S} with boundaries T=0T=0 and T=1T=1, where the power-law dependence in the first equation (4.13) is eliminated. Using the logarithmic variable τ=ln(a)\tau=\ln(a), we obtain the complementary system

dTdτ=3(1T)Tsin2(θ)2Δ,\displaystyle\frac{dT}{d{\tau}}=\frac{3(1-T)T\sin^{2}(\theta)}{2-\Delta},
dθdτ=34sin(2θ).\displaystyle\frac{d\theta}{d{\tau}}=-\frac{3}{4}\sin(2\theta). (4.16)

The deceleration parameter is now written as

q=1+3Ωm(2Δ)ΩΛ(ΩmΩΛ+1)=1+3sin2(θ)2Δ.q=-1+\frac{3\Omega_{m}}{(2-\Delta)\Omega_{\Lambda}\left(\frac{\Omega_{m}}{\Omega_{\Lambda}}+1\right)}=-1+\frac{3\sin^{2}(\theta)}{2-\Delta}. (4.17)

From the first equation in (4.16), TT is a monotonically increasing function on 𝐒\mathbf{S}. As a consequence, all orbits originate from the invariant subset T=0T=0 (which contains the α\alpha-limit), which is classically related to the initial singularity with HH\rightarrow\infty, and ends on the invariant boundary subset T=1T=1, which corresponds asymptotically to H=0H=0.

We have the relations for the fractional energy densities:

Ωm=β(Δ+2)H01Δ(1T1)1Δ2(2Δ)ΛT6H0(1T),\displaystyle\Omega_{m}=\frac{\beta(\Delta+2)H_{0}^{1-\Delta}\left(\frac{1}{T}-1\right)^{1-\Delta}}{2(2-\Delta)}-\frac{\Lambda T}{6H_{0}(1-T)}, (4.18)
ΩΛ=ΛT6H0(1T).\displaystyle\Omega_{\Lambda}=\frac{\Lambda T}{6H_{0}(1-T)}. (4.19)

The system (4.16) admits the equilibrium points summarized in Table 2:

Refer to caption
Figure 3: Unwrapped solution space (left panel) and projection over the cylinder 𝐒\mathbf{S} defined in Cartesian coordinates (x,y,z)(x,y,z) by (4.20) (right panel) of the solution space of system (4.15) for Δ=5.912×104\Delta=5.912\times 10^{-4}, β¯=0.920\bar{\beta}=0.920 (top panel) and Δ=1\Delta=1, β¯=1\bar{\beta}=1 (bottom panel).
  1. 1.

    M±(0):θ=(4n±1)π2,T=0M_{\pm}^{(0)}:\theta=(4n\pm 1)\frac{\pi}{2},T=0, represented in Fig. 3;

  2. 2.

    M±(1):θ=(4n±1)π2,T=1M_{\pm}^{(1)}:\theta=(4n\pm 1)\frac{\pi}{2},T=1, represented in Fig. 3;

  3. 3.

    dS+:θ=2nπ,T=arbitrarydS_{+}:\theta=2n\pi,T=\text{arbitrary}, with representatives dS+(0)dS_{+}^{(0)} and dS+(1)dS_{+}^{(1)} respectively, denoted in Fig. 3 by a red line;

  4. 4.

    dS:θ=(2n+1)π,T=arbitrarydS_{-}:\theta=(2n+1)\pi,T=\text{arbitrary}, with representatives dS(0)dS_{-}^{(0)} and dS(1)dS_{-}^{(1)} respectively, denoted in Fig. 3 by a blue line;

where nn is an integer. There are two equivalent (due to the discrete symmetry) hyperbolic fixed points M±M_{\pm} for which q=1+32Δq=-1+\frac{3}{2-\Delta}, i.e. they are associated with dust fluid for Δ=0\Delta=0, and two equivalent fixed points dS±dS_{\pm} for which q=1q=-1, which therefore correspond to a de Sitter state.

For a representation of the flow of (4.16), we integrate it in the variables T,θT,\theta and project in a compact set using the “cylinder-adapted” coordinates

𝐒:{x=cosθ,y=sinθ,z=T,\mathbf{S}:\begin{cases}x=\cos\theta,\\ y=\sin\theta,\\ z=T,\end{cases} (4.20)

with 0T1,θ1[π,π]0\leq T\leq 1,\theta_{1}\in[-\pi,\pi], with inverse

{θ=tan1(yx),T=z.\begin{cases}\theta=\tan^{-1}\left(\frac{y}{x}\right),\\ T=z.\end{cases} (4.21)

Also, we present the whole evolution in the space (Ωm,T)(\Omega_{m},T) through the transform (T,θ)(Ωm,T)(T,\theta)\mapsto(\Omega_{m},T) where

Ωm\displaystyle\Omega_{m} =[(2+Δ2Δ)1β¯Ωm0]T2(1T)2tan2(θ).\displaystyle=\left[\left(\frac{2+\Delta}{2-\Delta}\right)\frac{1}{\bar{\beta}}-\Omega_{m0}\right]\frac{T^{2}}{(1-T)^{2}}\tan^{2}(\theta). (4.22)

The value T=1/2T=1/2 corresponds to current time. In these variables we have the system

dΩmdτ=3Ωm(β¯((Δ2)T2Ωm0Δ(1T)2Ωm)+(Δ+2)T2)(Δ2)β¯((1T)2ΩmT2Ωm0)(Δ+2)T2,\displaystyle\frac{d\Omega_{m}}{d\tau}=\frac{3\Omega_{m}\left(\bar{\beta}\left((\Delta-2)T^{2}\Omega_{m0}-\Delta(1-T)^{2}\Omega_{m}\right)+(\Delta+2)T^{2}\right)}{(\Delta-2)\bar{\beta}\left((1-T)^{2}\Omega_{m}-T^{2}\Omega_{m0}\right)-(\Delta+2)T^{2}},
dTdτ=3(T1)3Tβ¯Ωm(Δ2)β¯((1T)2ΩmT2Ωm0)(Δ+2)T2.\displaystyle\frac{dT}{d\tau}=\frac{3(T-1)^{3}T\bar{\beta}\Omega_{m}}{(\Delta-2)\bar{\beta}\left((1-T)^{2}\Omega_{m}-T^{2}\Omega_{m0}\right)-(\Delta+2)T^{2}}. (4.23)

In Figure 3 are represented the streamlines of the flow of (4.15) onto the unwrapped solution space (left panel) and its projection over the cylinder 𝐒\mathbf{S} (right panel) for two values of Δ\Delta one obtained from the joint constraint Δ=5.912×104\Delta=5.912\times 10^{-4}, and the other one is the extreme value Δ=1\Delta=1. The phase space is qualitatively the same as for system (4.16). Firstly, observe that systems (4.15) and (4.16) are independent of β¯\bar{\beta}. Therefore, the parameter β¯\bar{\beta} is dynamically irrelevant. The results summarized in points 1-4 before are confirmed in Figure 3. That is, the matter dominated solutions M±(0):θ=(4n±1)π2,T=0(H)M_{\pm}^{(0)}:\theta=(4n\pm 1)\frac{\pi}{2},T=0\;(H\rightarrow\infty) are past attractors. The matter dominated solutions M±(1):θ=(4n±1)π2,T=1(H0)M_{\pm}^{(1)}:\theta=(4n\pm 1)\frac{\pi}{2},T=1\;(H\rightarrow 0) are saddle and the attractor is the line of equilibrium points connecting dS(0)dS_{-}^{(0)} and dS(1)dS_{-}^{(1)} which are de Sitter solutions.

