Given a velocity vector in the ecliptic inertial reference frame of a vessel orbiting the Moon (this vector is readily available in Orbiter), what transformation matrix, or series of transformation matrices, would provide the vessel's velocity vector in a reference frame fixed at the Moon's center (i.e. non-inertial and rotating with the Moon)?
Also, I have the same question regarding the similar transformation of position vector data.
Would appreciate any help. Thanks.
Also, I have the same question regarding the similar transformation of position vector data.
Would appreciate any help. Thanks.