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Science potential for stellar-mass black holes as neighbours of Sgr A*

Shammi Tahura [email protected] Department of Physics, University of Guelph, 50 Stone Road E., Guelph, ON N1G 2W1, Canada Perimeter Institute for Theoretical Physics, Waterloo, ON N2L 2Y5, Canada    Zhen Pan Perimeter Institute for Theoretical Physics, Waterloo, ON N2L 2Y5, Canada    Huan Yang [email protected] Department of Physics, University of Guelph, 50 Stone Road E., Guelph, ON N1G 2W1, Canada Perimeter Institute for Theoretical Physics, Waterloo, ON N2L 2Y5, Canada
Abstract

It has been suggested that there is possibly a class of stellar-mass black holes (BHs) residing near (distance 103M\leq 10^{3}M) the galactic center massive black hole, Sgr A*. Possible formation scenarios include the mass segregation of massive stellar-mass black holes and/or the disk migration if there was an active accretion flow near Sgr A* within 𝒪(10)\mathcal{O}(10) Myr. In this work, we explore the application of this type of objects as sources of space-borne gravitational wave detectors, such as Laser Interferometer Space Antenna (LISA). We find it is possible to probe the spin of Sgr A* based on the precession of the orbital planes of these stellar-mass black holes moving around Sgr A*. We also show that the dynamical friction produced by accumulated cold dark matter near Sgr A* generally produces small measurable phase shift in the gravitational waveform. In the case that there is an axion cloud near Sgr A*, the dynamical friction induced modification to gravitational waveform is measurable only if the mass of the axion field is in a narrow range of the mass spectrum. Gravitational interaction between the axion cloud and the stellar-mass black holes may introduce additional precession around the spin of Sgr A*. This additional precession rate is generally weaker than the spin-induced Lense-Thirring precession rate, but nevertheless may contaminate the spin measurement in a certain parameter regime. At last, we point out that the multi-body gravitational interaction between these stellar-mass black holes generally causes negligible phase shift during the LISA lifetime.

I Introduction

In the past years there were exciting revolutions in probing astrophysical black holes in the strong-gravity regime, thanks to the observations by the LIGO and the Virgo collaboration (the LVC) Abbott et al. (2021a, b, c, 2019) and EHT (Event Horizon Telescope) Akiyama et al. (2019a, b). In the next decades, space-based gravitational wave (GW) detectors, such as LISA Amaro-Seoane et al. (2017) and Tianqin Luo et al. (2016); Mei et al. (2021), will enable unprecedented measurements on the mass, spin, spacetime, orbital, and environmental properties of massive black holes at cosmological distances Glampedakis and Babak (2006); Barack and Cutler (2007). For example, one particularly interesting type of source is EMRI (extreme mass ratio inspirals), which often comprises a stellar-mass black hole orbiting around a massive black hole. As this kind of system usually stays within the LISA band for 10410510^{4}-10^{5} cycles during the observation period, small additional effects (e.g., extra channel of dissipation) may accumulate over many orbital cycles to generate measurable phase shifts. As a result, EMRIs may serve as an ideal probe for deviations from General Relativity Hannuksela et al. (2019); Zhang and Yang (2020, 2019); Glampedakis and Babak (2006); Barack and Cutler (2007) and astrophysical environmental effects Bonga et al. (2019); Yang et al. (2019); Yang and Casals (2017); Barausse et al. (2014). In addition, the formation of EMRIs may be greatly accelerated by accretion flows, which provides promising opportunities for multi-messenger observations Pan and Yang (2021); Pan et al. (2021a).

There is one special massive black hole (MBH), Sgr A*, which resides at the center of our own galaxy, with distance of orders of magnitude closer than any other massive black holes. The chance of forming an ordinary EMRI around Sgr A* during the LISA observation period is negligible (106\lesssim 10^{-6} from the loss-cone formation channel with EMRI rate 102Gyr1\sim 10^{2}\ {\rm Gyr}^{-1} per MBH Amaro-Seoane and Preto (2011); Babak et al. (2017); Amaro-Seoane (2018, 2020)). However, because of the small distance between Sgr A* and earth, it is still possible to probe stellar-mass black holes at the lower end of the LISA frequency band (105\geq 10^{-5}Hz), corresponding to orbital radius 102M\leq 10^{2}M Naoz et al. (2020), where MM is the gravitational radius of the MBH. On the other hand, there are in fact multiple ways to produce such low-frequency EMRIs (referred as “Sgr A* EMRI” hereafter). For example, it has been suggested that if there is a massive subclass of stellar-mass black holes in the galactic nuclear cluster, the mass segregation effect will lead to condensation of these black holes at galactic centers, with distances 𝒪(102)M\mathcal{O}(10^{2})M away from Sgr A* Emami and Loeb (2020, 2021). In addition, if there is a previous active accretion phase in Sgr A*, as supported by the presence of stellar disk near Sgr A* Levin and Beloborodov (2003), the disk-assisted migration tend to lead to a set of stellar-mass black holes accumulating at distances between 80M200M\sim 80M-200M depending on the disk models and parameters Gilbaum and Stone (2021); Pan and Yang (2021); Pan et al. (2021b), as required by equating the disk migration timescale with the gravitational wave radiation timescale. Frequencies of GWs from such Sgr A* EMRIs are within the range of [.52]×105[.5-2]\times 10^{-5} Hz, considering circular orbits. If the time that the latest accretion episode ended is not earlier than 𝒪(107)\mathcal{O}(10^{7}) years, we still expect some black holes have not merged with Sgr A* after the gravitational wave radiation-induced inspiral, as another way of forming Sgr A* EMRIs at present. Notice that gravitational wave measurement will likely be the only way to probe Sgr A* EMRIs if they do exist.

Assuming the presence of Sgr A* EMRIs, it is natural to ask what is the detectability of these systems using LISA, and what we can learn by observing them. The first question is partially answered by previous works in Gourgoulhon et al. (2019) by computing the event SNR (signal-to-noise ratio) as a function of orbital radius. For the sake of completeness, we present a distribution of SNR with system parameters drawn from Monte-Carlo samplings, assuming the detection by LISA. There is one subtle point worth noticing here: the detection threshold of SNR for such systems should be much smaller than 16\sim 16, which is commonly used as a benchmark value for EMRIs. For Sgr A* EMRIs the template bank contains much less parameters as the sky location and distance of the source is known. Smaller parameter space in the waveform results in smaller penalty in the false-alarm probability, which leads to smaller detection threshold SNR 10\color[rgb]{0,0,0}{\sim 10}.

Our work is primarily focusing on the second question, i.e., the applications of Sgr A* EMRIs. We consider three possible sources that may produce observable effect in the gravitational waveform. The first source is the spin-orbit coupling between Sgr A* and the stellar-mass black hole, which induces Lense-Thirring precession on the orbit. We construct the waveform model to include precession effect and perform the Fisher analysis to address the accuracy of the inferred spin. The result is rather promising: for Sgr A* EMRIs with orbital separation a90Ma\leq 90M, we generally have ΔS/S0.5%24%\color[rgb]{0,0,0}{\Delta S/S\sim 0.5\%-24\%}, with median value at 2%\sim 2\% level. Notice that while we have measurement on the mass of Sgr A* based on the motion of S stars, the spin is completely unknown. In the future we may obtain constraints on the spin using EHT, but based on the experience from the measurement on M87 Tamburini et al. (2020); Bambi et al. (2019), the spin constraint is unlikely to be very stringent. Measuring gravitational waves from Sgr A* EMRIs may be the most accurate way to probe the spin of Sgr A*.

Secondly, we have investigated possible influence of dark matter in the vicinity of Sgr A*. Assuming cold dark matter description with plausible density prescription at galactic center, we find that Sgr A* EMRIs are less capable of probing the effect due to dynamical friction than normal EMRIs, assuming comparable event SNR. On the other hand, if an axion dark matter cloud is excited by black hole superradiance around Sgr A*, considering a typical system configuration, we find the dynamical friction effect is above the measurement noise only if the mass of the axion field is between 3.1×10183.1\times 10^{-18} eV to 3.3×10183.3\times 10^{-18} eV. The chance that the axion mass lies in such narrow range is small. Moreover, in this case the gravitational coupling between the axion cloud and the stellar-mass BH may be strong enough to induce additional precession of the orbit plane which is larger than the measurement uncertainty. This additional precession is generally weaker than the Lense-Thirring precession, but they are degenerate with each other.

Thirdly, we also considered the influence of gravitational interaction between the stellar-mass black holes. As a model problem, we compute the Kozai-Lidov timescale assuming the presence of a nearby third body (stellar-mass black hole), and find it to be much smaller than the observation period of LISA. As a result, we conclude that multi-body effect is not important for Sgr A* EMRIs.

