国防科技大学学报Issue(4)：15-21,7.DOI:10.11887/j.cn.201404004
考虑可观测度的反交会规避机动方法
An anti-rendezvous evasion maneuver method based on degree of observability
摘要
Abstract
An anti-rendezvous evasion maneuver method is proposed in order to escape from the spacecraft that has autonomous approaching ability.Supposing that a two impulse C-W navigation strategy is used by the approaching spacecraft,first a bearing-only relative navigation model is built.Then,a definition of degree of observability based on state estimation error is proposed so as to quantify observability.By using the degree of observability conception,the evasion maneuver direction is chosen as its gradient,which guarantees that every unit impulse can reduce the system observability mostly.Finally,the numerical simulation is conducted with different maneuver impulse,and the result shows that the method proposed can attenuate the system observability obviously.The method offers a new viewpoint for evasion maneuver research.关键词
可观测度/反交会/规避机动Key words
degree of observability/anti-rendezvous/evasion maneuver分类
航空航天引用本文复制引用
于大腾,王华,李九人..考虑可观测度的反交会规避机动方法[J].国防科技大学学报,2014,(4):15-21,7.基金项目
国家自然科学基金资助项目（11272346）；国家部委资助项目 （）