Refer to caption
Refer to caption
Figure 4: Streamlines of the flow of (4.23) for (a) Δ=5.912×104,β¯=0.920,Ωm0=0.311\Delta=5.912\times 10^{-4},\bar{\beta}=0.920,\Omega_{m0}=0.311 obtained from the joint constraints and (b) Δ=0,β=1,Ωm0=0.311\Delta=0,\beta=1,\Omega_{m0}=0.311 obtained from Λ\LambdaCDM model.

In Figure 4 streamlines of the flow of (4.23) are presented. We select the parameters (a) Δ=5.912×104,β¯=0.920,Ωm0=0.311\Delta=5.912\times 10^{-4},\bar{\beta}=0.920,\Omega_{m0}=0.311 obtained from the joint constraints and (b) Δ=0,β=1,Ωm0=0.311\Delta=0,\beta=1,\Omega_{m0}=0.311 for Λ\LambdaCDM model. These plots confirms that the late time attractor is the line of de Sitter points dS+dS_{+} and dSdS_{-}.

Complementary, we define an unbounded variable T~\tilde{T} and keep θ\theta:

T~=H0H,θ=tan1(8πGρmΛ),\tilde{T}=\frac{H_{0}}{H},\quad\theta=\tan^{-1}\left(\sqrt{\frac{8\pi G\rho_{m}}{\Lambda}}\right), (4.24)

and using the logarithmic variable τ=ln(a)=ln(1+z)\tau=\ln(a)=-\ln(1+z), we obtain the complementary system

dT~dτ=3T~sin2(θ)2Δ,\displaystyle\frac{d\tilde{T}}{d{\tau}}=\frac{3\tilde{T}\sin^{2}(\theta)}{2-\Delta},
dθdτ=34sin(2θ).\displaystyle\frac{d\theta}{d{\tau}}=-\frac{3}{4}\sin(2\theta). (4.25)

Setting a=1a=1 for the current universe, and considering the initial conditions:

θ(0)=tan1(Ωm0ΩΛ0),T~(0)=1,\theta(0)=\tan^{-1}\left(\sqrt{\frac{\Omega_{m0}}{\Omega_{\Lambda 0}}}\right),\quad\tilde{T}(0)=1, (4.26)

the system (4.1.1) is integrated to obtain

θ(τ)=tan1(e3τ/2Ωm0ΩΛ0),\displaystyle\theta(\tau)=\tan^{-1}\left(e^{-3\tau/2}\sqrt{\frac{\Omega_{m0}}{\Omega_{\Lambda 0}}}\right), (4.27)
T~(τ)=e3τΔ2(ΩΛ0+Ωm0ΩΛ0)12Δ(e3τ+Ωm0ΩΛ0)1Δ2,\displaystyle\tilde{T}(\tau)=e^{-\frac{3\tau}{\Delta-2}}\left(\frac{\Omega_{\Lambda 0}+\Omega_{m0}}{\Omega_{\Lambda 0}}\right)^{\frac{1}{2-\Delta}}\left(e^{3\tau}+\frac{\Omega_{m0}}{\Omega_{\Lambda 0}}\right)^{\frac{1}{\Delta-2}}, (4.28)

Finally, we get the exact evolution of HH and ρm\rho_{m}:

H=H0e3τ2Δ(ΩΛ0ΩΛ0+Ωm0)12Δ(e3τ+Ωm0ΩΛ0)12Δ\displaystyle H=H_{0}e^{-\frac{3\tau}{2-\Delta}}\left(\frac{\Omega_{\Lambda 0}}{\Omega_{\Lambda 0}+\Omega_{m0}}\right)^{\frac{1}{2-\Delta}}\left(e^{3\tau}+\frac{\Omega_{m0}}{\Omega_{\Lambda 0}}\right)^{\frac{1}{2-\Delta}}
=H0(Ωm0(z+1)3+ΩΛ0ΩΛ0+Ωm0)12Δ,\displaystyle=H_{0}\left(\frac{\Omega_{m0}(z+1)^{3}+\Omega_{\Lambda 0}}{\Omega_{\Lambda 0}+\Omega_{m0}}\right)^{\frac{1}{2-\Delta}}, (4.29)
ρm=Λtan2(θ)8πG=Λe3τΩm08πGΩΛ0=3H02Ωm08πG(z+1)3.\displaystyle\rho_{m}=\frac{\Lambda\tan^{2}(\theta)}{8\pi G}=\frac{\Lambda e^{-3\tau}\Omega_{m0}}{8\pi G\Omega_{\Lambda 0}}=\frac{3H_{0}^{2}\Omega_{m0}}{8\pi G}(z+1)^{3}. (4.30)

Eq. (4.29) can be deduced from Eq. (2.13) after the substitution of (2+Δ2Δ)1β¯\left(\frac{2+\Delta}{2-\Delta}\right)\frac{1}{\bar{\beta}} from Eq. (2.15).

These expressions are used to obtain the fractional energy densities corresponding to matter, to an effective a Λ\Lambda-like source, and to the effective dark energy as follows:

Ωm(z)=8πGρm3H2=Ωm0(z+1)3(Ωm0(z+1)3+ΩΛ0ΩΛ0+Ωm0)22Δ,\Omega_{m}(z)=\frac{8\pi G\rho_{m}}{3H^{2}}=\Omega_{m0}(z+1)^{3}\left(\frac{\Omega_{m0}(z+1)^{3}+\Omega_{\Lambda 0}}{\Omega_{\Lambda 0}+\Omega_{m0}}\right)^{-\frac{2}{2-\Delta}}, (4.31)

and

ΩΛ(z)=Λ3H2=ΩΛ0(Ωm0(z+1)3+ΩΛ0ΩΛ0+Ωm0)22Δ,ΩΛ0=Λ3H02.\Omega_{\Lambda}(z)=\frac{\Lambda}{3H^{2}}=\Omega_{\Lambda 0}\left(\frac{\Omega_{m0}(z+1)^{3}+\Omega_{\Lambda 0}}{\Omega_{\Lambda 0}+\Omega_{m0}}\right)^{-\frac{2}{2-\Delta}},\quad\Omega_{\Lambda 0}=\frac{\Lambda}{3H_{0}^{2}}. (4.32)