The rest of this article is organized as follows. In section II study the effect of spin induced orbital precession to gravitational waveforms in case of Sgr A* EMRIs and determine the prospect of measuring the spin of Sgr A* with a 10 years observation period of LISA. In section III we explore the prospect of detecting the signature of dark matter cloud from similar observations, focusing on cold dark matter in section III.1 and axion dark matter in III.2. Finally, we discuss the Kozai-Lidov effect in the presence of a third object and present our concluding remarks in section IV. Throughout this paper, we use units in which =c=G=1\hbar=c=G=1.

II Spin induced orbital precession

We begin by assessing the spin induced orbital precession of an Sgr A* EMRI. We will first discuss the gravitational waveform generated by such a binary and the modification to its phase due to orbital precession in Sec. II.1 and Sec. II.2 respectively. Next, we present the data analysis formalism (Fisher analysis) that we implement for the estimation of measurement uncertainties and summarize the results in Sec. II.3. The main results of this section include the threshold SNR for detecting a signal from Sgr A* EMRI with LISA and constraints on various waveform parameters, including the spin of Sgr A*.

II.1 Waveform

We implement the time domain waveform for LISA presented in Ref. Cutler (1998). Following Ref. Cutler (1998), we make use of two sets of Cartesian coordinates– one associated with the detector denoted by (x,y,z)(x,y,z) and the other (x¯,y¯,z¯)(\bar{x},\bar{y},\bar{z}) tied to the ecliptic in a heliocentric frame (see Fig. 1). The corresponding spherical polar coordinates are (θ,ϕ)(\theta,\phi) and (θ¯,ϕ¯)(\bar{\theta},\bar{\phi}) respectively. The detector arms lie in the xyx-y plane and the plane corotates with the detector.

Refer to caption
Figure 1: An illustration of the coordinate systems we use in Sec. II. The set of barred Cartesian coordinates (x¯,y¯,z¯)(\bar{x},\bar{y},\bar{z}) is tied to the eclicptic with the origin at the sun. On the other hand, the unbarred coordinates (x,y,z)(x,y,z) are tied to the detector LISA, with the detector’s arms lying in the xyx-y plane. Angle ϕ¯(t)\bar{\phi}(t) describes the location of the detector with respect to the barred coordinates in x¯y¯\bar{x}-\bar{y} plane. (θ¯s,ϕ¯s)(\bar{\theta}_{s},\bar{\phi}_{s}) are the spherical polar angles associated with location of the source in barred coordinates.

The detector strain for LISA in time domain can be expressed as Cutler (1998)

h(t)=32A(t)cos[2πft+πf˙t2+φpol(t)\displaystyle h(t)=\frac{\sqrt{3}}{2}A(t)\cos\left[2\pi ft+\pi\dot{f}t^{2}+\varphi_{pol}(t)\right.
+φD(t)+φp(t)].\displaystyle\left.+\varphi_{D}(t)+\varphi_{p}(t)\right]\,.

Here A(t)A(t) is the amplitude, φpol(t)\varphi_{pol}(t) is the polarization phase and φD(t)\varphi_{D}(t) is the Doppler phase that takes into account the motion of the detector with respect to the sun. We also include the effect of a small constant frequency evolution f˙\dot{f}, which may come from various dissipation mechanisms of the binary. For the spin induced orbital precession, we set f˙=0\dot{f}=0, however this term will be considered in a later part of the paper. The unconventional factor of 3/2\sqrt{3}/2 is attributed to the 6060^{\circ} angle between the detector arms. φp(t)\varphi_{p}(t) is the modulation to GW phase due to the orbital precession. A(t)A(t) and φpol(t)\varphi_{pol}(t) are given by

A(t)=(A+2F+2(t)+A×2F×2(t))1/2,\displaystyle A(t)=\left(A_{+}^{2}F_{+}^{2}(t)+A_{\times}^{2}F_{\times}^{2}(t)\right)^{1/2}\,, (2)
φp(t)=tan1(A×F×(t)A+F+(t)),\displaystyle\varphi_{p}(t)=\tan^{-1}\left(\frac{-A_{\times}F_{\times}(t)}{A_{+}F_{+}(t)}\right)\,, (3)

where F+F_{+} and F×F_{\times} are the antenna pattern functions:

F+(t)\displaystyle F_{+}(t) =\displaystyle= 12(1+cos2θs)cos2ϕscos2ψs\displaystyle\frac{1}{2}\left(1+\cos^{2}\theta_{s}\right)\cos 2\phi_{s}\cos 2\psi_{s} (4a)
cosθssin2ϕssin2ψs,\displaystyle-\cos\theta_{s}\sin 2\phi_{s}\sin 2\psi_{s}\,,
F×(t)\displaystyle F_{\times}(t) =\displaystyle= 12(1+cos2θs)cos2ϕssin2ψs\displaystyle\frac{1}{2}\left(1+\cos^{2}\theta_{s}\right)\cos 2\phi_{s}\sin 2\psi_{s} (4b)
+cosθssin2ϕscos2ψs.\displaystyle+\cos\theta_{s}\sin 2\phi_{s}\cos 2\psi_{s}\,.

Here (θs,ϕs)(\theta_{s},\phi_{s}) are polar spherical coordinates associated with n^\hat{n} where we use the convention that GWs from the source propagate along n^-\hat{n}. Note that (θs,ϕs)(\theta_{s},\phi_{s}) are time-dependent and we need to express them in terms of fixed coordinates (θ¯s,ϕ¯s)(\bar{\theta}_{s},\bar{\phi}_{s}) following Eq. 3.16 and Eq. 3.17 of Ref. Cutler (1998). The polarization angle ψs\psi_{s} is given by

ψs=arctan(L^z^(L^n^)(z^n^)n^(L^×z^)).\displaystyle\psi_{s}=\arctan\left(\frac{\hat{L}\cdot\hat{z}-(\hat{L}\cdot\hat{n})(\hat{z}\cdot\hat{n})}{\hat{n}\cdot(\hat{L}\times\hat{z})}\right)\,. (5)

Here L^\hat{L} is the unit vector along the orbital angular momentum of the binary and z^\hat{z} is the unit vector along the zz-axis of the detector. A+A_{+} and A×A_{\times} are the amplitudes of plus and cross polarization respectively,

A+=2M1M2aD[1+(L^n^)2],\displaystyle A_{+}=\frac{2M_{1}M_{2}}{aD}\left[1+\left(\hat{L}\cdot\hat{n}\right)^{2}\right]\,, (6a)
A×=4M1M2aDL^n^,\displaystyle A_{\times}=-\frac{4M_{1}M_{2}}{aD}\hat{L}\cdot\hat{n}\,, (6b)
with DD denoting the distance to the Sgr A* EMRI and aa is the orbital separation. Various quantities in Eqs. (5)-(6) can be expressed in terms of barred coordinates with the help of Eqs. (3.20)-(3.22) of Ref. Cutler (1998).

The Doppler phase φD\varphi_{D} in Eq. (II.1) denotes the phase difference of the wavefronts at the detector and at the sun, which is given by

φD(t)=2πfRsinθ¯Scos(ϕ¯(t)ϕ¯S).\varphi_{D}(t)=2\pi fR\sin\bar{\theta}_{S}\cos\left(\bar{\phi}(t)-\bar{\phi}_{S}\right)\,. (7)

In above expression, RR is the distance between sun and the earth, and ϕ¯(t)\bar{\phi}(t) is associated with location of center-of-mass of the detector:

ϕ¯(t)=ϕ¯0+2πt/T.\bar{\phi}(t)=\bar{\phi}_{0}+2\pi t/T\,. (8)

Here TT is period of LISA’s orbit around sun which is one year, and ϕ¯0\bar{\phi}_{0} is a constant denoting the position of the detector at t=0t=0 which we will set to zero. Note that the Doppler phase in Eq. (7) is the leading order correction due to the orbital motion of the detector around the sun. Second order Doppler shift to the GW phase is of the order v|φD|v|\varphi_{D}|, which is a small correction Cutler (1998) as vv is the orbital speed of the detector. Due to the time delay Rsinθ¯R\sin\bar{\theta} between a signal at the Barycenter and the detector, there is additional correction to the phase Cutler (1998). This is however negligible as it depends on the frequency evolution which is either zero or very small in our analyses. An additional Doppler phase occurs from the rotation of the detector about its axis which is of the order ff times the arm length of LISA in geometrized units and such correction is two orders of magnitude smaller than the leading order Doppler correction above. Hence, φD\varphi_{D} in Eq. (7) should suffice for our purposes. Finally, we write down the modulation of GW phase due to orbital precession following Apostolatos et al. (1994):

φp(t)=20t(L^n^1(L^n^)2)(L^×n^)L^˙𝑑t,\varphi_{p}(t)=2\int_{0}^{t}\left(\frac{\hat{L}\cdot\hat{n}}{1-(\hat{L}\cdot\hat{n})^{2}}\right)(\hat{L}\times\hat{n})\cdot\dot{\hat{L}}dt\,, (9)

where L^˙\dot{\hat{L}} is the derivative of L^\hat{L} in time.

