上海航天2000，Vol.17Issue(6)：16-20,5.
气动力星座保持的最优控制
OPTIMIZATION CONTROL OF FORMATION KEEPING OF SATELLITE CONSTELLATION USING AERODYNAMIC FORCE
摘要
Abstract
Optimization control of formation keeping of a satellite constellation using aerodynamic force is studied in this paper. At first the state/costate equations are derived. Then a new algorithm is developed on this optimum problem. The simulation results show that the algorithm is efficient.关键词
气动力/小卫星/星座保持/最优控制Key words
Aerodynamic force/Small satellite/Sate llite constellation formation keeping/Optimization control分类
航空航天引用本文复制引用
林西强,张育林..气动力星座保持的最优控制[J].上海航天,2000,17(6):16-20,5.基金项目
得到国家863-2项目基金的资助 （）
