摘要
微小卫星编队飞行中的队形设计好坏,直接影响到编队卫星用于队形保持消耗的能量;介绍了2种常见的队形设计方法:Hill设计方法和一般设计方法,分析了利用这2种方法设计的构形的稳定性;提出了一种长半轴加修正的队形设计新方法.仿真表明:利用长半轴加修正的队形设计新方法来设计编队构形,能够在地球J2项摄动影响下自然地保持初始编队构形,是一种较好的编队构形设计方法,具有很好的参考应用价值.
In this paper, configuration design problem of micro satellite formation flying is discussed. The quality of configuration design directly affects the energy for the formation keeping. At first, two basic methods of configuration design are introduced: Hill method and generalized method, and stability of configuration design is analyzed. Then, based on the generalized method, a modified method using adjusted semi major axis is presented. It is suggested that configuration design using this new method can be maintained naturally under J 2 perturbation, and this method is a good formation configuration design method.
出处
《装备指挥技术学院学报》
2002年第6期38-42,共5页
Journal of the Academy of Equipment Command & Technology
基金
国家高技术 863 2资助项目 (863 2 5 1 1.2 )