II.2 GW phase modulation due to orbital precession of Sgr A* EMRI

We now apply Eq. (9) for the case of an Sgr A* EMRI. The mass of Sgr A* is M1=(4.297±0.012)×106MM_{1}=(4.297\pm 0.012)\times 10^{6}M_{\odot} Abuter et al. (2021, 2020, 2018) and we consider a stellar mass compact object with mass M2=20MM_{2}=20M_{\odot}. We further assume that the spin of Sgr A* (S1S_{1}) is much greater than the spin of the stellar mass object (S2S_{2}), which is reasonable because the mass ratio is already over 10510^{5}. Consequently, we work in the limit of M2M1M_{2}\ll M_{1} and S20S_{2}\simeq 0. For such assumptions, L^˙\dot{\hat{L}} due to spin precession is given by Apostolatos et al. (1994)

L^˙ΩpS^×L^,\dot{\hat{L}}\simeq\Omega_{p}\,\hat{S}\times\hat{L}\,, (10)

where the precession frequency Ωp\Omega_{p} takes the form:

ΩP2S1a3.\displaystyle\Omega_{P}\simeq\frac{2S_{1}}{a^{3}}\,. (11)

Hereafter we will assume an orbital separation of a90M1a\sim 90M_{1}, in which case the GW radiation-induced phase shift is negligible during the observation period of LISA. One can also find the dependence of signal-to-noise ratio on the orbital separation in Gourgoulhon et al. (2019). In the well-motivated model where the stellar-mass black holes migrated to the vicinity of the MBH assisted by the MBH accretion disk, the orbital eccentricity damping timescale is much shorter than its migration timescale Pan et al. (2021b). Therefore we assume that the stellar-mass black hole moves along a circular orbit, although it is straightforward to allow nonzero eccentricity in the Fisher analysis. The precession angle will be given by

αp=αp,0+ΩPt.\alpha_{p}=\alpha_{p,0}+\Omega_{P}t\,. (12)

Here αp,0\alpha_{p,0} denotes the value of α\alpha at time t=0t=0. We adopt the convention that αp=0\alpha_{p}=0 when L^z¯^\hat{L}\cdot\hat{\bar{z}} is maximum (which also means L^\hat{L}, z¯^\hat{\bar{z}}, and S^\hat{S} will be on the same plane), for which L^\hat{L} can be written as Apostolatos et al. (1994)

L^=S^cosλp\displaystyle\hat{L}=\hat{S}\cos\lambda_{p} +(z¯^S^cosθ¯sp)sinθ¯spsinλpcosαp\displaystyle+\frac{\left(\hat{\bar{z}}-\hat{S}\cos\bar{\theta}_{sp}\right)}{\sin\bar{\theta}_{sp}}\sin\lambda_{p}\cos\alpha_{p}
+S^×z¯^sinθ¯spsinλpsinαp.\displaystyle+\frac{\hat{S}\times\hat{\bar{z}}}{\sin\bar{\theta}_{sp}}\sin\lambda_{p}\sin\alpha_{p}\,. (13)

Here λp\lambda_{p} is the angle between L^\hat{L} and S^\hat{S}, while (θ¯sp,ϕ¯sp)(\bar{\theta}_{sp},\bar{\phi}_{sp}) are spherical polar angles of the vector S^\hat{S}. The angle φp(t)\varphi_{p}(t) now can be evaluated by plugging Eq. (II.2) and Eq. (10) in Eq. (9).

II.3 Analysis and results

We now proceed to the discussion of data analysis technique and results pertaining the spin induced orbital precession in the Sgr A* EMRI. We assume a maximum observation period of Tobs=10T_{\rm obs}=10 years with LISA Amaro-Seoane et al. (2017) to explore the science potential of these systems.

II.3.1 Data analysis formalism

We implement the Fisher analysis formalism to estimate the statistical error on various parameters in the waveform. Such analysis assumes the noise of the detector to be Gaussian and stationary, which works better in the limit of high SNR. Let us denote the detector’s noise as n(t)n(t); then the detector output can be expressed in terms of noise and signal as

s(t)=n(t)+h(t).s(t)=n(t)+h(t)\,. (14)

We define the inner product between two quantities AA and BB in the following manner:

(A|B)=40A~(f)B~(f)Pn(f)𝑑f.(A|B)=4\Re\int_{0}^{\infty}\frac{\tilde{A}^{*}(f)\tilde{B}(f)}{P_{n}(f)}\,df\,. (15)

A~(f)\tilde{A}(f) is the Fourier transform corresponding to AA, and the asterisk superscript denotes complex conjugate. Pn(f)P_{n}(f) is the one-side detector noise spectral density for which we consider the LISA detector noise given in Ref. Robson et al. (2019) (we ignore the galactic confusion noise as it is small compared to the instrumental for the frequency range we are working in).

The SNR of an event is

ρ=(h|h),\rho=\sqrt{(h|h)}\,, (16)

while a Fisher matrix element is defined as

Γij=(ih|jh).\Gamma_{ij}=(\partial_{i}h|\partial_{j}h)\,. (17)

In above equation, we denote a derivative with respect to a binary parameter θi\theta^{i} as i\partial_{i}. For a Sgr A* EMRI, the orbital frequency can be considered as almost constant during the observation period, so that it is more convenient to use the time-domain waveform which is real-valued. Hence, the Fisher matrix can be simplified in the following way:

(ih|jh)\displaystyle(\partial_{i}h|\partial_{j}h) =\displaystyle= 4I,II0ih~(f)jh~(f)Pn(f)𝑑f,\displaystyle 4\sum_{I,II}\Re\int_{0}^{\infty}\frac{\partial_{i}\tilde{h}^{*}(f)\partial_{j}\tilde{h}(f)}{P_{n}(f)}\,df\,, (18)
\displaystyle\simeq 2Pn(f)I,II0ih(t)jh(t)dt,\displaystyle\frac{2}{P_{n}(f)}\sum_{I,II}\int_{0}^{\infty}\partial_{i}h(t)\partial_{j}h(t)dt\ ,
\displaystyle\simeq 4Pn(f)0ih(t)jh(t)dt,\displaystyle\frac{4}{P_{n}(f)}\int_{0}^{\infty}\partial_{i}h(t)\partial_{j}h(t)dt\ ,

where we have considered the contribution from two LISA channels {I,II}\{I,II\}, and approximated the Sgr A* EMRI as a monochromatic source with constant frequency ff. In practice, the upper limit of above integral is taken to be the observation period which is 10 years in our case. Let us denote the 1-σ\sigma error bar on Fisher parameter θi\theta^{i} as Δθi=θtiθi\Delta\theta^{i}=\theta^{i}_{t}-\theta^{i} with θti\theta^{i}_{t} denoting the true value of θi\theta^{i}. If we do not impose any prior information, the root-mean-square of Δθi\Delta\theta^{i} can be obtained as the square root of diagonal elements of the inverse Fisher matrix:

(Γ1)ab=ΔθiΔθj.(\Gamma^{-1})^{ab}=\langle\Delta\theta^{i}\Delta\theta^{j}\rangle\,. (19)

The waveform of a precessing Sgr A* EMRI contains nine parameters as follows:

(ln𝒜,θ¯s,ϕ¯s,θ¯sp,ϕ¯sp,αp,0,λp,Ωp,f),\left(\ln\mathcal{A},\bar{\theta}_{s},\bar{\phi}_{s},\bar{\theta}_{sp},\bar{\phi}_{sp},\alpha_{p,0},\lambda_{p},\Omega_{p},\color[rgb]{0,0,0}{f}\right)\,, (20)

where 𝒜=(M1M2)/(Da)\mathcal{A}=(M_{1}M_{2})/(Da). Strictly speaking we know the distance DD and the sky locations of Sgr A* (θ¯s,ϕ¯s)(\bar{\theta}_{s},\bar{\phi}_{s}) from electromagnetic observations, but here we still include (θ¯s,ϕ¯s)(\bar{\theta}_{s},\bar{\phi}_{s}) as Fisher variables to address the angular resolution of LISA for such systems. As the measurement error varies for different system configurations, we use the Monte-Carlo method to sample 100 different sets of underlying parameters of Sgr A* EMRI, assuming uniform sky distribution for the angles and uniform distribution for the spin of Sgr A*. The underlying parameters for (θ¯s,ϕ¯s),D,M1(\bar{\theta}_{s},\bar{\phi}_{s}),D,M_{1} are set to be their known values, and M2M_{2} is assumed with the same value in the fiducial model (M2=20MM_{2}=20M_{\odot}). For each set of the underlying parameters we perform the Fisher analysis to compute the measurement uncertainties for various parameters. The histograms summarizing these Fisher analysis results are presented in Sec. II.3.3.

