Low thrust relative orbital transfer uses orbital motion equations (such as the Clohessy-Wiltshire equations that are very useful in planning rendezvous of the chaser with the target, published in 1962) to explain the differences in orbits and displacements of target and chaser spacecraft.
Low thrust relative orbital transfer uses orbital motion equations (such as the Clohessy-Wiltshire equations that are very useful in planning rendezvous of the chaser with the target, published in 1962) to explain the differences in orbits and displacements of target and chaser spacecraft.