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Quantifying torque from the Milky Way bar using Gaia DR2

Rain Kipper1, Peeter Tenjes1, Taavi Tuvikene1, Punyakoti Ganeshaiah Veena1,2 E-mail: [email protected]    Elmo Tempel1
1Tartu Observatory, University of Tartu, Observatooriumi 1, 61602 Tõravere, Estonia
2Kapteyn Astronomical Institute, University of Groningen,PO Box 800, 9747 AD Groningen, The Netherlands
(Accepted 2020 March 31. Received 2020 March 31; in original form 2019 October 14)
Abstract

We determine the mass of the Milky Way bar and the torque it causes, using Gaia DR2, by applying the orbital arc method. Based on this, we have found that the gravitational acceleration is not directed towards the centre of our Galaxy but a few degrees away from it. We propose that the tangential acceleration component is caused by the bar of the Galaxy. Calculations based on our model suggest that the torque experienced by the region around the Sun is 2400km2s2\approx 2400\,{\rm km^{2}\,s^{-2}} per solar mass. The mass estimate for the bar is 1.6±0.3×1010M\sim 1.6\pm 0.3\times 10^{10}\,\mathrm{M_{\odot}}. Using greatly improved data from Gaia DR2, we have computed the acceleration field to great accuracy by adapting the oPDF method (Han et al. 2016) locally and used the phase space coordinates of 4×105\sim 4\times 10^{5} stars within a distance of 0.5 kpc from the Sun. In the orbital arc method, the first step is to guess an acceleration field and then reconstruct the stellar orbits using this acceleration for all the stars within a specified region. Next, the stars are redistributed along orbits to check if the overall phase space distribution has changed. We repeat this process until we find an acceleration field that results in a new phase space distribution that is the same as the one that we started with; we have then recovered the true underlying acceleration.

keywords:
Galaxy: kinematics and dynamics – Galaxy: fundamental parameters – Galaxy: structure
pubyear: 2020pagerange: Quantifying torque from the Milky Way bar using Gaia DR23

1 Introduction

Gaia satellite data releases allow us to construct quite detailed models for the Milky Way (MW) stellar density distribution and its kinematics. The latest Data Release 2 (Lindegren et al., 2018) gives us an excellent opportunity to explore the solar neighbourhood (SN) and somewhat more distant regions. In the present paper, we calculate the gravitational acceleration of the MW using the Gaia DR2 data, in an ellipsoidal region within a distance of 0.5 kpc from the Sun in the Galactic plane.

Modelling the MW is very different from modelling other disc galaxies since we make observations from within the MW. Although our location within the MW can make modelling easier, (e.g. individual stars are resolved) it can also add complications to it, e.g. dust attenuation and selection function can have a strong influence on modelling. For example, it was only at beginning of the 1980s that the first direct hints that the MW may be a barred spiral galaxy came to light (Matsumoto et al., 1982). This was possible because of near-IR observations. Due to dust attenuation and our position inside the MW, it was difficult to draw such a conclusion on the morphology of MW before that.

On the other hand, we are at a great advantage because of the wealth of observational data available for the MW, unmatched and unavailable for other galaxies. For instance, axisymmetric models developed by Piffl et al. (2014); McMillan (2017); Binney & Wong (2017) use HI and CO velocities, maser data, Sgr A* proper motions, the globular cluster system, the velocity distribution in the SN, SDSS star counts in different colours, RAVE data, detailed MW satellite data and N-body simulation data. Additional constraints on the mass distribution were derived from cold stellar streams (Bovy et al., 2016) and Gaia DR2 proper motions of globular clusters (Watkins et al., 2019). However, the assumption of axisymmetry in mass distribution models is only a first approximation.

The existence of the central bar of the MW was first confirmed by Weiland et al. (1994), by analysing asymmetries in the near-IR surface brightness distribution of the central bulge from the COBE/DIRBE data. This was further confirmed by correcting the data for extinction (Dwek et al., 1995; Binney et al., 1997).

There are currently two contrasting scenarios – a fast rotating bar and a slow rotating bar. In the first case (e.g. Binney et al., 1997; Bissantz et al., 2003; Monari et al., 2017) the bar is rotating with pattern speed Ωp=5070kms1kpc1\Omega_{p}=50-70~{}\mathrm{km\,s^{-1}kpc^{-1}}; in the second case (Wegg & Gerhard, 2013; Wegg et al., 2015; Portail et al., 2015; Dias et al., 2019) the calculated pattern speed is 2530kms1kpc125-30~{}\mathrm{km\,s^{-1}kpc^{-1}}. Intermediate pattern speed values were derived by Li et al. (2016); Portail et al. (2017); Pérez-Villegas et al. (2017); Sanders et al. (2019); Bovy et al. (2019) as Ωp=3540kms1kpc1\Omega_{p}=35-40~{}\mathrm{km\,s^{-1}kpc^{-1}}. These calculated pattern speeds vary by about two times and as a result their corotation radii and outer Lindblad radii vary quite significantly. Both these scenarios agree that the angle between the major axis of the bar and the line connecting the Sun and the Galactic centre (GC) is about 2030deg20-30\,\mathrm{deg}.

According to the axisymmetric models, the stars in orbits are phase-mixed. According to the non-axisymmetric models, stellar orbits are somewhat perturbed and phases of stars in orbits may not be completely mixed (Dehnen, 2000; Fux, 2001; Monari et al., 2017; Binney, 2018; Trick et al., 2019) and thus orbital structure is more complicated (i.e. there are resonances). For example, using the Gaia DR2 data, Ramos et al. (2018) found that, in the case of the MW, some orbit phases are mixed. Similar arcs and ridges were also found by Antoja et al. (2018); Kawata et al. (2018); Trick et al. (2019). Gravitational potential disturbances due to the bar may have caused deviations of stars from their initial orbits in the case of several cold stellar streams (Hattori et al., 2016; Pearson et al., 2017; Banik & Bovy, 2019) that originate from small stellar systems. The torque from the bar is not the only reason (see e.g. Kipper et al. (2019b)). These disturbances can create observed gaps in stream surface density distributions.

Unfortunately, the structural parameters of the bar and its contribution to the gravitational acceleration are still rather poorly constrained. Thus, it is important to know the gravitational acceleration distribution in the Galactic plane and also to study how this allows one to constrain the bar properties. The Gaia satellite data provide an excellent opportunity to do this.

In the present paper we calculate all three acceleration components in the SN. We use the orbital arc method, developed in Kipper et al. (2019a). The method and its specific implementation details are described in Sect. 2. The method is used on the Gaia DR2 data. We use two different versions of the data, from the StarHorse project (Anders et al., 2019) and from the Schönrich catalogue (Schönrich et al., 2019). The selection of the data used is described in Sect. 3. We demonstrate in Sect. 4 that the derived acceleration components cannot be explained within an axisymmetric model. The final section is dedicated to the summary and discussion.

We denote (x,y,z)(x,y,z) as Galactocentric rectangular coordinates and (R,θ,z)(R,\theta,z) as corresponding cylindrical coordinates, where θ=0\theta=0 corresponds to the opposite direction from the Sun. Transformations of sky coordinates, proper motions and radial velocities to Galactocentric coordinates and velocities were carried out using the Astropy package (Astropy Collaboration et al., 2013; Price-Whelan et al., 2018). For the solar velocity, we used the values (U,V,W)=(11.1,12.24,7.25)kms1(U_{\odot},V_{\odot},W_{\odot})=(11.1,12.24,7.25)\,\mathrm{km}\,\mathrm{s}^{-1}, and Vg,=Vc,+VV_{g,\odot}=V_{c,\odot}+V_{\odot}, with the circular velocity Vc,=240kms1V_{c,\odot}=240\,\mathrm{km}\,\mathrm{s}^{-1} (López-Corredoira & Sylos Labini, 2019).