II.3.2 Threshold SNR

In order to address the detectability of Sgr A* EMRIs, we need both the expected SNR of these systems and the SNR detection threshold. The first quantity is partially discussed in Gourgoulhon et al. (2019) and in Sec. II.3.3, and in this section we compute the threshold SNR, following similar strategy described in Ref. Moore et al. (2019) developed for stellar-mass black hole binaries. Generally speaking, the threshold SNR reflects our tolerance on the false-alarm probability with suitable detection probability. It depends on the number of templates in the template bank against which the observed signal needs to be matched. Let us denote the number of waveforms in the bank by NBN_{B}, and write the template waveforms as ha(t)=ρh^a(t)h_{a}(t)=\rho\hat{h}_{a}(t) such that h^|h^=1\langle\hat{h}|\hat{h}\rangle=1, where a=1,2,,NBa=1,2,\ldots,N_{B}.

The statistics σa:=s|ha\sigma_{a}:=\langle s|h_{a}\rangle between the data ss and the templates hah_{a} follows the following probability distribution:

f1(σa,ρ)=exp[(σa2+ρ22)]σaI0(ρσa),f_{1}\left(\sigma_{a},\rho\right)=\exp\left[-\left(\frac{\sigma_{a}^{2}+\rho^{2}}{2}\right)\right]\sigma_{a}I_{0}(\rho\sigma_{a})\,, (21)

where I0I_{0} is the modified Bessel function of the first kind of order 0. If there is no signal in the data (s=ns=n), the probability distribution is simply

f1(σa,ρ=0)=σaexp[(σa22)].f_{1}(\sigma_{a},\rho=0)=\sigma_{a}\exp\left[-\left(\frac{\sigma_{a}^{2}}{2}\right)\right]\ . (22)

We can claim a detection if σa>σthr\sigma_{a}>\sigma_{\rm thr} at least for one template aa, with σthr\sigma_{\rm thr} denoting a certain threshold determined by a conventional false alarm possibility PFP_{F}

PF(σthr)=σthrf1(σa,ρ=0)𝑑σa,P_{F}(\sigma_{\rm thr})=\int_{\sigma_{\rm thr}}^{\infty}f_{1}\left(\sigma_{a},\rho=0\right)d\sigma_{a}\ , (23)

i.e., σthr=2lnPF\sigma_{\rm thr}=\sqrt{-2\ln P_{F}}. Following Ref. Moore et al. (2019), we choose a representative value of PF=103/NBP_{F}=10^{-3}/N_{B}, which is similar to the threshold PFP_{F} in Abbott et al. (2016). The detection probability as a function of SNR for a given σthr\sigma_{\rm thr} is given by

PD(ρ)=σthrf1(σa,ρ)𝑑σa,P_{D}(\rho)=\int_{\sigma_{\rm thr}}^{\infty}f_{1}\left(\sigma_{a},\rho\right)d\sigma_{a}\ , (24)

and the threshold SNR ρthr\rho_{\rm thr} is obtained for a given detection probability of PD(ρthr)P_{D}(\rho_{\rm thr}) which is taken as 0.90.9 here.

We now implement Fisher analyses to estimate the number of templates in the bank NBN_{B}. In our case, the first 3 models parameters (the amplitude 𝒜\mathcal{A} and the source location θ¯s,ϕ¯s\bar{\theta}_{s},\bar{\phi}_{s}) do not affect NBN_{B}, because the amplitude which only shows up as a prefactor of each template, therefore can be searched over each template at negligible cost and the source location is well known. Let us define the following Fisher matrix for the remaining 6 model parameters (θ¯sp,ϕ¯sp,αp,0,λp,Ωp,f)(\bar{\theta}_{sp},\bar{\phi}_{sp},\alpha_{p,0},\lambda_{p},\Omega_{p},{\color[rgb]{0,0,0}f}):

Γ^ij=(ih^|jh^).\hat{\Gamma}_{ij}=\left(\partial_{i}\hat{h}|\partial_{j}\hat{h}\right)\,. (25)

Let us also define a prior range on a Fisher parameter θi\theta^{i} by δθi\delta\theta^{i}, and a modified Fisher matrix Γ~\tilde{\Gamma},

Γ~ij=max.(Γ^ij,δij(δθi)2).\tilde{\Gamma}_{ij}={\rm max.}\left(\hat{\Gamma}_{ij},\frac{\delta_{ij}}{\left(\delta\theta^{i}\right)^{2}}\right)\,. (26)

Then NBN_{B} can be approximated as the following integral over the Fisher variables:

NB=dDθDetΓ~,N_{B}=\int d^{D}\theta\sqrt{\mathrm{Det}\,\tilde{\Gamma}}\,, (27)

Eq. (27) can be evaluated using the Monte-Carlo integration method where the input Fisher parameter θi\theta^{i} is distributed over the prior range δθi\delta\theta^{i} Cornish and Porter (2005):

dDθDetΓ~VNβDetΓ~β.\int d^{D}\theta\sqrt{\mathrm{Det}\,\tilde{\Gamma}}\simeq\frac{V}{N}\sum_{\beta}\sqrt{\mathrm{Det}\,\tilde{\Gamma}_{\beta}}\,. (28)

Here DetΓ~β\mathrm{Det}\,\tilde{\Gamma}_{\beta} is the determinant of the of the matrix Γ~\tilde{\Gamma} for sample β\beta, NN is the number of samples, and VV is the volume of the search space.

II.3.3 Results

We first examine the threshold SNR for a detection of GWs from the Sgr A* EMRI. As explained in Sec. II.3.2, for detection purpose, we only need to consider the waveform containing seven free parameters. In addition, as the cost of searching over amplitude is negligible, we consider only the last six parameters in Eq. (20). The volume of search space is then V=δθ¯spδϕ¯spδαp,0δλpδΩpδfV=\delta\bar{\theta}_{sp}\,\delta\bar{\phi}_{sp}\,\delta\alpha_{p,0}\,\delta\lambda_{p}\,\delta\Omega_{p}\color[rgb]{0,0,0}{\delta f}. To evaluate Eq. (28), we apply Monte-Carlo sampling by distributing the direction of spin and angular momentum uniformly over the 2-sphere, αp,0\alpha_{p,0} between 0 to 2π2\pi, and dimensionless spin parameter between 0.01 to 1. The lower end of spin is set to be nonzero as the Fisher matrix tends to me more singular for small spins, which affects the accuracy in computing the determinant of the Fisher matrix. We distribute the frequency ff uniformly between 1.7×1051.7\times 10^{-5} Hz to 2×1052\times 10^{-5} Hz, corresponding to a range of orbital separation a=85M1a=85M_{1} to a=95M1a=95M_{1}. As a consistency check, We implement two independent sets of 100 samples to perform the integration in Eq. (28) and find a consistent threshold SNR ρthr9.8\rho_{\rm thr}\color[rgb]{0,0,0}{\approx 9.8}.

In order to estimate the statistical distribution of measurement errors, we perform a separate Monte-Carlo study with the waveform containing all 9 parameters in Eq. (20). We distribute θ¯sp\bar{\theta}_{sp}, ϕ¯sp\bar{\phi}_{sp}, αp,0\alpha_{p,0}, f\color[rgb]{0,0,0}{f}, and λp\lambda_{p} in a similar manner as in the case of threshold SNR computation. However, we distribute the magnitude of dimensionless spin parameter from 0 to 1 uniformly as the calculation of determinant is not needed here. For each set of Monte-Carlo samples we compute the Fisher matrix, and collect all the data in histograms.

For the M2M_{2} and range of aa assumed in this fiducial model, we find 80% of the samples produce SNR greater than the threshold SNR ρthr\rho_{thr}, while the median SNR is about 12 (see Fig. 4). Note that the SNR linearly scales as M2M_{2} if it is different from 20M20M_{\odot}, and its dependence on aa is discussed in Gourgoulhon et al. (2019). We also present a histogram distribution of the relative errors in measuring Ωp\Omega_{p} in Fig. 5, which shows that we can constrain Ωp\Omega_{p} (and hence the magnitude of spin) with a median relative error of 2%. The direction of spin can also be measured to percent level accuracy, as shown in Fig. 6 and 7. This level of accuracy is more than an order of magnitude better than the spin measurement accuracy of radio interferometry, which has to account for all the modelling uncertainties of the accretion flow. In addition, Fig. 2 and Fig. 3 show that the LISA resolution uncertainties for the sky angles are on the level of Δθ¯s0.033,Δϕs¯0.022\Delta\bar{\theta}_{s}\sim 0.033,\Delta\bar{\phi_{s}}\sim 0.022 radian, or ΔΩ/4π6×105\Delta\Omega/4\pi\sim 6\times 10^{-5}. This means that the chance of having a double white dwarf source having similar signal strength (less than parsec scale distance) and sky locations is negligible. The expected measurement error of the opening angle λp\lambda_{p} and initial precession angle αp\alpha_{p} are shown in Fig.  8, and 9. On the other hand, the frequency can be measured very precisely with an error bar of the order 101010^{-10} Hz.