From Eq. (2.6) we infer

ΩDE(z)=8πGρDE3H2=Λ3H2+[1β(Δ+2)2ΔHΔ]\displaystyle\Omega_{DE}(z)=\frac{8\pi G\rho_{DE}}{3H^{2}}=\frac{\Lambda}{3H^{2}}+\left[1-\frac{\beta(\Delta+2)}{2-\Delta}H^{-\Delta}\right]
=1+ΩΛβ(Δ+2)2ΔH0Δ(Ωm0(z+1)3+ΩΛ0ΩΛ0+Ωm0)Δ2Δ\displaystyle=1+\Omega_{\Lambda}-\frac{\beta(\Delta+2)}{2-\Delta}H_{0}^{-\Delta}\left(\frac{\Omega_{m0}(z+1)^{3}+\Omega_{\Lambda 0}}{\Omega_{\Lambda 0}+\Omega_{m0}}\right)^{-\frac{\Delta}{2-\Delta}}
=1+ΩΛ0(Ωm0(z+1)3+ΩΛ0ΩΛ0+Ωm0)22Δ(Δ+2)(2Δ)1β¯(Ωm0(z+1)3+ΩΛ0ΩΛ0+Ωm0)Δ2Δ\displaystyle=1+\Omega_{\Lambda 0}\left(\frac{\Omega_{m0}(z+1)^{3}+\Omega_{\Lambda 0}}{\Omega_{\Lambda 0}+\Omega_{m0}}\right)^{-\frac{2}{2-\Delta}}-\frac{(\Delta+2)}{(2-\Delta)}\frac{1}{\bar{\beta}}\left(\frac{\Omega_{m0}(z+1)^{3}+\Omega_{\Lambda 0}}{\Omega_{\Lambda 0}+\Omega_{m0}}\right)^{-\frac{\Delta}{2-\Delta}}
=1+ΩΛ0(Ωm0(z+1)3+ΩΛ0ΩΛ0+Ωm0)22Δ(ΩΛ0+Ωm0)(Ωm0(z+1)3+ΩΛ0ΩΛ0+Ωm0)Δ2Δ\displaystyle=1+\Omega_{\Lambda 0}\left(\frac{\Omega_{m0}(z+1)^{3}+\Omega_{\Lambda 0}}{\Omega_{\Lambda 0}+\Omega_{m0}}\right)^{-\frac{2}{2-\Delta}}-\left(\Omega_{\Lambda 0}+\Omega_{m0}\right)\left(\frac{\Omega_{m0}(z+1)^{3}+\Omega_{\Lambda 0}}{\Omega_{\Lambda 0}+\Omega_{m0}}\right)^{-\frac{\Delta}{2-\Delta}}
=1Ωm0(1+z)3(Ωm0(1+z)3+ΩΛ0ΩΛ0+Ωm0)22Δ\displaystyle=1-\Omega_{m0}(1+z)^{3}\left(\frac{\Omega_{m0}(1+z)^{3}+\Omega_{\Lambda 0}}{\Omega_{\Lambda 0}+\Omega_{m0}}\right)^{-\frac{2}{2-\Delta}} (4.33)

where we use Eq. (2.15) to eliminate the term (2+Δ2Δ)1β¯\left(\frac{2+\Delta}{2-\Delta}\right)\frac{1}{\bar{\beta}}, apply Δ2Δ=122Δ-\frac{\Delta}{2-\Delta}=1-\frac{2}{2-\Delta}, and algebraically manipulate the equations to obtain ΩDE=1Ωm\Omega_{DE}=1-\Omega_{m}. It is straightforward to infer Eqs. (4.31), (4.32) and (4.1.1) in terms of the scale factor by replacing z=(1/a)1z=(1/a)-1.

Figure 5 shows the evolution of the density parameters Ωm\Omega_{m} and ΩDE\Omega_{DE} as a function of the scale factor aa for two cases: the joint constraints for hh, Ωm0\Omega_{m0}, Δ\Delta and β¯\bar{\beta} presented in Table 1 (solid lines) and the values for the standard model Δ=0\Delta=0, β¯=1\bar{\beta}=1 (dashed lines). The shadowed regions represent the 3σ3\sigma confidence levels. It is worthy to note that there are values of the energy densities which satisfy Ωm>1\Omega_{m}>1 and ΩDE<0\Omega_{DE}<0, however, these values are close to Λ\LambdaCDM lines within the 3σ3\sigma error propagation.

Refer to caption
Figure 5: Evolution of the density parameters for matter and effective dark energy in Barrow Cosmology using the joint constraints (solid lines) and the standard model (Δ=0\Delta=0, and β¯=1\bar{\beta}=1, dashed lines). The shadow regions represent the 3σ3\sigma confidence levels.

4.2 Stability analysis of Model II

We start our stability study of the dynamical variables (2.11) and (2.22), say,

Ωm=8πGρm3H2,Ωr=8πGρr3H2,ΩΛ=Λ3H2,\Omega_{m}=\frac{8\pi G\rho_{m}}{3H^{2}},\quad\Omega_{r}=\frac{8\pi G\rho_{r}}{3H^{2}},\quad\Omega_{\Lambda}=\frac{\Lambda}{3H^{2}}, (4.34)

related by (2.23). The evolution equations are now given by

ΩΛ=2(q+1)ΩΛ,\displaystyle\Omega_{\Lambda}^{\prime}=2(q+1)\Omega_{\Lambda},
Ωm=(2q1)Ωm,\displaystyle\Omega_{m}^{\prime}=(2q-1)\Omega_{m},
Ωr=2(q1)Ωr,\displaystyle\Omega_{r}^{\prime}=2(q-1)\Omega_{r}, (4.35)

where the prime means derivative with respect to τ=ln(a)\tau=\ln(a), and qq is defined by (4.36)

q=1+3Ωm+4Ωr(2Δ)(ΩΛ+Ωm+Ωr).q=-1+\frac{3\Omega_{m}+4\Omega_{r}}{(2-\Delta)(\Omega_{\Lambda}+\Omega_{m}+\Omega_{r})}. (4.36)

The equilibrium points in the finite part of the phase space are the lines of equilibrium points:

  1. 1.

    the line A(ΩΛ):A(\Omega_{\Lambda}): Ωm=0,Ωr\Omega_{m}=0,\Omega_{r}, ΩΛ=arbitrary\Omega_{\Lambda}=\text{arbitrary}, for Δ=arbitrary\Delta=\text{arbitrary}, with eigensystem (043{1,0,0}{2Δ2,0,1}{2Δ2,1,0})\left(\begin{array}[]{ccc}0&-4&-3\\ \{1,0,0\}&\left\{\frac{2}{\Delta-2},0,1\right\}&\left\{\frac{2}{\Delta-2},1,0\right\}\\ \end{array}\right);

  2. 2.

    the line B(Ωm):B(\Omega_{m}): Ωm=arbitrary,Ωr=0,ΩΛ=0\Omega_{m}=\text{arbitrary},\Omega_{r}=0,\Omega_{\Lambda}=0, for Δ=0\Delta=0, with eigensystem (310{1,1,0}{0,1,1}{0,1,0})\left(\begin{array}[]{ccc}3&-1&0\\ \{-1,1,0\}&\{0,-1,1\}&\{0,1,0\}\\ \end{array}\right); and

  3. 3.

    the line C(Ωr):C(\Omega_{r}): Ωm=0,Ωr=arbitrary,ΩΛ=0\Omega_{m}=0,\Omega_{r}=\text{arbitrary},\Omega_{\Lambda}=0, for Δ=0\Delta=0, with eigensystem (410{1,0,1}{0,1,1}{0,0,1})\left(\begin{array}[]{ccc}4&1&0\\ \{-1,0,1\}&\{0,-1,1\}&\{0,0,1\}\\ \end{array}\right).

The last two lines of equilibrium points, B(Ωm)B(\Omega_{m}) and C(Ωr)C(\Omega_{r}), exist only for Δ=0\Delta=0. All three lines are normally hyperbolic because the tangent vector at a given point of each line is parallel to the corresponding eigenvector associated to the zero eigenvalue. This implies that the stability conditions can be inferred from the eigenvalues with non-zero real parts [55]. Therefore, the line A(ΩΛ)A(\Omega_{\Lambda}) is the attractor of the system, representing de Sitter solutions. For Δ=0\Delta=0, the line B(Ωm)B(\Omega_{m}) is a saddle, representing matter dominated solutions, and the line C(Ωr)C(\Omega_{r}) contains the past attractors, which represents radiation dominated solutions.