Refer to caption
Figure 1: An illustration of the region where the orbital arc method is applied. The central point represents the Sun and the circular region up to a distance of 0.5 kpc from the Sun is the region used in this paper. The black triangle points towards the Galactic centre. The coloured arcs for star 1 and star 2 represent the reconstructed orbits for these two stars. Orbital arcs are reconstructed for all stars in this region. The grey cells are the Voronoi cells, each of which contains a similar number of stars. The time interval, Δti\Delta t_{i}, is the time a star spends in the ithi^{\mathrm{th}} Voronoi cell. The times at which the star enters and exits the region are tentert_{\rm enter} and texitt_{\rm exit}, respectively.

2 Method and implementation

2.1 Orbital arc method

In this section, we provide a brief overview of the orbital arc method, which we have implemented in this paper to compute the gravitational acceleration, mass and torque estimates of the Galactic bar. For a detailed and thorough description of the formulation and tests of the model, please see Kipper et al. (2019a). We will refer to this particular method as the orbital arc method, since its most crucial step is the reconstruction of stellar orbits to accurately obtain the acceleration in the Milky Way, using the phase space information of stars. This has already been successfully applied to a simulation in Kipper et al. (2019a) and for the observational data in a simplified form (Kipper et al., 2018). Here we apply it for the Gaia DR2 data. The orbital arc method has five important steps.

  1. Step 1 – Acceleration field:

    We first select a region with a sufficiently large number of stars and known phase space coordinates. Next, we guess an acceleration field and use this to get the orbits. In the orbital arc method, the acceleration field is a free function of the model and contains free parameters. For instance, we can take advantage of the axisymmetric property of a galaxy, and choose an acceleration field described by the cylindrical coordinates:

    ax\displaystyle a_{x} =\displaystyle= aRcosθ,\displaystyle a_{R}\cos\theta, (1)
    ay\displaystyle a_{y} =\displaystyle= aRsinθ+Ay,\displaystyle a_{R}\sin\theta+A_{y}, (2)
    az\displaystyle a_{z} =\displaystyle= az.\displaystyle a_{z}. (3)

    Components aRa_{R} and aza_{z} are taken in the form of functions

    az\displaystyle a_{z} =\displaystyle= Az+Az,zz+Az,RΔR+Az,RzzΔR,\displaystyle A_{z}+A_{z,z}z+A_{z,R}\Delta R+A_{z,Rz}z\Delta R, (4)
    aR\displaystyle a_{R} =\displaystyle= AR+AR,RΔR,\displaystyle A_{R}+A_{R,R}\Delta R, (5)
    ΔR\displaystyle\Delta R =\displaystyle= RR,\displaystyle R-R_{\odot}, (6)

    where AyA_{y}, AzA_{z}, ARA_{R}, Az,zA_{z,z}, AR,RA_{R,R}, Az,RA_{z,R}, Az,RzA_{z,Rz} and in some cases also RR_{\odot} are free parameters obtained via fitting.

    If we do not assume axisymmetry, acceleration vector components are taken in the form of their first-order Taylor expansion:

    ax=Ax+Ax,xΔx+Ax,yΔy+Ax,zΔz\displaystyle a_{x}=A_{x}+A_{x,x}\Delta x+A_{x,y}\Delta y+A_{x,z}\Delta z (7)
    ay=Ax+Ay,xΔx+Ay,yΔy+Ay,zΔz\displaystyle a_{y}=A_{x}+A_{y,x}\Delta x+A_{y,y}\Delta y+A_{y,z}\Delta z (8)
    az=Ax+Az,xΔx+Az,yΔy+Az,zΔz.\displaystyle a_{z}=A_{x}+A_{z,x}\Delta x+A_{z,y}\Delta y+A_{z,z}\Delta z. (9)

    Here Δx\Delta x, Δy\Delta y, Δz\Delta z denote the distances from the region’s centre.

  2. 1.

    Step 2 – Orbital arc reconstruction: Using the initial conditions, which is the phase space information from the data, and the acceleration field from the previous step, we solve the equations of motion to obtain stellar orbits for each star. A schematic of the reconstructed orbit arcs is represented as coloured arcs in Fig. 1.

  3. 2.

    Step 3 – Randomizing star position: The core of the proposed method lies in the oPDF (orbital Probability Density Function), according to which the time of observing a star is random. This means, we can reposition a star along its orbit by picking a random time from a uniform distribution of time. By picking infinitely many times from this distribution, we reach a continuous distribution of the star along its orbit (a similar description to the procedure can be found in Han et al. 2016). Following this, we reposition every star in its orbit and get a new distribution of stars in the region. This is relevant in the last step where we will compare the old and new distributions.

  4. 3.

    Step 4 – Phase space density: In order to compute the probability of finding a star in its orbit, we need to first specify a small segment of the star’s orbit. For this, we construct Voronoi tessellations by considering small subsets of data, such that in each Voronoi cell there are similar numbers of stars; this reduces the Poisson error. The Voronoi cells are shown in the schematic diagram in Fig. 1. To compute the probability of finding a star in its orbit, we use the Voronoi cells as the orbital segments. For example, for star 1 in Fig. 1, the time spent by the star in each Voronoi cell along its orbit is given as Δti\Delta t_{i}. So, the probability of finding that star in the ithi^{\mathrm{th}} Voronoi cell is the time spent in that Voronoi cell, Δti\Delta t_{i}, divided by the time spent in the entire region, which is, Δti/(texittenter){\Delta t_{i}}/{\left(t_{\rm exit}-t_{\rm enter}\right)} as seen in Fig. 1. Eventually, a combined probability is calculated for each Voronoi cell, which is the sum of probabilities of all stars in each cell.

  5. 4.

    Step 5 – Comparing phase space density distributions: In this final step we compare the phase space distribution of the original data and the phase space distribution of the newly positioned stars. The phase space distribution comparison is done statistically by computing the likelihood. If the likelihood is not maximum then the entire process is repeated with new acceleration field parameters.

    Eventually, the orbital arc method will give the acceleration field corresponding to the maximum likelihood, which is the field that describes the true underlying acceleration of the MW. The distribution of likelihoods gives the statistical uncertainty.

Since the level of accuracy relies on the available data, we need the phase space coordinates of a sufficiently large number of stars. Hence, Gaia DR2 is aptly suited for the study.

2.2 Implementation: the smoothing kernel

In order to compare the phase space distributions of the original data and the repositioned stars, we have used Voronoi cells to get a smooth phase space density. This is achieved by computing the time stars spend in each Voronoi cell, as described in step 4 in Sect. 2.1. In Fig. 1, Δt\Delta t represents the time a star spends in a cell. The ratio of the time spent by a star in a Voronoi cell, Δti\Delta t_{i}, to the time that it spends in the entire region (see tentert_{\rm enter} and texitt_{\rm exit} in Fig. 1) gives the phase space density of this model.

The shapes and sizes of the regions in which we intend to calculate the accelerations are mainly motivated by the quality of 6D data. The shapes of these regions and the Voronoi cells used to smooth phase space111The Voronoi tessellation of the region is done in order to compare the original and the new phase space distributions. should be complementary to each other. For example, if the available data are of a spherical region, then a rectangular grid or cell is not the most optimal. Therefore, the best possible grid should coarsely follow the distribution of data. One of the best ways to achieve this is by Voronoi tessellations, and we have hence used this method for the paper. However, in principle, any similar grid can be used. We used a random small subset of the data of about 100\sim 100 stars to obtain the Voronoi cells.

Each grid-cell is described by two numbers: the closest tessellation centre in ordinary space and the closest tessellation centre in velocity space. These two indices are required to avoid combining velocity and distance data into a single quantity, because this kind of combination produces an additional free parameter that we wish to avoid. For example, by using 100100 data points to tessellate into a grid, we will have 1002=10 000100^{2}=10\,000 independent cells, which is usually sufficient to describe the phase space distribution of about 420 000\approx 420\,000 stars (i.e. 4242 stars per cell). For the current study, we have selected 100100 cells for each of position and velocity space, unless noted otherwise.

2.3 Implementation: flux limitedness

Flux-limited observational data are a natural constraint in large surveys. There are two common approaches to overcome this: a) to construct a volume-limited sample and discard some data, or b) to use all the data and add a weight to each point.

