采用多站接力跟踪策略的再入返回器定轨精度研究  被引量:4

Analysis of Reentry Capsule Orbit Determination Precision Using Multiple Station Relay Tracking Strategy

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作  者:段建锋[1,2] 谢剑锋[1,2] 张宇[1,2] 陈明[1,2] 段成林[1,2] 王震宇[1] 

机构地区:[1]北京航天飞行控制中心,北京100094 [2]航天飞行动力学技术重点实验室,北京100094

出  处:《航天器工程》2015年第5期38-43,共6页Spacecraft Engineering

基  金:国家自然科学基金(11173005,11073047,11203003)

摘  要:针对我国探月工程再入返回段分离前的精度要求,在无法实现对再入返回器的三向测量情况下,提出多站接力跟踪的测量策略,以解决测定轨精度不高的问题。结合再入返回分离前的测控弧段,制定两站及三站接力跟踪的策略。利用ESA"桑巴"(SAMBA)卫星进行多站接力跟踪试验数据分析,结果表明,三站接力跟踪策略的定轨预报精度优于两站接力跟踪策略,能够实现返回器安全可靠地再入返回,可为再入返回任务分离前跟踪策略的制定提供依据。In the case of inability to achieve three-way measurements of the reentry capsule,and for meeting the return accuracy requirements of the Chinese lunar reentry capsule before separation,this paper provides a measurement strategy of relay tracking for multiple stations to solve the problem of precision.The strategies of relay tracking for two stations and three stations is developed with the arc of the re-entry test task before the separation,and the SAMBA satellite is used as an example to analyze the multiple station relay tracking data.The analysis results show that the optimal strategy of the orbit prediction precision is the three station relay tracking which is able to achieve reliable and safe reentry.This conclusion can provide a recommendation for the tracking strategy on the upcoming reentry mission before separation.

关 键 词:再入返回器 多站接力跟踪 “桑巴”卫星 定轨试验 精度分析 

分 类 号:V448.2[航空宇航科学与技术—飞行器设计]

 

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