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Formation keeping problem of satellite cluster during non-coplanar orbit transfer is studied in this paper. Geometric method model is used to describe the relative motion of satellites in the cluster non-coplanar orbit transfer. As the orbital coordinate system of the center satellite rotates, the original relative orbit cannot be maintained. A concept of formation reconfiguration maneuver is presented...
For the short-range rendezvous problem, an approach of time-optimal multi-impulse rendezvous was put forward using hybrid genetic algorithm. Firstly, based on the state transition matrix of T-H equation, the mathematical models of time-optimal multi-impulse rendezvous was established and transformed into a nonlinear optimization problem, In order to obtain the global solution efficiently, a hybrid...
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