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Alternative TitleCorrection of the Relative Orbit States Based on Inter-Satellite Ranging for Micro-Satellites Formation
张晓磊; 郑建华; 高东; 钱航
Source Publication空间控制技术与应用
Keyword小卫星编队 星间测距 相对状态确定 扩展卡尔曼滤波
Other AbstractDetermination of the relative states is the primary and important guarantee for normal operation of micro-satellite formation. With the miniaturization and low-cost spaceborne GPS receiver, the accuracy of orbit determination is low. In order to solve this problem, a method of correcting the formation relative orbit is given with only inter-satellite ranging information used. Inter-satellite ranging information is introduced and the extended Kalman filter is used to enhance the estimation accuracy of the relative orbit. The numerical simulation results show the validity of this approach.
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GB/T 7714
张晓磊,郑建华,高东,等. 星间测距对小卫星编队相对轨道状态的修正[J]. 空间控制技术与应用,2015,41(3):42-47.
APA 张晓磊,郑建华,高东,&钱航.(2015).星间测距对小卫星编队相对轨道状态的修正.空间控制技术与应用,41(3),42-47.
MLA 张晓磊,et al."星间测距对小卫星编队相对轨道状态的修正".空间控制技术与应用 41.3(2015):42-47.
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