Most dynamical modelling methods are constructed based on the assumption that we are able to observe everything, i.e. the volume-limited approach. Some specifics of the present modelling allow us to use the advantage of increased amounts of data of the flux-limited selection, while essentially using the method constructed for the volume-limited approach. This approach is described further in this section.

A volume-limited selection is one in which both the stellar distance from an observer and absolute magnitudes of its stars are constrained by a flux limit of the sample. This grants that all of the stars would remain observable if we randomize their position in the region. Our aim is to combine volume-limited selections to acquire methodology that allows us to use flux-limited data. Let us denote mlimm_{\rm lim} as the completeness limit of the flux-limited sample. Then the corresponding absolute-magnitude limit MlimM_{\rm lim} and the distance limit dlimd_{\rm lim} are related by 5log10dlim=mlimMlim+55\log_{10}d_{\rm lim}=m_{\rm lim}-M_{\rm lim}+5 (at the moment we ignore the attenuation correction). It is possible to construct a volume-limited sample by selecting only stars that have M<MlimM<M_{\rm lim} and d<dlimd<d_{\rm lim}. The same applies if we use an additional cut from higher absolute magnitudes, leaving MM in the range MlimΔM<MMlimM_{\rm lim}-\Delta M<M\leq M_{\rm lim}. Following the denotations from Kipper et al. (2019a), the observed phase space density as a function of phase space coordinates (𝐪{\bf q}) for a volume-limited sample can now be written as pobs(𝐪|Mlim,dlim)p_{\rm obs}({\bf q}|M_{\rm lim},d_{\rm lim}), and the model one as p(𝐪|Mlim,dlim,ζ)p({\bf q}|M_{\rm lim},d_{\rm lim},\zeta). Here MlimM_{\rm lim} and dlimd_{\rm lim} are not independent, but tied to the absolute-magnitude definition. For the correct gravitational acceleration parameters ζ\zeta, and irrespective of the absolute-magnitude limit, these distributions must match:

p(𝐪|Mlim,dlim,ζ)=pobs(𝐪|Mlim,dlim).p({\bf q}|M_{\rm lim},d_{\rm lim},{\bf\zeta})=p_{\rm obs}({\bf q}|M_{\rm lim},d_{\rm lim}). (10)

If this relation matches for each small volume-limited sample, then the relation must hold for the sum (or integral) of these small volume-limited samples as well:

p(𝐪|Mlim,dlim(Mlim),ζ)dMlim=\displaystyle\int p({\bf q}|M_{\rm lim},d_{\rm lim}(M_{\rm lim}),{\bf\zeta})\,{\rm d}M_{\rm lim}=
=pobs(𝐪|Mlim,dlim(Mlim))dMlim.\displaystyle=\int p_{\rm obs}({\bf q}|M_{\rm lim},d_{\rm lim}(M_{\rm lim}))\,{\rm d}M_{\rm lim}. (11)

This means that we may integrate an orbit until the apparent magnitude of the corresponding star reaches the limiting magnitude mlimm_{\rm lim} due to its changing distance, and smooth the position of the star along its orbit within that limit. In Sect. 5.1 we test the validity of this approach.

2.4 Requirements for data

An integral part of the method is orbit calculation. This has two ingredients: the proposed acceleration function and initial conditions for the orbits. As an analytical expression the first one is infinitely precise for each likelihood evaluation. The second one is as precise as the data allow. Imprecisions in the data are amplified by the orbit integration, i.e. ΔxΔx0+tΔv\Delta x\sim\Delta x_{0}+t\Delta v, where Δ\Delta denotes uncertainty for positions and velocities respectively. This shows that the uncertainties accumulate with time; hence the position of a star is unknown in some cone. Due to uncertainties (especially heteroscedastic ones) in the Gaia data combined with smoothing phase space, we may reconstruct imprecise orbits, which will introduce a bias in the acceleration. The simplest way to avoid these problems is to use maximally precise data.

The second requirement is to have a sufficient amount of data. This is needed to describe the phase space density sufficiently precisely. Assuming that the data are very precise, the only source of uncertainty is the Poisson noise from the sampling.

3 Observational data

3.1 Construction of the data sample

Six-dimensional high-quality phase space coordinates in the SN are now available from Gaia satellite Data Release 2 for a significant number of stars. At present there are three catalogues available based on the Gaia measurements and including estimated star distances: the Gaia Collaboration catalogue (Lindegren et al., 2018), the StarHorse project catalog, SH, (Anders et al., 2019) and the Schönrich catalog, Sc, (Schönrich et al., 2019). There is a known issue concerning the zero point of parallaxes from the Gaia Collaboration, which is overcome in the latter two catalogues. Therefore we selected these two catalogues as our main sources of input data and calculated our results for both of them separately. To calculate gravitational acceleration, we need to know mass density gradients. Although the main source of density gradients results from the smooth density distribution of the MW, selection effects can produce artificial gradients. The two dominant ingredients for this kind of selection effects are Malmquist bias (covered in the previous section) and dust attenuation. To suppress the effects from dust attenuation, we use 2MASS (Skrutskie et al., 2006) catalogue JJ-band magnitudes where extinction is negligible.

The cross-match between the Anders et al. (2019) SH and 2MASS catalogues gave 6 964 515 entries; between the Schönrich et al. (2019) Sc and 2MASS catalogues there were 6 519 209 matches. We constrained the input magnitudes in such a way that the Gaia GG-band completeness (being affected by dust attenuation) has substantially less effect than our selection based on the JJ passband (being nearly attenuation free), i.e. P(G>Glim|J<Jlim)1P(G>G_{\rm lim}|J<J_{\rm lim})\ll 1. The apparent-magnitude data within 0.5kpc0.5~{}{\rm kpc} from the Sun for our selected sample are shown in Fig. 2. A strong correlation between the GG- and JJ-band magnitudes catches the eye. The JJ-band limit JlimJ_{\rm lim} was fixed to a value where the distribution of brighter stars in the GG band ends before reaching the Gaia spectroscopic completeness limit GlimG_{\rm lim}. This is shown as a green line in the left-hand panel and the corresponding probability density distribution p(G|J<Jlim)dGp(G|J<J_{\rm lim}){\rm d}G on the right-hand panel. The fraction of GG magnitudes crossing GlimG_{\rm lim} is 8×1048\times 10^{-4} for the adopted Jlim=10.25J_{\rm lim}=10.25; hence we conclude that our sample is almost independent of the Gaia completeness limit and dust attenuation.

Refer to caption
Figure 2: Distribution of apparent magnitudes of all stars within 0.50.5 kpc from the Sun. The GG-band magnitudes are from the Gaia data and the JJ-band magnitudes are from the 2MASS survey. The red horizontal line and the green vertical line depict the spectroscopic completeness limit and the limiting magnitude JlimJ_{\rm lim} respectively of our main sample. The right-hand panel shows the distribution of all stars from Gaia. The black line shows all the stars and the green line shows only those with magnitudes brighter than JlimJ_{\rm lim}. The distribution of our sample of stars drops before reaching the Gaia completeness limit. Only a fraction of 0.00080.0008 stars have a higher GG-band magnitude; therefore we choose our sample based on 2MASS photometry.

The smooth acceleration distribution of the MW is taken as an input in modelling process and it does not include local potential wells of stellar clusters. Hence, we cannot describe the motion of stars within clusters and must exclude these cluster stars from our sample. We excluded all stars that appeared to be cluster members in catalogues by Cantat-Gaudin et al. (2018) or the Gaia Collaboration et al. (2018). In total, 993993 stars or about 0.20.2 per cent of stars from the final selection were excluded.

3.2 Selection of the region

In the paper where we presented the method and tested it on simulation data (Kipper et al., 2019a), we aimed to use rather small regions in order to have a simple analytical form for acceleration vector components. In the current paper, we selected a larger region to suppress Poisson noise and to increase the region size in the radial direction to have a stronger basis to also estimate the first derivative of the radial acceleration. This changes our approach somewhat: instead of using a simple form for accelerations, we now try to model the underlying acceleration field with a well-motivated analytical form.