Refer to caption
Figure 2: Histogram distribution of 1-σ\sigma errors on the polar angle of location of Sgr A* EMRI (Δθ¯s\Delta\bar{\theta}_{s}) with respect to the heliocentric coordinates, computed with Fisher analyses with Monte-Carlo simulations. Vertical red line is the median of distribution which is about 0.033 radians.
Refer to caption
Figure 3: Histogram distribution of 1-σ\sigma errors on the azimuthal angle of location of Sgr A* EMRI (Δϕ¯s\Delta\bar{\phi}_{s}) in the heliocentric coordinates, computed with Fisher analyses with Monte-Carlo simulations. Vertical red line is the median of distribution which is about 0.022 radians.
Refer to caption
Figure 4: Histogram distribution of SNRs obtained from Fisher analyses with Monte-Carlo simulations. The blue vertical line shows the threshold SNR for detecting a signal: ρthr9.8\rho_{thr}\simeq\color[rgb]{0,0,0}{9.8}. The red vertical line shows the median SNR which is 11.7. About 80%\color[rgb]{0,0,0}{80\%} of the samples satisfy ρρthr\rho\geq\rho_{thr}.
Refer to caption
Figure 5: Histogram distribution of relative errors in measurement of precession orbital frequency Ωp\Omega_{p} obtained from Fisher analyses with Monte-Carlo simulations. The vertical red line denotes the median value of ΔΩp/Ωp\Delta\Omega_{p}/\Omega_{p} which is approximately 0.02.
Refer to caption
Figure 6: Histogram distribution of 1-σ\sigma error bars on the polar angle corresponding to the direction of spin (Δθ¯sp\Delta\bar{\theta}_{sp}), normalized by π\pi. Vertical red line shows the median of the distribution which is approximately 0.026.
Refer to caption
Figure 7: Histogram distribution of 1-σ\sigma error bars on the azimuthal angle corresponding to the direction of spin (Δϕ¯sp\Delta\bar{\phi}_{sp}), normalized by 2π2\pi. Vertical red line shows the median of the distribution which is approximately 0.016.
Refer to caption
Figure 8: Histogram distribution of 1-σ\sigma errors in the measurement of opening angle (Δλp\Delta\lambda_{p}) normalized by π\pi obtained from Fisher analyses with Monte-Carlo simulations. The vertical red line shows the median value of Δλp/π\Delta\lambda_{p}/\pi which is approximately 0.03.
Refer to caption
Figure 9: Histogram distribution of 1-σ\sigma error bars in the measurement of initial precession angle (Δαp,0\Delta\alpha_{p,0}) normalized by 2π2\pi. Vertical red line shows the median value of the distribution which is approximately 0.03.

III Probing dark matter

Massive black holes like Sgr A* can harbor dark matter clouds around them, and one way to probe the nature of such clouds is through GW observations. When a compact object travels through the cloud, a dark matter overdensity may form and create a friction force. Such friction force changes the frequency evolution of the binary. The cloud’s gravitational potential also applies a torque on the compact object, giving rise to an orbital precession. This section will focus on detecting such effects with Sgr A* EMRI, with both cold dark matter and axionic dark matter scenarios considered.

III.1 Cold dark matter

Dark matter may accumulate around a massive black hole like Sgr A*, forming overdensities or spikes  Gondolo and Silk (1999); Ullio et al. (2001). The change to GW phase due to the dynamical friction may be used to probe the dark matter profile around the central massive object, which has been explored in the case of intermediate-mass-ratio inspirals (IMRIs)  Kavanagh et al. (2020); Coogan et al. (2021); Eda et al. (2015). In the analysis below we comment on its application on EMRIs, especially the Sgr A* EMRIs.

Let us denote the frequency evolution as f˙\dot{f}, which is small and can be treated perturbatively with respect to the frequency of GWs at the beginning of observation period: f0f_{0}. Using the energy-balance law, f˙\dot{f} can be found as Kavanagh et al. (2020); Coogan et al. (2021)

f˙=96π8/3f011/3M1M25M1/3+12M2ξ(v)ρ0DMln(Λ)M1.\dot{f}=\frac{96\pi^{8/3}f_{0}^{11/3}M_{1}M_{2}}{5M^{1/3}}+\frac{12M_{2}\xi(v)\rho_{0}^{DM}\ln(\Lambda)}{M_{1}}\,. (29)

The first term on the right side of above equation is the frequency evolution due to the emission of GWs, while the second term is the contribution coming from dynamical friction. Here Λ\Lambda is defined as M1/M2\sqrt{M_{1}/M_{2}} and ξ(v)\xi(v) is the fraction of dark matter moving slower than the orbital speed vv. The dark matter density at the moving object’s location at time t=0t=0 is ρ0DM\rho_{0}^{DM}:

ρDM0=ρsp(aspa0)γsp,\rho^{0}_{DM}=\rho_{sp}\left(\frac{a_{sp}}{a_{0}}\right)^{\gamma_{sp}}\,, (30)

with a0a_{0} denoting the orbital separation at t=0t=0. The size of the spike is aspa_{sp} and ρsp\rho_{sp} is the density of dark matter at distance r=aspr=a_{sp}. The parameters (asp,ρsp,γspa_{sp},\rho_{sp},\gamma_{sp}) depend on the initial dark matter halo where the supermassive black hole was formed. If we consider the initial profile to be an NFW profile, γsp\gamma_{sp} is usually taken as 7/37/3. Using Eq. (30) to Eq. (29), we find that the contribution to f˙\dot{f} from the dynamical friction scales as f014/9f_{0}^{14/9}. As f0f_{0} for Sgr A* EMRIs is smaller than that of ordinary EMRIs detected by LISA by two orders of magnitude, the dark matter induced modification to f˙\dot{f} and GW phase (which scales as f˙Tobs2\dot{f}T^{2}_{\rm obs}) is supposed to be two orders of magnitude smaller as well. We expect such dark matter induced corrections to be more significant for ordinary EMRIs with smaller separation, higher orbital frequency and thus better detection prospects.

For a quantitative assessment of the modification to GW frequency evolution due to dynamical friction, let us first derive the parameters (asp,ρsp)(a_{sp},\rho_{sp}) for the cloud profile around Sgr A*. For the initial NFW profile, DM density ρ\rho at a distance rr from Sgr A* is Navarro et al. (1996)

ρNFW(r)=ρs(r/as)(1+r/as)2,\rho_{\mathrm{NFW}}(r)=\frac{\rho_{s}}{\left(r/a_{s}\right)\left(1+r/a_{s}\right)^{2}}\,, (31)

where ρs\rho_{s} and asa_{s} are characteristic density and radius respectively. asa_{s} is usually defined to be the radius within which the average DM density becomes 200 times the critical density of the universe ρc\rho_{c}. Then ρs\rho_{s} is related to ρc\rho_{c} according to

ρsρc=2003c2003(c200),\frac{\rho_{s}}{\rho_{c}}=\frac{200}{3}\frac{c_{200}^{3}}{\mathcal{F}\left(c_{200}\right)}\,, (32)

where (x)=ln(1+x)x/(1+x)\mathcal{F}(x)=\ln(1+x)-x/(1+x) Dutton and Macciò (2014). c=r/asc=r/a_{s} is the concentration parameter, and DM mass within r=asr=a_{s} is approximated by

M200=4πρsas3(c200).M_{200}=4\pi\rho_{s}a_{s}^{3}\mathcal{F}(c_{200})\,. (33)

We consider the low red shift approximation for parameter c200c_{200} which is Dutton and Macciò (2014)

log10c200=0.9050.101log10[M200h1012M],\log_{10}c_{200}=0.905-0.101\log_{10}\left[\frac{M_{200}h}{10^{12}M_{\odot}}\right]\,, (34)

where hh is the dimensionless Hubble constant and M200M_{200} is related to Sgr A* mass M1M_{1} as Ferrarese (2002)

M1107M(M2001012M)1.65\frac{M_{1}}{10^{7}M_{\odot}}\approx\left(\frac{M_{200}}{10^{12}M_{\odot}}\right)^{1.65} (35)

Using Eqs. (32)-(35),we achieve as=19.6a_{s}=19.6 kpc and ρs=3×1028g/cm3\rho_{s}=3\times 10^{-28}\mathrm{g/cm^{3}}.

Next, following Merritt (2004) we take the spike size aspa_{sp} to be 0.2rh0.2r_{h} where rhr_{h} is the gravitational influence radius of Sgr A* which is 1.67pc. Then matching Eq. (31) to spike profile ρDM=ρsp(asp/r)7/3\rho_{DM}=\rho_{sp}(a_{sp}/r)^{7/3} at r=aspr=a_{sp} we obtain ρsp262M/pc3\rho_{sp}\simeq 262\mathrm{M_{\odot}/pc^{3}}. Finally, Let us define the second term in Eq. (29) as

f˙DF=12M2ξ(v)ρ0DMln(Λ)M1\dot{f}_{DF}=\frac{12M_{2}\xi(v)\rho_{0}^{DM}\ln(\Lambda)}{M_{1}} (36)

Plugging ρsp\rho_{sp} and aspa_{sp} in above equation, and considering static dark matter case (ξ=1\xi=1) for simplicity, we obtain f˙DF=4×1021s2\dot{f}_{DF}=4\times 10^{-21}s^{-2}. This is more than two orders of magnitude smaller compared to the frequency evolution due to GW emission which we find as 1.3×1018s21.3\times 10^{-18}s^{-2}. We present a comparison of f˙DF\dot{f}_{DF} between the cold DM case and Axion DM case in the next subsection.