4.2.1 Global dynamical systems formulation

In this section we define the compact variable (assuming H0,H0>0H\geq 0,{H_{0}}>0) based on the approach by [56]:

T=H0H0+H,T=\frac{{H_{0}}}{{H_{0}}+H}, (4.37)

along with the angular ones

θ1=tan1(8πGρmΛ),θ2=tan1(8πGρrΛ),\theta_{1}=\tan^{-1}\left(\sqrt{\frac{8\pi G\rho_{m}}{\Lambda}}\right),\quad\theta_{2}=\tan^{-1}\left(\sqrt{\frac{8\pi G\rho_{r}}{\Lambda}}\right), (4.38)

with inverse

H=H0(1T)T,ρm=Λtan2(θ1)8πG,ρr=Λtan2(θ2)8πG.H=\frac{H_{0}(1-T)}{T},\quad\rho_{m}=\frac{\Lambda\tan^{2}(\theta_{1})}{8\pi G},\quad\rho_{r}=\frac{\Lambda\tan^{2}(\theta_{2})}{8\pi G}. (4.39)

Furthermore, we have

β=(2Δ)ΛT2(tan2(θ1)+tan2(θ2)+1)(H0(1T1))Δ3(Δ+2)H02(1T)2,\beta=\frac{(2-\Delta)\Lambda T^{2}\left(\tan^{2}(\theta_{1})+\tan^{2}(\theta_{2})+1\right)\left({H_{0}}\left(\frac{1}{T}-1\right)\right)^{\Delta}}{3(\Delta+2){H_{0}}^{2}(1-T)^{2}}, (4.40)

and

q=1+3tan2(θ1)+4tan2(θ2)(2Δ)(tan2(θ1)+tan2(θ2)+1)q=-1+\frac{3\tan^{2}(\theta_{1})+4\tan^{2}(\theta_{2})}{(2-\Delta)\left(\tan^{2}(\theta_{1})+\tan^{2}(\theta_{2})+1\right)} (4.41)

We obtain the dynamical system

dTdτ¯=(1T)2T(3tan2(θ1)+4tan2(θ2))(2Δ)(tan2(θ1)+tan2(θ2)+1),\displaystyle\frac{dT}{d\bar{\tau}}=\frac{(1-T)^{2}T\left(3\tan^{2}(\theta_{1})+4\tan^{2}(\theta_{2})\right)}{(2-\Delta)\left(\tan^{2}(\theta_{1})+\tan^{2}(\theta_{2})+1\right)},
dθ1dτ¯=34(1T)sin(2θ1),\displaystyle\frac{d\theta_{1}}{d\bar{\tau}}=-\frac{3}{4}(1-T)\sin(2\theta_{1}),
dθ2dτ¯=(1T)sin(2θ2),\displaystyle\frac{d\theta_{2}}{d\bar{\tau}}=-(1-T)\sin(2\theta_{2}), (4.42)

where for any function f{T,θ1,θ2}f\in\{T,\theta_{1},\theta_{2}\} we have introduced the new derivative

dfdτ¯=1(H0+H)dfdt,\frac{df}{d\bar{\tau}}=\frac{1}{({H_{0}}+H)}\frac{df}{dt},

which allows for a global dynamical system analysis.

Using the logarithmic variable τ=ln(a)\tau=\ln(a), we get the complementary system

dTdτ=(1T)T(3tan2(θ1)+4tan2(θ2))(2Δ)(tan2(θ1)+tan2(θ2)+1),\displaystyle\frac{dT}{d{\tau}}=\frac{(1-T)T\left(3\tan^{2}(\theta_{1})+4\tan^{2}(\theta_{2})\right)}{(2-\Delta)\left(\tan^{2}(\theta_{1})+\tan^{2}(\theta_{2})+1\right)},
dθ1dτ=34sin(2θ1),\displaystyle\frac{d\theta_{1}}{d{\tau}}=-\frac{3}{4}\sin(2\theta_{1}),
dθ2dτ=sin(2θ2).\displaystyle\frac{d\theta_{2}}{d{\tau}}=-\sin(2\theta_{2}). (4.43)

There exist three classes of equilibrium points/lines: dSdS, RR, and MM. The deceleration parameter qq evaluated at the lines dSdS is q=1q=-1, thus, it denotes the de Sitter solutions. Evaluating qq at the points RR and MM we have q=1+4(2Δ)q=-1+\frac{4}{(2-\Delta)} or q=1+32Δq=-1+\frac{3}{2-\Delta}, respectively; i.e. for Δ=0\Delta=0 they are associated with radiation-dominated and with dust fluid solutions, respectively.

Label Coordinates Eigenvalues Stability
dS++dS_{++} {θ1=2nπ,θ2=2mπ}\{\theta_{1}=2n\pi,\theta_{2}=2m\pi\} {32,2,0}\left\{-\frac{3}{2},-2,0\right\} stable
dS+dS_{+-} {θ1=2nπ,θ2=(2m+1)π}\{\theta_{1}=2n\pi,\theta_{2}=(2m+1)\pi\} {32,2,0}\left\{-\frac{3}{2},-2,0\right\} stable
dS+dS_{-+} {θ1=(2n+1)π,θ2=2mπ}\{\theta_{1}=(2n+1)\pi,\theta_{2}=2m\pi\} {32,2,0}\left\{-\frac{3}{2},-2,0\right\} stable
dSdS_{--} {θ1=(2n+1)π,θ2=(2m+1)π}\{\theta_{1}=(2n+1)\pi,\theta_{2}=(2m+1)\pi\} {32,2,0}\left\{-\frac{3}{2},-2,0\right\} stable
R+±(0)R_{+\pm}^{(0)} {T=0,θ1=2nπ,θ2=12(4m±1)π}\left\{T=0,\theta_{1}=2n\pi,\theta_{2}=\frac{1}{2}(4m\pm 1)\pi\right\} {32,2,42Δ}\left\{-\frac{3}{2},2,\frac{4}{2-\Delta}\right\} saddle
R±(0)R_{-\pm}^{(0)} {T=0,θ1=(2n+1)π,θ2=12(4m±1)π}\left\{T=0,\theta_{1}=(2n+1)\pi,\theta_{2}=\frac{1}{2}(4m\pm 1)\pi\right\} {32,2,42Δ}\left\{-\frac{3}{2},2,\frac{4}{2-\Delta}\right\} saddle
R+±(1)R_{+\pm}^{(1)} {T=1,θ1=2nπ,θ2=12(4m±1)π}\left\{T=1,\theta_{1}=2n\pi,\theta_{2}=\frac{1}{2}(4m\pm 1)\pi\right\} {32,2,42Δ}\left\{-\frac{3}{2},2,-\frac{4}{2-\Delta}\right\} saddle
R±(1)R_{-\pm}^{(1)} {T=1,θ1=(2n+1)π,θ2=12(4m±1)π}\left\{T=1,\theta_{1}=(2n+1)\pi,\theta_{2}=\frac{1}{2}(4m\pm 1)\pi\right\} {32,2,42Δ}\left\{-\frac{3}{2},2,-\frac{4}{2-\Delta}\right\} saddle
M±+(0)M_{\pm+}^{(0)} {T=0,θ1=12(4n±1)π,θ2=2mπ}\left\{T=0,\theta_{1}=\frac{1}{2}(4n\pm 1)\pi,\theta_{2}=2m\pi\right\} {32,2,42Δ}\left\{\frac{3}{2},-2,\frac{4}{2-\Delta}\right\} saddle
M±(0)M_{\pm-}^{(0)} {T=0,θ1=12(4n±1)π,θ2=(2m+1)π}\left\{T=0,\theta_{1}=\frac{1}{2}(4n\pm 1)\pi,\theta_{2}=(2m+1)\pi\right\} {32,2,42Δ}\left\{\frac{3}{2},-2,\frac{4}{2-\Delta}\right\} saddle
M±+(1)M_{\pm+}^{(1)} {T=1,θ1=12(4n±1)π,θ2=2mπ}\left\{T=1,\theta_{1}=\frac{1}{2}(4n\pm 1)\pi,\theta_{2}=2m\pi\right\} {32,2,42Δ}\left\{\frac{3}{2},-2,-\frac{4}{2-\Delta}\right\} saddle
M±(1)M_{\pm-}^{(1)} {T=1,θ1=12(4n±1)π,θ2=(2m+1)π}\left\{T=1,\theta_{1}=\frac{1}{2}(4n\pm 1)\pi,\theta_{2}=(2m+1)\pi\right\} {32,2,42Δ}\left\{\frac{3}{2},-2,-\frac{4}{2-\Delta}\right\} saddle
Table 3: Equilibrium points/lines of system (4.43).