Thus, due to available data, instead of using several small regions as we did in Kipper et al. (2019a), we selected one larger region, as shown in the schematic in Fig. 1. Our main aim was to recover the acceleration field in the plane of the Galaxy; hence we constructed a region where accelerations in the MW plane have a longer time to act on stars. In the vertical direction, density gradients are much steeper and one may expect that the corresponding accelerations may have also more complex forms. To avoid using more complex accelerations in vertical directions, we selected a thin region.

The region size is selected to balance two previous effects: maximally small to have a simple acceleration form and maximally close to keep the observational uncertainties low, and at the same time maximally large to let acceleration act for a sufficiently long time in the model. The boundary of the selected region is described by a biaxial ellipsoid:

(Δxxmax)2+(Δyymax)2+(Δzzmax)2=1,\left(\frac{\Delta x}{x_{\rm max}}\right)^{2}+\left(\frac{\Delta y}{y_{\rm max}}\right)^{2}+\left(\frac{\Delta z}{z_{\rm max}}\right)^{2}=1, (12)

with xmax=ymax=0.494kpcx_{\rm max}=y_{\rm max}=0.494\,{\rm kpc} and zmax=0.218kpcz_{\rm max}=0.218\,{\rm kpc}. Here Δx\Delta x, Δy\Delta y and Δz\Delta z denote the coordinates from the centre of the region. The centre of the region is at (x,y,z)=(8.3,0.0,0.0)(x,y,z)=(-8.3,0.0,0.0) in kpc. The position of the Sun with respect to the region centre is (0.040,0.0,0.027)(-0.040,0.0,0.027) in kpc. Within this region there are 417 727417\,727 stars when using the Schönrich et al. (2019) catalogue (Sc), and 426 767426\,767 stars when using the StarHorse (SH) catalogue. Larger regions would require the use of a precise selection function, which would complicate the analysis.

4 Results

We calculated gravitational acceleration in the region around the SN as described in Sect. 3.2 using the method and its implementation explained in Sect. 2. In order to decipher various aspects of the acceleration field (e.g. deviations from axisymmetry), we used different functional forms to describe the underlying acceleration.

4.1 Calculated acceleration components

In our first attempt to model the acceleration in the region we did not specify a design-based form of an overall gravitational potential of the MW. Instead we assumed that any acceleration form can be approximated with their Taylor expansions Eqs. (7) – (9) and we fit the coefficients of this acceleration (AxA_{x}, Ax,xA_{x,x}, Ax,yA_{x,y}, Ax,zA_{x,z}, AyA_{y}, Ay,xA_{y,x}, Ay,yA_{y,y}, Ay,zA_{y,z}, AzA_{z}, Az,xA_{z,x}, Az,yA_{z,y}, Az,zA_{z,z}). This way of modelling is powerful because it allows us to not only model the acceleration in a tiny region, but in principle the entire MW if we can get the overall gravitational potential. We fit a total of 1212 free parameters, AiA_{i} and Ai,jA_{i,j} for the flux-limited samples of stars within the selected region (see Sect. 3.2) for both the Sc and SH catalogues of Gaia DR2 (for more details see Sect. 3.1).

We used 100100 random points to describe the grid; hence, there are 42\approx 42 stars per grid bin. The fitting was done with the Multinest code (Feroz & Hobson, 2008; Feroz et al., 2009; Feroz et al., 2013) using 500500 live points. To include the randomness caused by the gridding, we ran the code eight times and averaged the posterior distribution of different runs. All the modelling was done in this way, unless noted otherwise. The priors of the Bayesian modelling were chosen to be of uniform distribution with the limiting values provided in Table 1. In the table we give the posterior distribution of each parameter ζ\zeta with five quantiles positioned at P(ζ)={0.023,0.159,0.500,0.841,0.977}P(\zeta)=\{0.023,0.159,0.500,0.841,0.977\}.

Previous studies have shown that the Sun is not located precisely at the centre of the Galactic plane, but is about 25pc25\,{\rm pc} away from it (Bland-Hawthorn & Gerhard, 2016). Thus, there must be an acceleration component in the vertical direction, as confirmed in e.g. Kipper et al. (2018) based on dynamics. In Table 1 our estimation of the vertical acceleration AzA_{z} and its gradient in the zz-direction Az,zA_{z,z} are given. Using these two values and by making a linear approximation at distances close to the plane, we deduce that we are located at zAz/Az,z={11176+33(SH),11766+58(Sc)}z_{\odot}\approx A_{z}/A_{z,z}=\{-111^{+33}_{-76}({\rm SH}),\,-117^{+58}_{-66}({\rm Sc})\} pc from the vertical coordinate value defined as having zero vertical acceleration in contrast to the symmetry-defined centre.

The Poisson equation combines the gravitational potential and total mass density. By using calculated acceleration components in the Poisson equation, we can compute the average total matter density in our selected region as:

2Φ=Ax,xAy,yAz,z=4πGρtotal,\nabla^{2}\Phi=-A_{x,x}-A_{y,y}-A_{z,z}=4\pi G\rho_{\rm total}, (13)

where Φ\Phi is the gravitational potential and ρtotal\rho_{\rm total} is the total mass density inside the region. Calculated Taylor expansion fit components for two different Gaia catalogues give us ρtotal=0.0700.016+0.016Mpc3\rho_{\rm total}=0.070^{+0.016}_{-0.016}{\rm\,M_{\odot}\,pc^{-3}} (SH catalogue) and ρtotal=0.0690.023+0.016Mpc3\rho_{\rm total}=0.069^{+0.016}_{-0.023}{\rm\,M_{\odot}\,pc^{-3}} (Sc catalogue). The full probability density distribution of the total matter density ρtotal\rho_{\rm total} can be seen in Fig. 3. One must bear in mind, that this total density value applies as the average in this region (extent in the zz-direction is 2×0.222\times 0.22 kpc). In order to describe the changes in the vertical component of the acceleration, we need a more sophisticated form of acceleration as the linear form cannot capture quick density changes along the zz-direction. Therefore, if we use another form by assuming axisymmetry with respect to the centre, then the number of free parameters can be significantly reduced and more concrete conclusions can be made. Selected Taylor expansion might not fully grasp all the details of the vertical structure, since it is described with just one free parameter (Az,zA_{z,z}).

Refer to caption
Figure 3: The figure shows the average matter density in the solar neighbourhood and is compared with the results from Bienaymé et al. (2014); McKee et al. (2015); Kipper et al. (2018). These results do not match very well because they use different datasets and different assumptions of the underlying acceleration. The high uncertainty in the calculated results is due to the optimization of the selected acceleration form to determine accelerations in Galactic plane. Note that this is not the vertical component, which is usually used to determine the overall matter density.

4.2 Deviations from a simple axisymmetric MW model

In case of a stationary axisymmetric MW, the acceleration component along the direction of Galactic rotation ay(Δx,Δy=0,Δz)=0a_{y}(\Delta x,\Delta y=0,\Delta z)=0 and equipotential curves are concentric circles. The median values of acceleration computed within the selected region using the coordinates (x,y,z)=(8.3,0,0)(x,y,z)=(-8.3,0,0) kpc as the centre are 306 and 284km2s2kpc1284\,{\rm km^{2}\,s^{-2}\,kpc^{-1}} for the SH and Sc catalogues respectively. Results of these calculations along with 1σ1\sigma and 2σ2\sigma limits are shown in Fig. 4 and the used priors are given in Table 2. They are designated as ’Sc, flux’ and ’SH, flux’. None of the 27 74827\,748 posterior samples from multinest show negative AyA_{y} values. Thus, the results are not consistent with axisymmetry.

