远程导引变轨故障后轨道重构设计与分析

The Orbital Reconfiguring Design and Analysis after Maneuver Failure for Rendezvous Phasing

研究了空间交会远程导引变轨故障后轨道重构问题,提出了轨道重构设计准则,对五冲量远程导引的每一次变轨故障分别给出了四类轨道重构方案。根据提出的设计准则对给出轨道重构方案的修正能力、测控条件、推进剂消耗、终端精度和安全性进行初步分析,确定了处理远程导引变轨故障的轨道预案。

The orbital reeonfiguring problem after maneuver failure for rendezvous phasing is studied. The orbital reconfiguring design rules are proposed and four types of orbital reconfiguring plan are provided respectively for every maneuver failure in five-impulse phasing mission. Based on the proposed design rules, the provided reeonfiguring plan＇s correcting ability, tracking and command condition, propellant consumed, terminal precision and security are analyzed. Finally, the orbital counter plan to deal with rendezvous phasing maneuver failure is obtained.