Some data and simplifications, that can be used here :
- the target's orbit is circular
- the RTN position of the chaser is (30;10;10) m
- the mass of the chaser is 1000kg and the mass of the target is 8000kg
- the target has an altitude of 800e3 m
Hi all,
I'm curently meeting the following problem and can't figure it out by myself.
Assume we have to vehicles in space, a target and a chaser spacecraft . The target spacecraft defines the RTN frame of reference.
Given the position and velocity of the chaser in RTN-coordinates, how can I...