Based on the assumption that equipotential curves are concentric circles, we derived the radius of this circle. The radii are 3.4kpc3.4\,{\rm kpc} for the SH catalogue and 3.2kpc3.2\,{\rm kpc} for the Sc catalogue. Most of the posterior distribution had values lower than 8.38.3 kpc, i.e. P(R>8.3kpc)={0.048(Sc), 0.11(SH)}P(R_{\odot}~{}>~{}8.3\,{\rm kpc})~{}=~{}\{0.048({\rm Sc}),\,0.11({\rm SH})\}. Hence, the ’acceleration centre’ is most likely closer to us than the GC and equipotential curves have higher curvature than one would expect for the distance to the Galactic centre. Thus we conclude that axisymmetric potential distribution is not valid at SN, and interpret it as an argument to support the presence of a rather massive central bar.

As already explained in Sect. 5.1, we calculated the acceleration components assuming axisymmetry, by selecting the components aR,aza_{R},a_{z} to be in the form of Eqs. (4) – (6). During the fitting the solar distance RR_{\odot} was also taken as a free parameter. Taking the posterior in these fits close to R=8.3kpcR_{\odot}=8.3\,\mathrm{kpc}, we found the radial acceleration to be 6190160+70km2s2kpc1-6190^{+70}_{-160}\,{\rm km^{2}\,s^{-2}\,kpc^{-1}}, which corresponds to the circular velocity 227 km s-1. The combined estimate of the observed circular velocity at 8.3 kpc is somewhat larger, being 238±15kms1238\pm 15~{}{\rm km\,s^{-1}} (Bland-Hawthorn & Gerhard, 2016), but it is consistent with the calculated result within errors.

Refer to caption
Figure 4: The central panel shows the correlation between the centre of acceleration, RR_{\odot}, and the component of the acceleration vector, AyA_{y}, as described in Sec. 4.2. The top panel shows the distribution of RR_{\odot} for an axisymmetric fit. The brown point at 8.38.3~{}kpc shows the distance of the Sun to the centre of our Galaxy. This indicates that the curvature of the isopotential lines is very likely less than 8.38.3~{}kpc. The right-hand panel shows the distribution of the AyA_{y} component of the acceleration vector at the region centre. The green lines are for the overall posterior distribution and the red lines are for the subset where R8.3kpcR_{\odot}\approx 8.3\,{\rm kpc}. This figure highlights the necessity to include the non-axisymmetric component to fit the acceleration, since the default for the MW at (R=8.3,Ay=0)(R_{\odot}=8.3,A_{y}=0) does not account for what is observed.

4.3 Deriving the properties of the bar

To calculate the total mass of the bar, we assumed that spatial density distribution of the bar has the same form as that derived by Wegg et al. (2015):

ρ\displaystyle\rho =\displaystyle= Mbar4πx0y0z0exp([(xx0)c+(yy0)c]1/c)×\displaystyle\frac{M_{\rm bar}}{4\pi x_{0}y_{0}z_{0}}\exp{\left(-\left[\left(\frac{x}{x_{0}}\right)^{c_{\perp}}+\left(\frac{y}{y_{0}}\right)^{c_{\perp}}\right]^{1/c_{\perp}}\right)}\times (14)
×\displaystyle\times exp[zz0]Cut[RRoutσout]Cut[RinRσin]\displaystyle\exp{\left[-\frac{z}{z_{0}}\right]}{\rm Cut}\left[\frac{R-R_{\rm out}}{\sigma_{\rm out}}\right]{\rm Cut}\left[\frac{R_{\rm in}-R}{\sigma_{\rm in}}\right]
Cut(x)\displaystyle{\rm Cut}(x) =\displaystyle= {exp(x2)ifx>11ifx1.\displaystyle\begin{cases}\exp(-x^{2})&{\rm if\,}x>1\\ 1&{\rm if\,}x\leq 1.\end{cases} (15)

The values of the parameters x0,y0,z0,σin,σout,c,Rin,Routx_{0},y_{0},z_{0},\sigma_{\rm in},\sigma_{\rm out},c_{\perp},R_{\rm in},R_{\rm out} were also taken to be the same as those derived by Wegg et al. (2015). In this form Wegg et al. (2015) excluded symmetric parts of the Galaxy (e.g. bulge) by cut-off. By calculating tangential accelerations for this bar and fitting the calculated values with the values derived by us and referred to in the previous subsection, we derived that the mass of the bar (using the cut-off in previous equations) will be 0.410.08+0.071010M0.41^{+0.07}_{-0.08}10^{10}\mathrm{M}_{\odot} for the SH catalogue and 0.400.11+0.071010M0.40^{+0.07}_{-0.11}10^{10}\mathrm{M}_{\odot} for the Sc catalogue. Without the cut-off, by adopting their profile (and inferring their MbarM_{\rm bar}) the overall bar mass would be {1.590.31+0.27(SH), 1.550.43+0.29(Sc)} 1010M\{1.59^{+0.27}_{-0.31}({\rm SH}),\,1.55^{+0.29}_{-0.43}({\rm Sc})\}\,10^{10}\mathrm{M}_{\odot}.

In the previous subsection we concluded that the assumption that equipotential curves are circles is clearly not valid. Therefore, we assumed that these curves are confocal ellipses in the Galactic plane and then computed the acceleration due to the bar. An analytical form for accelerations describing the potential of the bar as confocal ellipsoids was chosen to be

ax\displaystyle a_{x} =\displaystyle= aRcosθ+AR,barΔx(Δx,Δy)\displaystyle a_{R}\cos\theta+A_{R,{\rm bar}}\Delta x(\Delta x^{\prime},\Delta y^{\prime}) (16)
ay\displaystyle a_{y} =\displaystyle= aRsinθ+AR,barΔy(Δx,Δy)\displaystyle a_{R}\sin\theta+A_{R,{\rm bar}}\Delta y(\Delta x^{\prime},\Delta y^{\prime}) (17)
az\displaystyle a_{z} =\displaystyle= Az+Az,zz+Az,RΔR+Az,RzzΔR,\displaystyle A_{z}+A_{z,z}z+A_{z,R}\Delta R+A_{z,Rz}z\Delta R, (18)

where aRa_{R} and ΔR\Delta R are given by Eqs. (5) and (6). The normalized vector components of the potential gradient of the confocal bar, Δx\Delta x^{\prime} and Δy\Delta y^{\prime}, are described by

Δx2a2+Δy2a2Lbar2=1.\frac{\Delta x^{\prime 2}}{a^{2}}+\frac{\Delta y^{\prime 2}}{a^{2}-L_{\rm bar}^{2}}=1. (19)

LbarL_{\rm bar} is the focal length of the equipotential curves and aa describes the size of the ellipsoid. The coordinate transformation from (x,y)(x,y) to (x,y)(x^{\prime},y^{\prime}) is done by rotating the original axes by an angle of 29.529.5^{\circ} which is the position angle of the major axis of the bar (Wegg et al., 2015). Results from these calculations are given in Table 3, they contain the coefficients obtained from the fits.

Refer to caption
Figure 5: The relation between acceleration from the axisymmetric component and from the bar component. The contours show 1σ1\sigma and 2σ2\sigma confidence intervals for the Anders et al. (2019) (SH) and Schönrich et al. (2019) (Sc) datasets. The strong correlation between them shows degeneracy of accelerations in the functional form of equations (16)-(18).
Refer to caption
Figure 6: The top panel depicts the degeneracy between the length of the bar and the acceleration from it. The bottom panel shows the fraction of bar acceleration. The degeneracy can be broken when additional information such as bar length is used. We used the bar length value from Wegg et al. (2015). The contours show 1σ1\sigma and 1σ1\sigma confidence intervals for the Anders et al. (2019) (SH) and Schönrich et al. (2019) (Sc) datasets.

When using accelerations in the form of Eqs. (16)–(18), substantial correlations exist in the modelled posterior samples (e.g. between ArA_{r} and Ar,barA_{r,{\rm bar}}). The largest correlation coefficient was found to be 1.01.0 between ArA_{r} and Ar,barA_{r,{\rm bar}} (see Fig. 5). We also found a strong correlation (correlation coefficient 0.85) between bar acceleration/total acceleration and its focal length as shown in Fig. 6. The rest of the correlations were much weaker, and the only other noticeable correlation was between ARA_{R} and AR,barA_{R,{\rm bar}} and the radial acceleration derivative AR,RA_{R,R} (correlation coefficient 0.260.26).