The equilibrium points/lines of system (4.43) are summarized in table 3. The label dS++dS_{++} means that θ1\theta_{1} and θ2\theta_{2} are both even multiples of π\pi; dS+dS_{+-} means that θ1\theta_{1} is an even multiple of π\pi and θ2\theta_{2} is an odd multiple of π\pi, and so on. The left sign in kernel RR is ++ if θ1\theta_{1} is an even multiple of π\pi, and - if it is odd multiple of π\pi. The right sign in kernel RR is ++ if θ2\theta_{2} is co-terminal of π2\frac{\pi}{2}, and - if it is co-terminal of π2-\frac{\pi}{2}. For kernel MM, the left sign is ++ if θ1\theta_{1} is co-terminal of π2\frac{\pi}{2}, and - if it is co-terminal of π2-\frac{\pi}{2}, whereas the right sign in kernel MM is ++ if θ2\theta_{2} is an even multiple of π\pi, and - if it is odd multiple of π\pi. For MM, RR- points, the upper indexes are (0){(0)} or (1){(1)} depending on whether T=0T=0 or T=1T=1.

As summarized in table 3, we found three classes of equilibrium points/lines:

  1. 1.

    the family dSdS, which comprises the lines of equilibrium points dS++dS_{++}, dS+dS_{+-}, dS+dS_{-+} and dSdS_{--}. They represent the de Sitter solutions and are stable.

  2. 2.

    The family RR, which encompass the equilibrium points R+±(0)R_{+\pm}^{(0)}, R±(0)R_{-\pm}^{(0)}, R+±(1)R_{+\pm}^{(1)} and R±(1)R_{-\pm}^{(1)}. For Δ=0\Delta=0, they are associated to radiation-dominated solutions and are saddles.

  3. 3.

    The family MM, which contains the equilibrium points M±+(0)M_{\pm+}^{(0)}, M±(0)M_{\pm-}^{(0)}, M±+(1)M_{\pm+}^{(1)} and M±(1)M_{\pm-}^{(1)}. For Δ=0\Delta=0, they are associated with dust fluid solutions and are saddles.

Using E:=HH0=1TTE:=\frac{H}{H_{0}}=\frac{1-T}{T} we obtain

E=E[3tan2(θ1)+4tan2(θ2)(2Δ)(tan2(θ1)+sec2(θ2))].E^{\prime}=-E\left[\frac{3\tan^{2}(\theta_{1})+4\tan^{2}(\theta_{2})}{(2-\Delta)\left(\tan^{2}(\theta_{1})+\sec^{2}(\theta_{2})\right)}\right]. (4.44)

This implies that EE is a monotonic decreasing function. According to the monotonicity principle, the late time attractors satisfy T=1T=1, whereas the early time attractors satisfy T=0T=0. For a representation of the flow of (4.43), we integrate in the variables T,θ1,θ2T,\theta_{1},\theta_{2} and project in a compact set using the “torus-adapted” coordinates

𝐓1:{x=cosθ1(2+Tcosθ2),y=sinθ1(2+Tcosθ2),z=Tsinθ2,\mathbf{T}^{1}:\begin{cases}x=\cos\theta_{1}(2+T\cos\theta_{2}),\\ y=\sin\theta_{1}(2+T\cos\theta_{2}),\\ z=T\sin\theta_{2},\end{cases} (4.45)

with 0T1,θ1,θ2[π,π]0\leq T\leq 1,\theta_{1},\theta_{2}\in[-\pi,\pi], with inverse

{θ1=tan1(yx),θ2=tan1(zx2+y22),T=(x2+y22)2+z2.\begin{cases}\theta_{1}=\tan^{-1}\left(\frac{y}{x}\right),\\ \theta_{2}=\tan^{-1}\left(\frac{z}{\sqrt{x^{2}+y^{2}}-2}\right),\\ T=\sqrt{\left(\sqrt{x^{2}+y^{2}}-2\right)^{2}+z^{2}}.\end{cases} (4.46)
Refer to caption
Figure 6: Unwrapped solution space (left panel) projected both onto the plane θ1,θ2\theta_{1},\theta_{2} and the torus 𝐓1\mathbf{T}^{1} given in Cartesian coordinates by (4.45) (right panel) of the solution space of system (4.43) (in the invariant set T=1T=1) for the cases Δ=6.245×104\Delta=6.245\times 10^{-4} (top panels), and Δ=1\Delta=1 (bottom panels).

In addition, we present the whole evolution in the space (Ωm,Ωr,T)(\Omega_{m},\Omega_{r},T) through the transform (T,θ1,θ2)(Ωm,Ωr,T)(T,\theta_{1},\theta_{2})\mapsto(\Omega_{m},\Omega_{r},T) where

(Ωm,Ωr)\displaystyle\left(\Omega_{m},\Omega_{r}\right) =[(2+Δ2Δ)1β¯Ωm0Ωr0]T2(1T)2(tan2(θ1),tan2(θ2)).\displaystyle=\left[\left(\frac{2+\Delta}{2-\Delta}\right)\frac{1}{\bar{\beta}}-\Omega_{m0}-\Omega_{r0}\right]\frac{T^{2}}{(1-T)^{2}}\left(\tan^{2}(\theta_{1}),\tan^{2}(\theta_{2})\right). (4.47)

The case T=1/2T=1/2 corresponds to current time. Using these variables we have the system

dΩmdτ=Ωm(2(1T)2β¯(3Ωm+4Ωr)(Δ2)β¯((1T)2ΩmT(T(Ωm0Ωr+Ωr0)+2Ωr)+Ωr)(Δ+2)T2+3),\displaystyle\frac{d\Omega_{m}}{d\tau}=-\Omega_{m}\left(\frac{2(1-T)^{2}\bar{\beta}\left(3\Omega_{m}+4\Omega_{r}\right)}{(\Delta-2)\bar{\beta}\left((1-T)^{2}\Omega_{m}-T\left(T\left(\Omega_{m0}-\Omega_{r}+\Omega_{r0}\right)+2\Omega_{r}\right)+\Omega_{r}\right)-(\Delta+2)T^{2}}+3\right),
dΩrdτ=2Ωr((1T)2β¯(3Ωm+4Ωr)(Δ2)β¯((1T)2ΩmT(T(Ωm0Ωr+Ωr0)+2Ωr)+Ωr)(Δ+2)T2+2),\displaystyle\frac{d\Omega_{r}}{d\tau}=-2\Omega_{r}\left(\frac{(1-T)^{2}\bar{\beta}\left(3\Omega_{m}+4\Omega_{r}\right)}{(\Delta-2)\bar{\beta}\left((1-T)^{2}\Omega_{m}-T\left(T\left(\Omega_{m0}-\Omega_{r}+\Omega_{r0}\right)+2\Omega_{r}\right)+\Omega_{r}\right)-(\Delta+2)T^{2}}+2\right),
dTdτ=(1T)3Tβ¯(3Ωm+4Ωr)(Δ2)β¯((1T)2ΩmT(T(Ωm0Ωr+Ωr0)+2Ωr)+Ωr)(Δ+2)T2.\displaystyle\frac{dT}{d\tau}=-\frac{(1-T)^{3}T\bar{\beta}\left(3\Omega_{m}+4\Omega_{r}\right)}{(\Delta-2)\bar{\beta}\left((1-T)^{2}\Omega_{m}-T\left(T\left(\Omega_{m0}-\Omega_{r}+\Omega_{r0}\right)+2\Omega_{r}\right)+\Omega_{r}\right)-(\Delta+2)T^{2}}. (4.48)
Refer to caption
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Figure 7: Streamlines of the flow of (4.48) for (a) Δ=6.245×104,β¯=0.915,Ωm0=0.311,Ωr0=9×105\Delta=6.245\times 10^{-4},\bar{\beta}=0.915,\Omega_{m0}=0.311,\Omega_{r0}=9\times 10^{-5} obtained from the joint constraints and (b) Δ=0,β¯=1,Ωm0=0.311,Ωr0=9×105\Delta=0,\bar{\beta}=1,\Omega_{m0}=0.311,\Omega_{r0}=9\times 10^{-5} for Λ\LambdaCDM model.