III.2 Axion dark matter

Axion or axion-like particles are well-motivated from string theory Marsh (2016); Arvanitaki et al. (2010) and standard model extension Peccei and Quinn (1977); Weinberg (1978); Dine and Fischler (1983); Abbott and Sikivie (1983) as dark matter candidates Press et al. (1990); Peebles (2000); Amendola and Barbieri (2006); Hui et al. (2017); Preskill et al. (1983). Axion fields close to spinning BH can extract angular momentum from the BH, leading to superradiance. In this subsection, we consider the effect of a bosonic cloud around Sgr A* on the orbit of the stellar mass BH. Axion dark matter density profile can achieve extremely high concentration near the central SMBHB, as compared with the cold dark matter scenario. Additional conservative dynamical effect may become significant because of the high mass density. For example, the Newtonian potential of the cloud can exert a torque on the orbiting object and induce orbital precession. We first study such precession effect in case of an Sgr A* EMRI, and then we analyze the change in GW frequency evolution induced by the dynamical friction of axion dark matter.

III.2.1 Newtonian potential of the cloud

To study the nonrelativistic description of the superradiant cloud, we will work in spherical coordinate systems (r,θ,ϕ)(r,\theta,\phi) and Cartesian coordinate (x,y,z)(x,y,z) with Sgr A* located at the origin. We consider a free complex scalar field, in which case the cloud is axisymmetric around the direction of spin of Sgr A* Zhang and Yang (2020); Baumann et al. (2019). In the nonrelativistic limit, the axion field can be expressed as

Ψ(r,t)=eiωtRnl(r)Ym(θ,ϕ).\Psi(r,t)=\mathcal{B}e^{-i\omega t}R_{nl}(r)Y_{\ell m}(\theta,\phi)\,. (37)

(n,l,m)(n,l,m) label the stationary eigenmodes of the field and ω\omega is the eigenfrequency. The radial function RnlR_{nl} takes the form of that of hydrogen atom, which we can conveniently write as

Rn(x~)=\displaystyle R_{n\ell}(\tilde{x})= [(2αμn)3(n1)!2n(n+l)!]1/2×\displaystyle\left[\left(\frac{2\alpha\mu}{n}\right)^{3}\frac{(n-\ell-1)!}{2n(n+l)!}\right]^{1/2}\times (38)
ex~n(2x~n)Ln12+1[2x~n].\displaystyle e^{-\frac{\tilde{x}}{n}}\left(\frac{2\tilde{x}}{n}\right)^{\ell}L_{n-\ell-1}^{2\ell+1}\left[\frac{2\tilde{x}}{n}\right]\,.

Here we introduce the parameter x~=α2r/M1\tilde{x}=\alpha^{2}r/M_{1} with α=M1μ\alpha=M_{1}\mu and μ\mu is the mass of the scalar field. Ln12+1[2x~n]L_{n-\ell-1}^{2\ell+1}\left[\frac{2\tilde{x}}{n}\right] is the generalized Laguerre polynomial of degree (nl1)(n-l-1) 111We implement the convention where Lna(x)L_{n}^{a}(x) satisfies the differential equation xy′′+(a+1x)y+ny=0xy^{\prime\prime}+(a+1-x)y^{\prime}+ny=0.. We choose the constant \mathcal{B} in Eq. (37) such that the total mass of the cloud McM_{c} is normalized to αM1\alpha M_{1}, namely,

d3xρ=McαM1,ρ=μΨΨ.\int d^{3}x\rho=M_{c}\sim\alpha M_{1}\,,\qquad\rho=\mu\Psi^{*}\Psi\,. (39)

Such an approximation is reasonable when α1\alpha\ll 1 and the initial BH spin is close to the maximal spin Baumann et al. (2019). Using Eq. (39) we then find =M1\mathcal{B}=M_{1}.

In the next step we derive the gravitational potential generated by the bosonic cloud. Since the potential satisfies the Poisson equation, we decompose it in terms of spherical harmonics in the following manner Poisson and Will (2014); Ferreira et al. (2017):

Φc=m4π2+1\displaystyle\Phi_{c}=\sum_{\ell m}\frac{4\pi}{2\ell+1} [qm(t,r)Ym(θ,ϕ)r+1\displaystyle\left[q_{\ell m}(t,r)\frac{Y_{\ell m}(\theta,\phi)}{r^{\ell+1}}\right. (40)
+pm(t,r)rYm(θ,ϕ)],\displaystyle\left.+p_{\ell m}(t,r)r^{\ell}Y_{\ell m}(\theta,\phi)\right],

with

qm(t,r)\displaystyle q_{\ell m}(t,r) =0rsρm(s)s2𝑑s,\displaystyle=\int_{0}^{r}s^{\ell}\rho_{\ell m}(s)s^{2}ds\,, (41a)
pm(t,r)\displaystyle p_{\ell m}(t,r) =rρm(s)s+1s2𝑑s.\displaystyle=\int_{r}^{\infty}\frac{\rho_{\ell m}(s)}{s^{\ell+1}}s^{2}ds\,. (41b)

We further define the harmonic components of the density ρ\rho as

ρm(t,r)=ρ(r,θ,ϕ)Ym(θ,ϕ)𝑑Ω.\rho_{\ell m}(t,r)=\int\rho(r,\theta,\phi)Y_{\ell m}^{*}(\theta,\phi)d\Omega\,. (42)

For simplicity we restrict ourselves to the fastest growing mode, which corresponds to n=2n=2, l=1l=1, and m=1m=1. For this particular mode, using Eq. (37) and Eq. (39) to Eq. (42), non-zero contributions to cloud density ρ\rho come from

ρ00\displaystyle\rho_{00} =\displaystyle= M12x~2ex~α3μ448π,\displaystyle\frac{M_{1}^{2}\tilde{x}^{2}e^{-\tilde{x}}\alpha^{3}\mu^{4}}{48\sqrt{\pi}}\,, (43a)
ρ20\displaystyle\rho_{20} =\displaystyle= M12x~2ex~α3μ4485π.\displaystyle-\frac{M_{1}^{2}\tilde{x}^{2}e^{-\tilde{x}}\alpha^{3}\mu^{4}}{48\sqrt{5\pi}}\,. (43b)

Finally, using Eq. (43) and Eq. (41) to Eq. (40), we obtain the gravitational potential of the cloud as

Φc=P1(x~)+P2(x~)cos2θ,\Phi_{c}=P_{1}(\tilde{x})+P_{2}(\tilde{x})\cos{2\theta}\,, (44)

with

P1=α3ex~32x~3(4848ex~\displaystyle P_{1}=\frac{\alpha^{3}e^{-\tilde{x}}}{32\tilde{x}^{3}}(48-48e^{\tilde{x}} +\displaystyle+ 48x~8x~2+32ex~x~2\displaystyle 48\tilde{x}-8\tilde{x}^{2}+32e^{\tilde{x}}\tilde{x}^{2} (45)
\displaystyle- 16x~36x~4x~5),\displaystyle 16\tilde{x}^{3}-6\tilde{x}^{4}-\tilde{x}^{5})\,,

and

P2=α3ex~32x~3(144144ex~\displaystyle P_{2}=\frac{\alpha^{3}e^{-\tilde{x}}}{32\tilde{x}^{3}}(144-144e^{\tilde{x}} +\displaystyle+ 144x~+72x~2\displaystyle 144\tilde{x}+72\tilde{x}^{2} (46)
+\displaystyle+ 24x~3+6x~4+x~5).\displaystyle 24\tilde{x}^{3}+6\tilde{x}^{4}+\tilde{x}^{5})\,.

III.2.2 Axion dark matter induced precession

It is convenient to express the components of the torque applied on Sgr A* EMRI orbit using the Cartesian coordinates (x,y,z)(x,y,z). Implementing the Newtonian potential in Eq. (44), the torque on object M2M_{2}, is

τ\displaystyle\vec{\tau} =\displaystyle= M2r×Φc\displaystyle-M_{2}\vec{r}\times\vec{\nabla}\Phi_{c}
=\displaystyle= 4M2P2(x~){sinθcosθsinϕ,sinθcosθcosϕ,0}.\displaystyle-4M_{2}P_{2}(\tilde{x})\{\sin\theta\cos\theta\sin\phi,-\sin\theta\cos\theta\cos\phi,0\}\,.