Currently we have only used the SN region to disentangle the bar parameters; hence, we were able to determine only some of the degenerate values. We were also able to determine that the sum of the radial acceleration due to the bar and axisymmetric components is constant, as seen in Fig. 5. Hence, if we know one then we can easily estimate the other.

Based on the results from Sect. 4.2, we modelled the tangential acceleration value AyA_{y}. From this, we can calculate the zz-component of the torque caused by the bar per solar mass using:

Tz=AyRGC{2450480+420(SH), 2390660+440(Sc)}km2s2T_{z}=A_{y}R_{\rm GC}\approx\{2450^{+420}_{-480}({\rm SH}),\,2390^{+440}_{-660}({\rm Sc})\}\,{\rm km^{2}\,s^{-2}}

or

Tz2470kms1kpcGyr1.T_{z}\approx 2470\,{\rm km\,s^{-1}\,kpc\,Gyr^{-1}}.

Here RGCR_{\rm GC} is our physical distance from the Galactic centre (instead of the modelled radius of curvature of equipotential curves RR_{\odot}). The degeneracy is because a long bar closer to us and a short massive bar engender the same force, making it difficult to distinguish the two scenarios. This is seen in Fig. 6 where the acceleration value due to the bar and the fraction of acceleration caused by the bar as a function of the length of the bar are given. The degeneracy can be broken when we fix the length of the bar from independent measurements. As an example, Wegg et al. (2015) estimated that the half-length of the bar is 4.6±0.3kpc4.6\pm 0.3\,{\rm kpc}. If we fix this value as LbarL_{\rm bar}, it gives the fraction of acceleration caused by the bar as about a third: 0.34±0.070.34\pm 0.07 in the case of the SH catalogue and 0.29±0.090.29\pm 0.09 in the case of the Sc catalogue.

5 Discussion and conclusion

5.1 Validity of the sample construction

To test how well the approach described in Sect. 2.3 is able to cope with flux-limited data, we applied our model to two sets: a flux-limited sample and a volume-limited sample. The volume-limited approach was tested with simulation data in Kipper et al. (2019a) and was found to be consistent. Since the results for the flux-limited sample agreed well with those of the volume-limited sample, we are confident that our model is very suitable for the current case.

The acceleration components used for this test are in the axisymmetric form of Eqs. (4) – (5). The geometry of the region was biaxial ellipsoid in the form of Eq. (12), but its selection and modelling had some differences: the sample was limited by the absolute JJ-magnitude value of 1.2m1.2^{\rm m}, yielding 54 81954\,819 stars. The grid was constructed by using 7070 random sample points, and fitting was done eight times to include the uncertainty from the gridding randomness.

The results of the test calculations for volume- and flux-limited selections from the Sc catalogue are given in Table 2, where calculated acceleration components are given with labels ‘Sc, vol’ and ‘Sc, flux’. The most interesting acceleration components are radial acceleration aRa_{R} and vertical acceleration aza_{z} (see their main parameters ARA_{R} and AzA_{z}). For the volume-limited sample AR=6128±199km2s2kpc1A_{R}=-6128\pm 199\,{\rm km^{2}s^{-2}kpc^{-1}} and Az=183±106km2s2kpc1A_{z}=183\pm 106\,{\rm km^{2}s^{-2}kpc^{-1}}, for the flux-limited sample AR=6181±82km2s2kpc1A_{R}=-6181\pm 82\,{\rm km^{2}s^{-2}kpc^{-1}} and Az=203±48km2s2kpc1A_{z}=203\pm 48\,{\rm km^{2}s^{-2}kpc^{-1}}. The smaller errors in the flux-limited sample are due to the larger data sample. The results are clearly consistent and we may conclude that our approach to cope from here on with the flux-limited sample, described in Sect. 2.3, is valid.

5.2 Time dependence of acceleration due to the bar

During calculations of stellar orbits (see selected analytical forms for acceleration) we assume that accelerations do not have an explicit time dependence. However, it is known that about a quarter of galaxies contain a more or less prominent bar (Cheung et al., 2013); in the case of the MW a central bar was introduced by de Vaucouleurs (1964). A rotating bar would violate this assumption of our modelling.

To test how much a bar would influence our results, we used the same simulation (the barred one) from Garbari et al. (2011) as was used in Kipper et al. (2019a). We selected a region close to the solar radius, with an angle between the major axis of the bar and direction to the centre of the region 30\approx 30^{\circ} and fitted the acceleration components (7) – (9) (Taylor expansion) with our model. We expect that including the tangential component of the acceleration due to the bar which is changing in time would give us a somewhat wrong acceleration direction. We found that the acceleration vector was directed away by 3.27±2.233.27\pm 2.23^{\circ} from the Galactic centre. The corresponding true angle calculated directly from the simulation gravitational potential was 2.212.21^{\circ}. The difference between the true and calculated values is smaller than the 1σ1\sigma error of the calculated value. Hence the effect of the time dependence of the bar in this case is not so significant.

Another approach to estimate the effect of a time dependent gravitational potential is to use available data from the literature. The average angular speed of the bar is about 40kms1kpc1\sim 40\,{\rm km\,s^{-1}kpc^{-1}}, although there is significant uncertainty in this value (see Sect. 1). The angular speed of the Sun is 30kms1kpc1\simeq 30\,{\rm km\,s^{-1}kpc^{-1}}(Bland-Hawthorn & Gerhard, 2016). The strong similarity between these two values suggests that the potential of the bar near the Sun does not change very fast. A hypothetical star moving with a speed of 220kms1220\,{\rm km\,s^{-1}} passes the half box-size distance of 0.50.5 kpc within 2.3\sim 2.3 Myr. Within this time, the angle of the bar orientation with respect to our comoving location changes only by 2.3Myr×(4030)kms1kpc11.42.3\,\mathrm{Myr}\,\times\,(40-30)\,\mathrm{km\,s^{-1}kpc^{-1}}\approx 1.4^{\circ}. If we assume that the angle between us and the major axis of the bar is θ0=30\theta_{0}=30^{\circ} and the ’tip of the bar’ is about L=5L=5 kpc away from the centre of the Galaxy222We make an approximation that the mass of the bar is a point mass at the tip of the bar. This gives an upper limit for the bar influence. then our distance to the tip of the bar is

w2=L2+R22LRcosθ0.w^{2}=L^{2}+R_{\odot}^{2}-2LR_{\odot}\cos{\theta_{0}}. (20)

The force due to the bar changes within 2.32.3 Myr maximally by

ΔFF=1FdFdwdwdθ0dθ0dtΔt2LRsinθ0w2Δθ00.046.\frac{\Delta F}{F}=\frac{1}{F}\,\frac{{\rm d}F}{{\rm d}w}\,\frac{{\rm d}w}{{\rm d}\theta_{0}}\,\frac{{\rm d}\theta_{0}}{{\rm d}t}\Delta t\approx\frac{2LR_{\odot}\sin\theta_{0}}{w^{2}}\Delta\theta_{0}\approx 0.046. (21)

Hence, the force due to the bar changes by about 55 per cent if the force due to the bar is not steeper than w2\propto w^{-2} and the bar dominates the potential. If it does not, then the result must be multiplied by the acceleration fraction of the bar. This can be considered as a component of systematic uncertainty. While calculating the orbital arcs for stars within the selected region, the time dependence of accelerations due to the bar has quite a small effect. Therefore in the current study we ignore this effect.

5.3 Influence of uncertainties in input data

The input to this modelling does not include uncertainties. The resulting uncertainties are statistical in nature and include only sampling errors seen from the likelihood equation (7) of Kipper et al. (2019a). In order to see how observational uncertainties influence our results, we randomized phase space coordinates of stars according to their uncertainties, reconstructed the selection sample as described in Sect. 3, and remodelled the selected region. To account for the randomness in this process, we modelled the SN 4747 times and combined the corresponding posterior distributions. The results of the calculations are shown in Table 2 with the label ‘Sc, rnd’ after the variable name. Comparing calculated accelerations with labels ‘Sc, rnd’ and ‘Sc, flux’, it is seen that randomization had very little effect on the results. We conclude that uncertainties can be ignored for this selection.