In Figure 6 are represented streamlines of the flow of (4.43) onto the unwrapped solution space (left panel) projected both onto the plane θ1,θ2\theta_{1},\theta_{2} and the torus 𝐓1\mathbf{T}^{1}, setting T=1T=1 (right panel) of the solution space of system (4.43) for the joint constraint value Δ=6.245×104\Delta=6.245\times 10^{-4}, and the extreme value Δ=1\Delta=1, respectively.

The results summarized in points 1-3 above are confirmed in Figure 6. That is, the lines of equilibrium points dS++dS_{++}, dS+dS_{+-}, dS+dS_{-+} and dSdS_{--} (the family dSdS), denoting the de Sitter solutions, are stable. The equilibrium points R+±(0)R_{+\pm}^{(0)}, R±(0)R_{-\pm}^{(0)}, R+±(1)R_{+\pm}^{(1)} and R±(1)R_{-\pm}^{(1)} (the family RR), associated to radiation dominated solutions for Δ=0\Delta=0, are saddles. Finally, the equilibrium points M±+(0)M_{\pm+}^{(0)}, M±(0)M_{\pm-}^{(0)}, M±+(1)M_{\pm+}^{(1)} and M±(1)M_{\pm-}^{(1)} (the family MM), associated to matter dominated solutions for Δ=0\Delta=0, are saddles.

In Figure 7 streamlines of the flow of (4.48) are presented. We select the values (a) Δ=6.245×104,β¯=0.915,Ωm0=0.311,Ωr0=9×105\Delta=6.245\times 10^{-4},\bar{\beta}=0.915,\Omega_{m0}=0.311,\Omega_{r0}=9\times 10^{-5} obtained from the joint constraints, and (b) Δ=0,β¯=1,Ωm0=0.311,Ωr0=9×105\Delta=0,\bar{\beta}=1,\Omega_{m0}=0.311,\Omega_{r0}=9\times 10^{-5} for Λ\LambdaCDM model.

Figure 7 shows, in a phase space, a crucial difference of Barrow Entropy Cosmology (top panel) and Λ\LambdaCDM (bottom panel) related to the early universe. Barrow Entropy Cosmology does not admits a late-time radiation dominated phase (past attractor) and the solutions emerges from the point (Ωr,Ωm,T)=(0,0,0)(\Omega_{r},\Omega_{m},T)=(0,0,0) representing an effective DE- dominated early time attractor. However, both theories have the same late time dynamics, that is, the dominance of a de Sitter phase.

Complementary, we define an unbounded variable T~\tilde{T} and keep θ1,θ2\theta_{1},\theta_{2}:

T~=H0H,θ1=tan1(8πGρmΛ),θ2=tan1(8πGρrΛ),\tilde{T}=\frac{H_{0}}{H},\quad\theta_{1}=\tan^{-1}\left(\sqrt{\frac{8\pi G\rho_{m}}{\Lambda}}\right),\quad\theta_{2}=\tan^{-1}\left(\sqrt{\frac{8\pi G\rho_{r}}{\Lambda}}\right), (4.49)

and using the logarithmic variable τ=ln(a)=ln(1+z)\tau=\ln(a)=-\ln(1+z), we obtain the complementary system

dT~dτ=T~(3tan2(θ1)+4tan2(θ2))(2Δ)(tan2(θ1)+tan2(θ2)+1),\displaystyle\frac{d\tilde{T}}{d{\tau}}=\frac{\tilde{T}\left(3\tan^{2}(\theta_{1})+4\tan^{2}(\theta_{2})\right)}{(2-\Delta)\left(\tan^{2}(\theta_{1})+\tan^{2}(\theta_{2})+1\right)},
dθ1dτ=34sin(2θ1),\displaystyle\frac{d\theta_{1}}{d{\tau}}=-\frac{3}{4}\sin(2\theta_{1}),
dθ2dτ=sin(2θ2).\displaystyle\frac{d\theta_{2}}{d{\tau}}=-\sin(2\theta_{2}). (4.50)

Setting a=1a=1 for the current universe, and considering the initial conditions:

θ1(0)=tan1(Ωm0ΩΛ0),θ2(0)=tan1(Ωr0ΩΛ0),T~(0)=1,\theta_{1}(0)=\tan^{-1}\left(\sqrt{\frac{\Omega_{m0}}{\Omega_{\Lambda 0}}}\right),\quad\theta_{2}(0)=\tan^{-1}\left(\sqrt{\frac{\Omega_{r0}}{\Omega_{\Lambda 0}}}\right),\quad\tilde{T}(0)=1, (4.51)

the system (4.2.1) is integrated to obtain

θ1(τ)=tan1(e3τ/2Ωm0ΩΛ0),\displaystyle\theta_{1}(\tau)=\tan^{-1}\left(e^{-3\tau/2}\sqrt{\frac{\Omega_{m0}}{\Omega_{\Lambda 0}}}\right), (4.52)
θ2(τ)=tan1(e2τΩr0ΩΛ0),\displaystyle\theta_{2}(\tau)=\tan^{-1}\left(e^{-2\tau}\sqrt{\frac{\Omega_{r0}}{\Omega_{\Lambda 0}}}\right), (4.53)
T~(τ)=e4τΔ2(ΩΛ0+Ωm0+Ωr0ΩΛ0)12Δ(e4τΩΛ0+eτΩm0+Ωr0ΩΛ0)1Δ2.\displaystyle\tilde{T}(\tau)=e^{-\frac{4\tau}{\Delta-2}}\left(\frac{\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}}{\Omega_{\Lambda 0}}\right)^{\frac{1}{2-\Delta}}\left(\frac{e^{4\tau}\Omega_{\Lambda 0}+e^{\tau}\Omega_{m0}+\Omega_{r0}}{\Omega_{\Lambda 0}}\right)^{\frac{1}{\Delta-2}}. (4.54)

Finally, we work out the exact evolution of HH, ρm\rho_{m} and ρr\rho_{r}:

