Optimization Of Cruise Tourist Orbit For Multiple Targets On GEO

摘要

It is supposed to maneuver orbit if the tourist orbit is used to make detailed investigation of multiple targets on GEO. The problem is how to minimize the energy dissipations of the orbit maneuver. In this paper, the optimization strategy is offered: 1. The difference of individual orbit inclination is supposed to be minimum by adjusting the configuration parameters such as radius of cruise, cruise speed and phase difference; 2. The pulse position is supposed to adjust based on the achieving the task that the targets on GEO are closely observed. Finally, the results show that the proposed optimization strategy can reduce the energy consumption greatly through the two target spacecraft and multiple target spacecraft simulation.