Another source of error can be due to the gridding approach employed in this study (see Sect. 2.2). Since there is randomization, we must include the noise caused by it. We rerun each modelling eight times to include the source of noise. All of these runs had similar posterior distributions; hence we are certain that gridding does not introduce large artificial uncertainties. To include the gridding uncertainties, we combined the posterior distributions of randomized grid runs.

5.4 Conclusions

In this paper, we have applied the orbital arc method (Kipper et al., 2019a) to Gaia DR2 and modelled the acceleration along the plane of the Galactic disc. We approximated the acceleration in the solar neighbourhood with various functional forms and came to the following conclusions:

  1. 1.

    There are very few systematic biases between the Gaia DR2 datasets compiled by Schönrich et al. (2019) and Anders et al. (2019). Both the datasets give consistent results.

  2. 2.

    The distribution of axisymmetric gravitational acceleration does not account for the observed acceleration for the standard distance of the Sun from the Galactic centre R8.3kpcR_{\odot}\approx 8.3\,{\rm kpc}. The curvature of the isopotential lines is smaller than the standard RR_{\odot}, implying that there is a component of the Galactic bar causing this acceleration.

  3. 3.

    The acceleration vector in the solar neighbourhood is not directed towards the centre of the Galaxy. There is a significant component of the acceleration directed away from the Galactic centre. We propose that this is caused by the massive central bar. Based on our model, we calculate the torque to be 2400km2s2\sim 2400\,{\rm km^{2}\,s^{-2}} per solar mass.

  4. 4.

    Based on the assumption that isopotential surfaces of the bar are confocal ellipses, we estimate that about one third of the total acceleration in the solar neighbourhood is caused by the bar. In this computation we use the estimate of the length of the bar of Wegg et al. (2015).

  5. 5.

    Finally, using our model, we estimated the mass of the bar as (1.6±0.3)×1010M(1.6\pm 0.3)\times 10^{10}\,\mathrm{M}_{\odot}, using the density distribution parameters from Wegg et al. (2015).

Acknowledgements

We thank the referee for helpful comments and suggestions. We thank the StarHorse core team (F. Anders, A. Queiroz , B. Santiago, A. Kalathyan, C. Chiappini) for providing their data, and G. Monari for helpful comments about the paper. This work was supported by institutional research funding IUT26-2, IUT40-2 and PUTJD907 of the Estonian Ministry of Education and Research. We acknowledge the support by the Centre of Excellence “Dark side of the Universe” (TK133) and by the grant MOBTP86 financed by the European Union through the European Regional Development Fund. This work has made use of data from the European Space Agency (ESA) mission Gaia (https://www.cosmos.esa.int/gaia), processed by the Gaia Data Processing and Analysis Consortium (DPAC, https://www.cosmos.esa.int/web/gaia/dpac/consortium). Funding for the DPAC has been provided by national institutions, in particular the institutions participating in the Gaia Multilateral Agreement. This publication makes use of data products from the Two Micron All Sky Survey, which is a joint project of the University of Massachusetts and the Infrared Processing and Analysis Center/California Institute of Technology, funded by the National Aeronautics and Space Administration and the National Science Foundation.

