Description of Galactocentric Coordinates Transformation

This document describes the mathematics behind the transformation from ICRS to Galactocentric coordinates. This is described in detail here on account of the mathematical subtleties and the fact that there is no official standard/definition for this frame. For examples of how to use this transformation in code, see the the Examples section of the Galactocentric class documentation.

We assume that we start with a 3D position in the ICRS reference frame: a Right Ascension, Declination, and heliocentric distance, \((\alpha, \delta, d)\). We can convert this to a Cartesian position using the standard transformation from Cartesian to spherical coordinates:

\[\begin{split}\begin{aligned} x_{\rm icrs} &= d\cos{\alpha}\cos{\delta}\\ y_{\rm icrs} &= d\sin{\alpha}\cos{\delta}\\ z_{\rm icrs} &= d\sin{\delta}\\ \boldsymbol{r}_{\rm icrs} &= \begin{pmatrix} x_{\rm icrs}\\ y_{\rm icrs}\\ z_{\rm icrs} \end{pmatrix}\end{aligned}\end{split}\]

The first transformations will rotate the \(x_{\rm icrs}\) axis so that the new \(x'\) axis points towards the Galactic Center (GC), specified by the ICRS position \((\alpha_{\rm GC}, \delta_{\rm GC})\):

\[\begin{split}\begin{aligned} \boldsymbol{R}_1 &= \begin{bmatrix} \cos\delta_{\rm GC}& 0 & -\sin\delta_{\rm GC}\\ 0 & 1 & 0 \\ \sin\delta_{\rm GC}& 0 & \cos\delta_{\rm GC}\end{bmatrix}\\ \boldsymbol{R}_2 &= \begin{bmatrix} \cos\alpha_{\rm GC}& \sin\alpha_{\rm GC}& 0\\ -\sin\alpha_{\rm GC}& \cos\alpha_{\rm GC}& 0\\ 0 & 0 & 1 \end{bmatrix}.\end{aligned}\end{split}\]

The transformation thus far has aligned the \(x'\) axis with the vector pointing from the Sun to the GC, but the \(y'\) and \(z'\) axes point in arbitrary directions. We adopt the orientation of the Galactic plane as the normal to the north pole of Galactic coordinates defined by the IAU (Blaauw et. al. 1960). This extra “roll” angle, \(\eta\), was measured by transforming a grid of points along \(l=0\) to this interim frame and minimizing the square of their \(y'\) positions. We find:

\[\begin{split}\begin{aligned} \eta &= 58.5986320306^\circ\\ \boldsymbol{R}_3 &= \begin{bmatrix} 1 & 0 & 0\\ 0 & \cos\eta & \sin\eta\\ 0 & -\sin\eta & \cos\eta \end{bmatrix}\end{aligned}\end{split}\]

The full rotation matrix thus far is:

\[\begin{split}\begin{gathered} \boldsymbol{R} = \boldsymbol{R}_3 \boldsymbol{R}_1 \boldsymbol{R}_2 = \\ \begin{bmatrix} \cos\alpha_{\rm GC}\cos\delta_{\rm GC}& \cos\delta_{\rm GC}\sin\alpha_{\rm GC}& -\sin\delta_{\rm GC}\\ \cos\alpha_{\rm GC}\sin\delta_{\rm GC}\sin\eta - \sin\alpha_{\rm GC}\cos\eta & \sin\alpha_{\rm GC}\sin\delta_{\rm GC}\sin\eta + \cos\alpha_{\rm GC}\cos\eta & \cos\delta_{\rm GC}\sin\eta\\ \cos\alpha_{\rm GC}\sin\delta_{\rm GC}\cos\eta + \sin\alpha_{\rm GC}\sin\eta & \sin\alpha_{\rm GC}\sin\delta_{\rm GC}\cos\eta - \cos\alpha_{\rm GC}\sin\eta & \cos\delta_{\rm GC}\cos\eta \end{bmatrix}\end{gathered}\end{split}\]

With the rotated position vector \(\boldsymbol{R}\boldsymbol{r}_{\rm icrs}\), we can now subtract the distance to the GC, \(d_{\rm GC}\), which is purely along the \(x'\) axis:

\[\begin{aligned} \boldsymbol{r}' &= \boldsymbol{R}\boldsymbol{r}_{\rm icrs} - d_{\rm GC}\hat{\boldsymbol{x}}_{\rm GC}.\end{aligned}\]

where \(\hat{\boldsymbol{x}}_{\rm GC} = (1,0,0)^{\mathsf{T}}\).

The final transformation accounts for the (specified) height of the Sun above the Galactic midplane by rotating about the final \(y''\) axis by the angle \(\theta= \sin^{-1}(z_\odot / d_{\rm GC})\):

\[\begin{split}\begin{aligned} \boldsymbol{H} &= \begin{bmatrix} \cos\theta & 0 & \sin\theta\\ 0 & 1 & 0\\ -\sin\theta & 0 & \cos\theta \end{bmatrix}\end{aligned}\end{split}\]

where \(z_\odot\) is the measured height of the Sun above the midplane.

The full transformation is then:

\[\boldsymbol{r}_{\rm GC} = \boldsymbol{H} \left( \boldsymbol{R}\boldsymbol{r}_{\rm icrs} - d_{\rm GC}\hat{\boldsymbol{x}}_{\rm GC}\right).\]

Examples:

For an example of how to use the Galactocentric frame, see Transforming positions and velocities to and from a Galactocentric frame.