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视场约束的交会对接V-bar撤离控制研究
引用本文:王华,李海阳,唐国金.视场约束的交会对接V-bar撤离控制研究[J].宇航学报,2007,28(1):28-32.
作者姓名:王华  李海阳  唐国金
作者单位:国防科技大学航天与材料工程学院,长沙,410073
摘    要:利用解析和数值结合的方法研究了在视场约束条件下交会对接V-bar撤离的控制问题。描述了交会对接V-bar撤离的径向冲量机动方案,说明了径向机动撤离方案具有减少羽流污染和故障情况下能够避免飞行器碰撞的优点。基于CW方程推导出了机动点位于V-bar上的特殊情况下径向冲量和视场角的解析公式,同时也得到了求最大视场角时刻和冲量作用后V-bar方向撤离距离的计算公式。对于任意机动点的一般情况,得到了求解径向冲量和视场角关系的非线性方程,这一方程可利用数值方法求解。最后,通过数值仿真验证了该方法的正确性。

关 键 词:航天器  V-bar撤离  控制  交会对接
文章编号:1000-1328(2007)01-0028-05
修稿时间:2006-04-062006-06-28

The V-bar Departure Control in Rendezvous and Docking Under Field of View Constraint
WANG Hua,LI Hai-yang,TANG Guo-jin.The V-bar Departure Control in Rendezvous and Docking Under Field of View Constraint[J].Journal of Astronautics,2007,28(1):28-32.
Authors:WANG Hua  LI Hai-yang  TANG Guo-jin
Institution:College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073, China
Abstract:The control of V-bar departure in rendezvous and docking under field of view constraint is studied using both analytic and numerical methods. The basic maneuver strategy of V-bar departure using radial impulse is described, and the strategy fulfils the requirements of minimum plume impact on the target and trajectory safety. The analytic solution between field of view and radial impulse is developed based on CW equation for impulse point located on V-bar, and the other solution includes the formulas to calculate the time of maximum field of view and departure distance on the V-bar direction. For general case the nonlinear equation between field of view and radial impulse is developed, and can be solved using numerical method. At last, two examples are calculated, and the results show that the method developed in this paper is correct.
Keywords:Spacecraft  V-bar departure  Control  Rendezvous and docking
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