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Appendix A Tables

Table 1: The modelling of the acceleration function described with Eqs. (7)-(9) and using datasets from Schönrich et al. (2019) (Sc) or Anders et al. (2019) (SH). We use acceleration units of km2s2kpc1{\rm km^{2}\,s^{-2}\,kpc^{-1}}, which differ from the more intuitive kms1Gyr1{\rm km\,s^{-1}\,Gyr^{-1}} by about 2 per cent. The values of PP represent quantiles of the posterior distribution.
Variable Unit P=0.02P=0.02 P=0.16P=0.16 Median P=0.84P=0.84 P=0.98P=0.98 Lower prior limit Higher prior limit
AxA_{x} (SH) km2{}^{2}\,s-2kpc-1 6109.43 6178.27 6250.33 6382.74 6468.32 -10000 10000
AxA_{x} (Sc) km2{}^{2}\,s-2kpc-1 6026.12 6102.47 6195.79 6327.5 6420.91 -10000 10000
AyA_{y} (SH) km2{}^{2}\,s-2kpc-1 222.24 259.31 306.37 385.33 445.89 -10000 10000
AyA_{y} (Sc) km2{}^{2}\,s-2kpc-1 189.42 238.87 283.55 339.59 412.18 -10000 10000
AzA_{z} (SH) km2{}^{2}\,s-2kpc-1 138.96 175.95 211.06 254.66 295.01 -5000 5000
AzA_{z} (Sc) km2{}^{2}\,s-2kpc-1 95.85 135.28 186.81 245.17 286.13 -5000 5000
Ax,xA_{x,x} (SH) km2{}^{2}\,s-2kpc-2 252.69 658.7 1152.87 1764.86 2306.3 -3000 5000
Ax,xA_{x,x} (Sc) km2{}^{2}\,s-2kpc-2 -498 318.77 1109.62 1631.22 2088.79 -3000 5000
Ax,yA_{x,y} (SH) km2{}^{2}\,s-2kpc-2 -34.2 853.24 1867.96 2920.27 3606.84 -4000 4000
Ax,yA_{x,y} (Sc) km2{}^{2}\,s-2kpc-2 -479.88 494.3 1511.29 2379.45 3128.42 -4000 4000
Ax,zA_{x,z} (SH) km2{}^{2}\,s-2kpc-2 -1948.43 -1760.52 -1406.23 -860.97 -171.53 -2000 2000
Ax,zA_{x,z} (Sc) km2{}^{2}\,s-2kpc-2 -1945.27 -1748.13 -1339.24 -725.73 2.09 -2000 2000
Ay,xA_{y,x} (SH) km2{}^{2}\,s-2kpc-2 -702.07 -424.69 -59.88 253.95 538.2 -2000 2000
Ay,xA_{y,x} (Sc) km2{}^{2}\,s-2kpc-2 -541.84 -283.02 -28.31 275.48 640.52 -2000 2000
Ay,yA_{y,y} (SH) km2{}^{2}\,s-2kpc-2 -3505.68 -2862.34 -2148.94 -1487.17 -935.21 -5000 2000
Ay,yA_{y,y} (Sc) km2{}^{2}\,s-2kpc-2 -3662.39 -2914.14 -2154.12 -1566.75 -933.65 -5000 2000
Ay,zA_{y,z} (SH) km2{}^{2}\,s-2kpc-2 -1975.02 -1885.74 -1696.72 -1372.29 -860.07 -2000 2000
Ay,zA_{y,z} (Sc) km2{}^{2}\,s-2kpc-2 -1957.05 -1817.54 -1463.88 -864.12 -129.38 -2000 2000
Az,xA_{z,x} (SH) km2{}^{2}\,s-2kpc-2 -494.93 -145.76 155.8 428.63 700.61 -2000 2000
Az,xA_{z,x} (Sc) km2{}^{2}\,s-2kpc-2 -48.17 184.64 429.13 669.57 906.36 -2000 2000
Az,yA_{z,y} (SH) km2{}^{2}\,s-2kpc-2 -636.93 -50.74 562.24 1220.58 1772.55 -2000 2000
Az,yA_{z,y} (Sc) km2{}^{2}\,s-2kpc-2 -304.58 102.45 501.94 893 1284.27 -2000 2000
Az,zA_{z,z} (SH) km2{}^{2}\,s-2kpc-2 -3066.65 -2536.04 -1857.43 -1224.14 -664.61 -6000 0
Az,zA_{z,z} (Sc) km2{}^{2}\,s-2kpc-2 -3556.61 -2789.1 -1651.53 -1081.78 -588.78 -6000 0
Table 2: The modelling of the acceleration function aiming to describe an axisymmetric disc with a possible tangential component using equations (1) - (6) and using datasets from Schönrich et al. (2019) (Sc) or Anders et al. (2019) (SH). The extra denotations after the variable name show specifics of the modelling: ’flux’ denotes that the sample was flux-limited and ’vol’ volume-limited; ’rnd’ had phase space values randomized according to observational uncertainties. In the case of the random sample, the posterior distribution is averaged over 4747 different runs. The volume-limited sample fit was done with about a tenth of the number of data, which is the cause of reduced accuracy and precision.
Variable Unit P=0.02P=0.02 P=0.16P=0.16 Median P=0.84P=0.84 P=0.98P=0.98 Lower prior limit Higher prior limit
ARA_{R} (Sc, vol) km2 s-2kpc-1 -6495.2 -6328.1 -6127.9 -5942.7 -5785.8 -15000 15000
ARA_{R} (Sc, flux) km2 s-2kpc-1 -6466.8 -6300.4 -6181.2 -6110.2 -6043.4 -15000 15000
ARA_{R} (SH, flux) km2 s-2kpc-1 -6367.9 -6294.8 -6214 -6135.1 -6062.6 -15000 15000
ARA_{R} (Sc, rnd) km2 s-2kpc-1 -6656.2 -6517.4 -6391.2 -6284.1 -6188.4 -15000 15000
RR_{\odot} (Sc, vol) kpc 1.6 2.1 3.6 9.9 17.2 0.1 20
RR_{\odot} (Sc, flux) kpc 2 2.4 3.2 5 12.1 0.1 20
RR_{\odot} (SH, flux) kpc 1.7 2.2 3.4 6.3 14.6 0.1 20
RR_{\odot} (Sc, rnd) kpc 1.5 1.8 2.2 3.2 6.6 0.1 20
AzA_{z} (Sc, vol) km2 s-2kpc-1 3.5 90.6 183.5 300.3 391 -5000 5000
AzA_{z} (Sc, flux) km2 s-2kpc-1 96.7 151.6 203.5 249.2 287.7 -5000 5000
AzA_{z} (SH, flux) km2 s-2kpc-1 114.7 152.8 195.5 239.3 280.9 -5000 5000
AzA_{z} (Sc, rnd) km2 s-2kpc-1 105.7 155.8 205 256.4 299.6 -5000 5000
Az,zA_{z,z} (Sc, vol) km2 s-2kpc-2 -6815.1 -5339.3 -3731.1 -1644.7 -253.7 -8000 0
Az,zA_{z,z} (Sc, flux) km2 s-2kpc-2 -3590.3 -2872.3 -2083.4 -1427.1 -755.2 -8000 0
Az,zA_{z,z} (SH, flux) km2 s-2kpc-2 -3042.2 -2285.3 -1512 -786.5 -262.2 -8000 0
Az,zA_{z,z} (Sc, rnd) km2 s-2kpc-2 -3478.4 -2701.8 -1866.7 -1088.7 -428.3 -8000 0
Az,RA_{z,R} (Sc, vol) km2 s-2kpc-2 -1919.5 -1542 -991.9 -232 282.9 -5000 5000
Az,RA_{z,R} (Sc, flux) km2 s-2kpc-2 -742.1 -446.4 -145.4 176.9 473 -5000 5000
Az,RA_{z,R} (SH, flux) km2 s-2kpc-2 -817.1 -558.7 -299.3 -1.2 311.4 -5000 5000
Az,RA_{z,R} (Sc, rnd) km2 s-2kpc-2 -949.9 -653.9 -373.8 -43.5 320.3 -5000 5000
Az,RzA_{z,Rz} (Sc, vol) km2 s-2kpc-3 -4627.4 -3272.8 -104.6 3125.1 4569 -5000 5000
Az,RzA_{z,Rz} (Sc, flux) km2 s-2kpc-3 -4702.6 -3640.8 -1332.2 1973.6 4105.8 -5000 5000
Az,RzA_{z,Rz} (SH, flux) km2 s-2kpc-3 -4814.5 -3985.5 -1707.9 2408 4426 -5000 5000
Az,RzA_{z,Rz} (Sc, rnd) km2 s-2kpc-3 -4407.6 -2608.8 788.9 3471.8 4683.1 -5000 5000
AR,RA_{R,R} (Sc, vol) km2 s-2kpc-2 -2342.4 -938.9 909.7 2490.4 3444 -4000 4000
AR,RA_{R,R} (Sc, flux) km2 s-2kpc-2 -2591.1 -1809.7 -995.1 -102 975.3 -4000 4000
AR,RA_{R,R} (SH, flux) km2 s-2kpc-2 -2726.1 -1666.2 -500.3 531 1372.3 -4000 4000
AR,RA_{R,R} (Sc, rnd) km2 s-2kpc-2 -2591.9 -1721.2 -763.8 455.6 1799.6 -4000 4000
AyA_{y} (Sc, vol) km2 s-2kpc-1 -345.2 -226.3 -65 67.7 177.8 -3000 3000
AyA_{y} (Sc, flux) km2 s-2kpc-1 157.2 208.5 288.5 341.5 385.5 -3000 3000
AyA_{y} (SH, flux) km2 s-2kpc-1 159.3 237.3 295.4 345.9 400.4 -3000 3000
AyA_{y} (Sc, rnd) km2 s-2kpc-1 134.6 187.3 247.5 309.6 393 -3000 3000
Table 3: The modelling of the acceleration function (16)–(18) aiming to describe the sum of the axisymmetric and confocal bar components. The datasets used from Schönrich et al. (2019) and Anders et al. (2019) are abbreviated as Sc and SH.
Variable Unit P=0.02P=0.02 P=0.16P=0.16 Median P=0.84P=0.84 P=0.98P=0.98 Lower prior limit Higher prior limit
ARA_{R} (SH) km2 s-2kpc-1 -5347.36 -4713.55 -3107.82 -1291.7 -513.77 -10000 0
ARA_{R} (Sc) km2 s-2kpc-1 -5508.89 -4889.42 -3195.73 -1344.89 -513.04 -10000 0
AR,RA_{R,R} (SH) km2 s-2kpc-2 234.31 766.59 1248.09 1717.45 2202.51 -5000 5000
AR,RA_{R,R} (Sc) km2 s-2kpc-2 -739.71 164.14 1195.15 1966.9 2599.58 -5000 5000
AzA_{z} (SH) km2 s-2kpc-1 111.05 150.27 202.37 248.64 287.65 -5000 5000
AzA_{z} (Sc) km2 s-2kpc-1 141.71 178.88 216.77 256.01 293.62 -5000 5000
Az,zA_{z,z} (SH) km2 s-2kpc-2 -3331.1 -2737.24 -2135.29 -1479.55 -897.58 -8000 0
Az,zA_{z,z} (Sc) km2 s-2kpc-2 -3090.27 -2461.84 -1856.71 -1156 -582.57 -8000 0
Az,RA_{z,R} (SH) km2 s-2kpc-2 -873.7 -597.21 -286.73 -6.01 237.43 -5000 5000
Az,RA_{z,R} (Sc) km2 s-2kpc-2 -933.1 -636.23 -345.07 -83.41 154.43 -5000 5000
Az,RzA_{z,Rz} (SH) km2 s-2kpc-3 -4352.62 -2373.53 1429.96 3747.56 4718.91 -5000 5000
Az,RzA_{z,Rz} (Sc) km2 s-2kpc-3 -4341.86 -2571.03 399.29 3137.3 4610.42 -5000 5000
AR,barA_{R,{\rm bar}} (SH) km2 s-2kpc-1 -5761.45 -4984.16 -3168.97 -1562.17 -952.39 6000 -6000
AR,barA_{R,{\rm bar}} (Sc) km2 s-2kpc-1 -5738.29 -4899.51 -3050.55 -1367.63 -737.13 6000 -6000
LbarL_{\rm bar} (SH) kpc 2.62 3.03 3.76 5.18 6.4 0.1 7
LbarL_{\rm bar} (Sc) kpc 2.16 2.72 3.54 5.02 6.32 0.1 7