Such a torque will cause the orbit of M2M_{2} to precess around the direction of spin of Sgr A*. However, since the precession frequency is expected to be much smaller than the orbital frequency, we are interested in the torque averaged over one period. In this case the point mass can be replaced by a constant density ring of the same radius to receive the gravitational torque. Let us choose the z-axis to be along the direction of spin and the x-axis to be along the ascending node of the binary. We also assume at t=0t=0 object M2M_{2} is located along x-axis. The position of M2M_{2} can be expressed as

x=acosΩt,y=acosλpsinΩt,z=asinλpsinΩt.\displaystyle x=a\cos\Omega t,\qquad y=a\cos\lambda_{p}\sin\Omega t,\qquad z=a\sin\lambda_{p}\sin\Omega t\,.

Here Ω\Omega is the orbital angular frequency and λp\lambda_{p} is the angle between z-axis and the orbital angular momentum. Applying above equation to Eq. (III.2.2) and averaging over one orbital period we obtain

τ={P2(x~(a))M2sin2λp,0,0}.\langle\vec{\tau}\rangle=\left\{-P_{2}(\tilde{x}(a))M_{2}\sin 2\lambda_{p},0,0\right\}\,. (49)

Next, we can express the precession frequency as a small change of precession angle ΔΘ\Delta\Theta over small time Δt\Delta t as

Ωp=ΔΘΔttanΔΘΔt=ΔLLsinλpΔt=|τ|Lsinλp.\Omega_{p}=\frac{\Delta\Theta}{\Delta t}\simeq\frac{\tan{\Delta\Theta}}{\Delta t}=\frac{\Delta\vec{L}}{L\sin{\lambda_{p}}\Delta t}=\frac{|\langle\vec{\tau}\rangle|}{L\sin\lambda_{p}}\,. (50)

Using Eq. (49) to above equation leads to a precession frequency of

Ωp=4Ω1/3P2cosλpM12/3,\Omega_{p}=\frac{4\Omega^{1/3}P_{2}\cos\lambda_{p}}{M_{1}^{2/3}}\,, (51)

which depends on α\alpha through P2P_{2}. We need to choose a suitable range for α\alpha, which we discuss next.

To allow a detectable effect for Sgr A* EMRI, the growth period of the superradiant cloud needs to be much smaller than the Hubble time. In the limit of α1\alpha\ll 1, the growth period of the cloud is given by the Detweiler’s approximation Baumann et al. (2019); Detweiler (1980) :

τg24(a/M1)1α(4+5)M1.\tau_{g}\simeq 24(a/M_{1})^{-1}\alpha^{-(4\ell+5)}M_{1}\,. (52)

If we set τg\tau_{g} to be 𝒪(108)\mathcal{O}(10^{8}) years, above equation suggests α0.04\alpha\simeq 0.04, which we will consider as a lower limit on α\alpha. On the other hand, the cloud may deplete due to GW radiation if the field is real-valued. Notice that in this case the calculation for precession rate still applies, as the cloud rotates faster than the precession rate, and a rotation-averaged density profile for real-valued field is the same as that for complex-valued field. Taking into account the GW radiation, the lifetime of the cloud can be approximated by the following expression which is valid for α<0.1\alpha<0.1 Baumann et al. (2019):

τc109 years (M105M)(0.1α)15.\tau_{c}\simeq 10^{9}\text{ years }\left(\frac{M}{10^{5}M_{\odot}}\right)\left(\frac{0.1}{\alpha}\right)^{15}\,. (53)

If we choose an α\alpha of 0.1, which is the limit of validity of above expression, the cloud survives about 1 billion years for the Sgr A* EMRI. Hence it is reasonable to assume 0.1 as the upper bound on α\alpha. A range of α[0.04,0.1]\alpha\in[0.04,0.1] corresponds to the mass of the scalar field μ[13,32.6]×1019\mu\in[13,32.6]\times 10^{-19} eV.

In Fig. 10 we present Ωp\Omega_{p} as a function of α\alpha for λp=π/4\lambda_{p}=\pi/4, and also compare it with spin induced precession with same opening angle and a spin of S=0.5M12S=0.5M_{1}^{2}. We find that the dark matter induced precession frequency is overall smaller than that of spin-induced precession, although they are almost comparable near α=0.1\alpha=0.1. Nevertheless, since in both cases the precession happens around the direction of spin, the modification to GW phase is similar and in principle it is not possible to distinguish the two effects.

Refer to caption
Figure 10: Axion dark matter induced precession orbital frequency Ωp\Omega_{p} as a function of α=M1μ\alpha=M_{1}\mu according to Eq. (51), which is denoted by the blue curve. Here M1M_{1} is the mass of Sgr A* and μ\mu is the mass of the complex scalar field which describes the axion dark matter. The angle between spin and orbital angular momentum vector is taken to be π/4\pi/4. The red horizontal dotted line shows the orbital frequency of spin induced precession with same opening angle and S=0.5M12S=0.5M_{1}^{2}.

III.2.3 Modification to frequency evolution due to dynamical friction

In addition to the orbital precession caused by the Newtonian potential of the axion cloud, a dynamical friction force is also applied on object M2M_{2}, which can be expressed as Hui et al. (2017); Chandrasekhar (1943)

F=1v24πM22ρCΛ.F=\frac{1}{v^{2}}4\pi M_{2}^{2}\rho C_{\Lambda}\,. (54)

In case of Sgr A* EMRI where the orbit is circular, the velocity vv of M2M_{2} relative to the wave function can be approximated as the orbital velocity, and CΛC_{\Lambda} has a simplified form Zhang and Yang (2020)

CΛ(kr)02kr1s(1coss)𝑑s+sin2kr2kr1,C_{\Lambda}(kr)\simeq\int_{0}^{2kr}\frac{1}{s}(1-\cos s)ds+\frac{\sin 2kr}{2kr}-1\,, (55)

where k=μvk=\mu v with μ\mu representing the mass of the scalar field. We again restrict ourselves to the n=2n=2, l=1l=1, and m=1m=1 mode and use Eq. (55) and ρ=ΨΨ\rho=\Psi^{*}\Psi to Eq. (54) to obtain the rate of change of energy loss due to dynamical friction as E˙DF=Fv\dot{E}_{DF}=Fv. Similar to III.1, Energy loss due to dynamical friction and GW emission in this case can be taken as small and constant, which enters the GW phase as δφ=f˙πt2\delta\varphi=\dot{f}\pi t^{2}. The waveform we consider in this case is

h(t)=32A(t)cos[2πf0t+f˙πt2+φp(t)+φD(t)],\displaystyle h(t)=\frac{\sqrt{3}}{2}A(t)\cos\left[2\pi f_{0}t+\dot{f}\pi t^{2}+\varphi_{p}(t)+\varphi_{D}(t)\right]\,,

where φp(t)\varphi_{p}(t) is the polarization phase and φD(t)\varphi_{D}(t) is the Doppler phase as in section II.1, and

f˙96π8/3f011/3M1M25M1/3+3f01/3M1/3F0v0π2/3M1M2.\dot{f}\simeq\frac{96\pi^{8/3}f_{0}^{11/3}M_{1}M_{2}}{5M^{1/3}}+\frac{3f_{0}^{1/3}M^{1/3}F_{0}v_{0}}{\pi^{2/3}M_{1}M_{2}}\,. (57)

Quantities with subscript “0” are evaluated for a circular binary with a=90Ma=90M. The second term on the right side is the contribution to frequency evolution from dynamical friction: f˙DF\dot{f}_{DF}.

In Fig. 11 we present f˙DF\dot{f}_{DF} as a function of α\alpha for a Sgr A* EMRI in the equatorial plane θ=π/2\theta=\pi/2, as well as the 1-σ\sigma upper bound on f˙DF\dot{f}_{DF} obtained from Fisher analyses. The Fisher analysis is performed with the parameters ln𝒜\ln\mathcal{A}, θ¯s\bar{\theta}_{s}, ϕ¯s\bar{\phi}_{s}, θ¯L\bar{\theta}_{L}, ϕ¯L\bar{\phi}_{L}, f0\color[rgb]{0,0,0}{f_{0}}, and f˙DF\dot{f}_{DF}. Here (θ¯L,ϕ¯L\bar{\theta}_{L},\bar{\phi}_{L}) is the direction of orbital angular momentum of Sgr A* EMRI, for which we consider (π/4,3π/4\pi/4,3\pi/4) as a fiducial value. The error of f˙DF\dot{f}_{DF} is not sensitive to the fiducial value of f˙DF\dot{f}_{DF}. We find the 1-σ\sigma upper bound on f˙DF\dot{f}_{DF} is approximately 3.47×1018s2\color[rgb]{0,0,0}{3.47\times 10^{-18}}\,\mathrm{s}^{-2}, which roughly corresponds to α=0.095\color[rgb]{0,0,0}{\alpha=0.095}, which means an effect to the waveform phase coming from α[0.095,0.1]\color[rgb]{0,0,0}{\alpha\in[0.095,0.1]} or μ[3.1,3.3]×1018\color[rgb]{0,0,0}{\mu\in[3.1,3.3]\times 10^{-18}} eV can exceed the statistical uncertainty. The chance that axion mass lies within such narrow range is small. Fig. 11 also shows that the dynamical friction due to cold DM spike around Sgr A* can produce f˙DF\dot{f}_{DF} which is comparable to the Axion DM case only when α0.054\alpha\leq 0.054. Note that this is an overestimate, as we assumed static cold dark (ξ=1\xi=1) while in reality ξ\xi is expected to be smaller Coogan et al. (2021); Kavanagh et al. (2020). On the other hand, f˙DF\dot{f}_{DF} in Axion DM case can be greater than the GW radiation induced f˙\dot{f} if α>0.087\alpha>0.087.