H\displaystyle H =H0(ΩΛ0+e3τΩm0+e4τΩr0ΩΛ0+Ωm0+Ωr0)12Δ\displaystyle=H_{0}\left(\frac{\Omega_{\Lambda 0}+e^{-3\tau}\Omega_{m0}+e^{-4\tau}\Omega_{r0}}{\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}}\right)^{\frac{1}{2-\Delta}}
=H0(ΩΛ0+Ωm0(1+z)3+Ωr0(1+z)4ΩΛ0+Ωm0+Ωr0)12Δ,\displaystyle=H_{0}\left(\frac{\Omega_{\Lambda 0}+\Omega_{m0}(1+z)^{3}+\Omega_{r0}(1+z)^{4}}{\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}}\right)^{\frac{1}{2-\Delta}}, (4.55)
ρm\displaystyle\rho_{m} =Λtan2(θ1)8πG=Λe3τΩm08πGΩΛ0=3H02Ωm08πG(z+1)3,\displaystyle=\frac{\Lambda\tan^{2}(\theta_{1})}{8\pi G}=\frac{\Lambda e^{-3\tau}\Omega_{m0}}{8\pi G\Omega_{\Lambda 0}}=\frac{3H_{0}^{2}\Omega_{m0}}{8\pi G}(z+1)^{3}, (4.56)
ρr\displaystyle\rho_{r} =Λtan2(θ2)8πG=Λe4τΩr08πGΩΛ0=3H02Ωr08πG(z+1)4.\displaystyle=\frac{\Lambda\tan^{2}(\theta_{2})}{8\pi G}=\frac{\Lambda e^{-4\tau}\Omega_{r0}}{8\pi G\Omega_{\Lambda 0}}=\frac{3H_{0}^{2}\Omega_{r0}}{8\pi G}(z+1)^{4}. (4.57)

These expressions are used to calculate the fractional energy densities corresponding to matter, radiation, and a Λ\Lambda-like source as follows:

Ωm(z)=8πGρm3H2=Ωm0(z+1)3(ΩΛ0+Ωm0(1+z)3+Ωr0(1+z)4ΩΛ0+Ωm0+Ωr0)22Δ,\Omega_{m}(z)=\frac{8\pi G\rho_{m}}{3H^{2}}=\Omega_{m0}(z+1)^{3}\left(\frac{\Omega_{\Lambda 0}+\Omega_{m0}(1+z)^{3}+\Omega_{r0}(1+z)^{4}}{\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}}\right)^{-\frac{2}{2-\Delta}}, (4.58)
Ωr(z)=8πGρm3H2=Ωr0(z+1)4(ΩΛ0+Ωm0(1+z)3+Ωr0(1+z)4ΩΛ0+Ωm0+Ωr0)22Δ,\Omega_{r}(z)=\frac{8\pi G\rho_{m}}{3H^{2}}=\Omega_{r0}(z+1)^{4}\left(\frac{\Omega_{\Lambda 0}+\Omega_{m0}(1+z)^{3}+\Omega_{r0}(1+z)^{4}}{\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}}\right)^{-\frac{2}{2-\Delta}}, (4.59)

and

ΩΛ(z)=Λ3H2=ΩΛ0(ΩΛ0+Ωm0(1+z)3+Ωr0(1+z)4ΩΛ0+Ωm0+Ωr0)22Δ,ΩΛ0=Λ3H02.\Omega_{\Lambda}(z)=\frac{\Lambda}{3H^{2}}=\Omega_{\Lambda 0}\left(\frac{\Omega_{\Lambda 0}+\Omega_{m0}(1+z)^{3}+\Omega_{r0}(1+z)^{4}}{\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}}\right)^{-\frac{2}{2-\Delta}},\quad\Omega_{\Lambda 0}=\frac{\Lambda}{3H_{0}^{2}}. (4.60)

From Eq. (2.6) we infer

ΩDE(z)=8πGρDE3H2=Λ3H2+[1β(Δ+2)2ΔHΔ]\displaystyle\Omega_{DE}(z)=\frac{8\pi G\rho_{DE}}{3H^{2}}=\frac{\Lambda}{3H^{2}}+\left[1-\frac{\beta(\Delta+2)}{2-\Delta}H^{-\Delta}\right]
=1+ΩΛ0(ΩΛ0+Ωm0(1+z)3+Ωr0(1+z)4ΩΛ0+Ωm0+Ωr0)22Δ\displaystyle=1+\Omega_{\Lambda 0}\left(\frac{\Omega_{\Lambda 0}+\Omega_{m0}(1+z)^{3}+\Omega_{r0}(1+z)^{4}}{\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}}\right)^{-\frac{2}{2-\Delta}}
(Δ+2)(2Δ)1β¯(ΩΛ0+Ωm0(1+z)3+Ωr0(1+z)4ΩΛ0+Ωm0+Ωr0)Δ2Δ\displaystyle-\frac{(\Delta+2)}{(2-\Delta)}\frac{1}{\bar{\beta}}\left(\frac{\Omega_{\Lambda 0}+\Omega_{m0}(1+z)^{3}+\Omega_{r0}(1+z)^{4}}{\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}}\right)^{-\frac{\Delta}{2-\Delta}}
=1+ΩΛ0(ΩΛ0+Ωm0(1+z)3+Ωr0(1+z)4ΩΛ0+Ωm0+Ωr0)22Δ\displaystyle=1+\Omega_{\Lambda 0}\left(\frac{\Omega_{\Lambda 0}+\Omega_{m0}(1+z)^{3}+\Omega_{r0}(1+z)^{4}}{\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}}\right)^{-\frac{2}{2-\Delta}}
(ΩΛ0+Ωm0+Ωr0)(ΩΛ0+Ωm0(1+z)3+Ωr0(1+z)4ΩΛ0+Ωm0+Ωr0)Δ2Δ\displaystyle-\left(\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}\right)\left(\frac{\Omega_{\Lambda 0}+\Omega_{m0}(1+z)^{3}+\Omega_{r0}(1+z)^{4}}{\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}}\right)^{-\frac{\Delta}{2-\Delta}}
=1(Ωm0(1+z)3+Ωr0(1+z)4)(ΩΛ0+Ωm0(1+z)3+Ωr0(1+z)4ΩΛ0+Ωm0+Ωr0)22Δ,\displaystyle=1-\left(\Omega_{m0}(1+z)^{3}+\Omega_{r0}(1+z)^{4}\right)\left(\frac{\Omega_{\Lambda 0}+\Omega_{m0}(1+z)^{3}+\Omega_{r0}(1+z)^{4}}{\Omega_{\Lambda 0}+\Omega_{m0}+\Omega_{r0}}\right)^{-\frac{2}{2-\Delta}}, (4.61)

where we use Eq. (2.26) to eliminate the term (2+Δ2Δ)1β¯\left(\frac{2+\Delta}{2-\Delta}\right)\frac{1}{\bar{\beta}}, recall Δ2Δ=122Δ-\frac{\Delta}{2-\Delta}=1-\frac{2}{2-\Delta}, and algebraically manipulate the equations to obtain ΩDE=1ΩmΩr\Omega_{DE}=1-\Omega_{m}-\Omega_{r}. It is straightforward to obtain Eqs. (4.58), (4.59), (4.60) and (4.2.1) in terms of the scale factor by replacing z=(1/a)1z=(1/a)-1.

Refer to caption
Figure 8: Evolution of the density parameters for matter, radiation, and effective dark energy using the joint constraint of Barrow Cosmology (solid lines) and the values for the standard model Δ=0\Delta=0, and β¯=1\bar{\beta}=1 (dashed lines). The shadow regions represent the 3σ3\sigma confidence levels.

Figure 8 shows the evolution of the density parameters Ωm\Omega_{m}, Ωr\Omega_{r} and ΩDE\Omega_{DE} vs the scale factor aa for two cases: the joint constraints for hh, Ωm0\Omega_{m0}, Δ\Delta and β¯\bar{\beta} shown in Table 1 (solid lines), and the values for the standard model Δ=0\Delta=0, β¯=1\bar{\beta}=1 (dashed lines). We estimate Ωr09×105\Omega_{r0}\sim 9\times 10^{-5} consistent with the CMB data [2]. The shadowed regions represent the 3σ3\sigma confidence levels. It is worthy to note that there are values of the energy densities which satisfy Ωm>1\Omega_{m}>1, Ωr>1\Omega_{r}>1, and ΩDE<0\Omega_{DE}<0, however, these values are close to Λ\LambdaCDM lines within the 3σ3\sigma error propagation.

5 Summary and discussion

Barrow entropy cosmology is a recent model [20] based on the modification of the entropy-area black hole relation proposed by Barrow [19] that involves a new parameter Δ\Delta, recovering the standard form of the Bekenstein entropy for Δ=0\Delta=0. Considering this new relation, the modified Friedmann equations governing the dynamics of the Universe can be obtained from the gravity-thermodynamics approach. These new equations contain two parameters Δ\Delta, and β¯\bar{\beta} (where the standard model is recovered for Δ=0\Delta=0 and β¯=1\bar{\beta}=1) and could source the cosmic acceleration at late times. We investigate two Barrow cosmological models: I) Universe filled only by a matter component and II) Universe filled by matter and radiation components. Furthermore, we divide the study of Barrow proposition in two ways: an observational approach and a dynamical system stability analysis.

For the first approach we constrained the free parameters Δ\Delta, hh, and Ωm0\Omega_{m0}, for both cosmological models, employing the observational Hubble data, type Ia supernovae, HII galaxies, strong lensing systems, baryon acoustic oscillations, and a joint analysis of these samples. We provide the observational constraints in section 3 (see table 1), showing that for the model I the Barrow parameters are Δ=(5.9123.112+3.353)×104\Delta=(5.912^{+3.353}_{-3.112})\times 10^{-4}, β¯=0.9200.042+0.042\bar{\beta}=0.920^{+0.042}_{-0.042}, and for the model II Δ=(6.2453.164+3.377)×104\Delta=(6.245^{+3.377}_{-3.164})\times 10^{-4}, β¯=0.9150.043+0.043\bar{\beta}=0.915^{+0.043}_{-0.043}. For both models these constraints are consistent at 2σ2\sigma with both the standard cosmological model and the standard entropy-area entropy relation. By reconstructing the cosmic expansion rate using the joint constraints in both cosmologies, we found consistency with the observational Hubble data. In addition, for the more realistic model with matter and radiation components, we calculated the deceleration parameter and obtained a transition at zt0.7110.034+0.035z_{t}\simeq 0.711^{+0.035}_{-0.034} from a decelerated stage to an accelerated stage with q0=0.5730.019+0.019q_{0}=-0.573^{+0.019}_{-0.019}, suggesting a de Sitter solution. We also confirm that, under these cosmologies, the equation of state of the effective dark energy can undergo from a quintessence-like regime to a phantom-like one as found by [20], yielding wDE(0)1.0001340.000068+0.000069w_{DE}(0)\simeq-1.000134^{+0.000069}_{-0.000068} at current times which is consistent with the cosmological constant at 1σ1\sigma. Furthermore, we estimated the age of the Universe as t014.0620.170+0.179t_{0}\simeq 14.062^{+0.179}_{-0.170} Gyr, consistent within 2σ2\sigma confidence level with the measurements of Planck [2].

The second approach, the stability analysis, allowed to find regions on the parameter space where the different cosmic epochs take place. In this regard, we obtained a qualitative description of the local and global dynamics of both cosmological scenarios, irrespective of the initial conditions and the specific evolution of the universe. Moreover, we have found asymptotic solutions calculated various theoretical values for the observable quantities that can be compared with previous observational constraints. From the analysis at the finite region of the phase space in the model I, we have found the line A(ΩΛ)A(\Omega_{\Lambda}) of equilibrium points, which is is the attractor of the system and represents the de Sitter solutions. For Δ=0\Delta=0, the line B(Ωm)B(\Omega_{m}) contains the past attractors, which represents the matter dominated solutions. Additionally, we have defined the compact variables (assuming H0,H0>0H\geq 0,H_{0}>0) based on the approach by [56]. We have found two equivalent (due to the discrete symmetry) hyperbolic fixed points M±M_{\pm} associated with dust fluid for Δ=0\Delta=0, and two equivalent fixed points dS±dS_{\pm} corresponding to the de Sitter states (see Table 2). On the other hand, in the model II, the line A(ΩΛ)A(\Omega_{\Lambda}) is the attractor of the system and represents the de Sitter solutions. For Δ=0\Delta=0, the line B(Ωm)B(\Omega_{m}) is a saddle, indicating the matter dominated solutions, while the line C(Ωr)C(\Omega_{r}) contains the past attractors and specify the radiation dominated solutions. Finally, we found three classes of equilibrium points/ lines: dSdS, RR and MM; with dSdS denoting the de Sitter solutions, and for Δ=0\Delta=0, RR and MM are the radiation-dominated and dust fluid solutions, respectively (see Table 3).

For both models we reconstruct the evolution of the density parameters Ωm\Omega_{m}, Ωr\Omega_{r}, and ΩDE\Omega_{DE} as a function of the scale factor aa for two cases: using the joint constraints for hh, Ωm0\Omega_{m0}, Δ\Delta and β¯\bar{\beta}, and the values for the standard model Δ=0\Delta=0, β¯=1\bar{\beta}=1 (see Figs. 5 and 8). We found that at the early times there are values of the energy densities which satisfy Ωm>1\Omega_{m}>1, Ωr>1\Omega_{r}>1, and ΩDE<0\Omega_{DE}<0. However, these values are close to Λ\LambdaCDM lines within the 3σ3\sigma error propagation. Thus, with more and high precision cosmological data, these non-physical density parameter values could be avoided.

A crucial difference of Barrow Entropy Cosmology and the standard Λ\LambdaCDM model is related to the early universe. Barrow Entropy Cosmology does not admits a late-time radiation dominated phase and the solutions are past asymptotic to a point representing an effective DE- dominated early time attractor. However, both theories have the same late time dynamics, that is, the dominance of a de Sitter phase. In summary, we have showed, from several points of view, that the dynamical equations have a de Sitter solution at late times but the dynamics at early times is not consistent with the evolution of the standard cosmological model.

Acknowledgments

The authors are grateful for the figure 7 provided by Alfredo D. Millano (PhD student at Universidad Católica del Norte (UCN)). G.L. was funded by Agencia Nacional de Investigación y Desarrollo - ANID for financial support through the program FONDECYT Iniciación grant no. 11180126 and by Vicerrectoría de Investigación y Desarrollo Tecnológico at UCN. J.M. acknowledges the support from ANID project Basal AFB-170002 and ANID REDES 190147. M.A.G.-A. acknowledges support from SNI-México, CONACyT research fellow, ANID REDES (190147), COZCyT and Instituto Avanzado de Cosmología (IAC). A.H.A. thanks to the PRODEP project, Mexico for resources and financial support and thanks also to the support from Luis Aguilar, Alejandro de León, Carlos Flores, and Jair García of the Laboratorio Nacional de Visualización Científica Avanzada. V.M. acknowledges support from Centro de Astrofísica de Valparaíso and ANID REDES 190147.

References