Refer to caption
Figure 11: Dynamical friction induced frequency evolution (f˙DF\dot{f}_{DF}) as a function of α\alpha (shown by blue solid line) for a Sgr A* EMRI in equatorial plane θ=π/2\theta=\pi/2. The horizontal dashed red line shows the 1-σ\sigma upper bound on f˙DF\dot{f}_{DF} achieved from Fisher analyses, which roughly corresponds to Δf˙DF=3.47×1018s2\Delta\dot{f}_{DF}=\color[rgb]{0,0,0}{3.47\times 10^{-18}}\,\mathrm{s}^{-2}. The green dotted line indicates the frequency evolution due to emission of GWs (1.3×1018s21.3\times 10^{-18}s^{-2}), while the magenta dash-dotted line represents f˙DF\dot{f}_{DF} in the case of a cold dark matter spike around Sgr A* (4×1021s24\times 10^{-21}s^{-2}) discussed in Sec. III.1.

IV Discussion

IV.1 Multi-body effect

We now explore the case where the Sgr A* EMRI experiences the Kozai-Lidov effect due to the presence of a tertiary stellar-mass object, and determine whether or not such effects would be detectable. Let us denote the mass of the third body by M3M_{3}, which orbits around the center of mass of the Sgr A* EMRI consisting of masses M1M_{1} and M2M_{2}. We assume aoutaina_{out}\gg a_{in} where aina_{in} and aouta_{out} are semimajor axes of the inner and outer binary respectively. We also assume the eccentricities of inner and outer binaries are eine_{in} and eoute_{out} respectively. The outer perturber M3M_{3} induce time-dependent evolution of the orbital elements of the inner binary, such as the eccentricity, inclination, argument of periapsis, and longitude of ascending nodes.

The orbital evolution of the Sgr A* EMRI in such a hierarchical triple system happens in a typical rate tLK1t_{LK}^{-1}, where tLKt_{LK} is Kozai-Lidov time scale Liu et al. (2014); Su et al. (2021):

tLK1=M1+M2ain3(M3M1+M2)(ainaout1eout2)3.t_{LK}^{-1}=\sqrt{\frac{M_{1}+M_{2}}{a_{in}^{3}}}\left(\frac{M_{3}}{M_{1}+M_{2}}\right)\left(\frac{a_{in}}{a_{out}\sqrt{1-e_{out}^{2}}}\right)^{3}\,. (58)

In this case, M3/(M1+M2)𝒪(105)M_{3}/(M_{1}+M_{2})\sim\mathcal{O}(10^{-5}), together with the fact that (M1+M2)/ain3𝒪(105)\sqrt{(M_{1}+M_{2})/a_{in}^{3}}\sim\mathcal{O}(10^{-5}) Hz, suggests that tLK1𝒪(103)t_{LK}^{-1}\sim\mathcal{O}(10^{3}) year, i.e., the Kozai-Lidov time scale is much longer than our observation period. Therefore the multibody effect is negligible for the Sgr A* EMRIs considered here.

IV.2 Conclusion

We have investigated several possible applications of Sgr A* EMRIs if they exist within 10210^{2}M distance from Sgr A*. The detection threshold for these systems is significantly smaller than that of ordinary EMRIs, thanks to the known location of the source and much smaller waveform parameter space. The primary application of an Sgr A* EMRI is to measure the spin of Sgr A*, which likely has the best accuracy compared to alternative observation methods, such as using EHT. We have investigated the case of a cold dark matter cloud around Sgr A* and have found that EMRIs that have higher orbital frequency would be more efficient to probe such a scenario. On the other hand, the presence of an axion cloud, if the axion mass falls into the range with α(0.040.1)\alpha\in(0.04-0.1), may generate an additional precession effect for the EMRI orbit, which is degenerate with the spin induced precession. However, the degeneracy effect is only significant in a narrow mass range of Axion, so it will not likely pose serious challenge for the Sgr A* spin measurement. Nevertheless, we’d like to remove this “contamination” for the spin; on the other hand, if the inferred dimensionless spin based on precession rate is greater than one, it is a sign of the existence of a dark matter cloud.

One may also imagine possible ways to break the degeneracy. First, if there are multiple Sgr A* EMRIs being detected at the same time, it is likely that they have different orbital radii. Therefore the relative weight expected from Lense-Thirring precession and cloud-induced precession should be different, which may be used to separately determine different components of contributions. Second, if the relevant axion mass range is ruled out by other measurements, e.g., using the spins of other massive black holes inferred from X-ray reverberation or iron line measurements Crescini et al. (2020); Gramolin et al. (2021), the possible degeneration can be obviously neglected. Third, as axion cloud may have a mass of fraction of α\alpha of the Sgr A* mass, it may influence the spacetime to the extent that EHT can probe the difference. We don’t have a quantitative estimation for this last point, but it may worth further detailed study in the future, along with the science goals of EHT in probing dark matter.

There is also the possibility that we don’t find the sign of Sgr A* EMRI using LISA, which may be explained by various reasons. In the disk migration channel, the accumulation of stellar-mass black hole in the disk close to the MBH is a result of that the migration timescale peaks where the gravitational wave emission becomes dominant over the effect of density waves, and the number of stellar-mass BH accumulation mainly depends on the disk model and the disk lifetime. As shown in Pan et al. (2021b), the peak of the migration timescale in a β\beta disk is rather mild and no more than two black holes of 10M10M_{\odot} assemble in the range of r200Mr\leq 200M. We therefore expect negligible amount of heavier BHs with mass 20M\geq 20M_{\odot} considering their even lower abundance. In a α\alpha disk, a larger number (220)(2-20) of 10M10M_{\odot} BHs are expected to accumulate in the range of r200Mr\leq 200M depending on the disk lifetime (108106)(10^{8}-10^{6}) yr Pan et al. (2021b). For heavier 20M\geq 20M_{\odot} black holes, the number should be lower by a factor of a few again due to the lower abundance. In this case, the non-detection of Sgr A* EMRIs may indicate that the latest accretion episode is more than 1 Myrs ago such that all nearby stellar-mass black holes detectable by LISA have merged with Sgr A* due to GW emission. It is also possibly due to the fact that the accretion disk direction is random in each episode, and the lifetime of each episode is less than 10510^{5} yr Pan et al. (2021b), such that the stellar-mass black holes captured by the disk had not had enough time to migrate to the vicinity of the MBH, so the assumption of “in-disk migration” made in Fig. 7 of Pan et al. (2021b) breaks down. For the mass segregation scenario, it could come from the paucity of massive stellar-mass black holes within the nuclear star cluster, or other relevant assumption of the calculation that affects the final distribution in Emami and Loeb (2020, 2021). Lastly, if there is a set of stellar-mass black holes at 102M1\sim 10^{2}M_{1} but with mass several times smaller than 2020 MM_{\odot}, we may still miss the detection because of insufficient signal-to-noise ratio.

We have assumed circular obits in the analysis as disk-driven migration efficiently damps out eccentricity, but eccentric orbits are allowed in the mass segregation scenario, or during the time that the disk has disappeared. For eccentric orbits, higher harmonics of the orbital frequency generically contribute to the waveform, which may lead to high event SNR as the frequencies of higher harmonics are closer to the sensitive band of LISA. The waveform discussed in Sec. II.1 should include eccentricity as another parameter, and Post-Newtonian effects such as the periapsis shift should be consistently included. The accuracy in constraining various system parameters may also be improved thanks to the larger event SNR.

Acknowledgements.
We thank Jun Zhang for the fruitful discussion on probing axion dark matter with Sgr A* EMRIs. We also thank Hang Yu and Zhenwei Lyu for their assistance on computing the waveform modulation due to spin induced orbital precession. S.T. thanks Zack Carson for his help in performing Fisher analyses on Mathematica. S. T., Z. P. and H. Y. are supported by the Natural Sciences and Engineering Research Council of Canada and in part by Perimeter Institute for Theoretical Physics. Research at Perimeter Institute is supported in part by the Government of Canada through the Department of Innovation, Science and Economic Development Canada and by the Province of Ontario through the Ministry of Colleges and Universities.

References