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Alternative TitleAnalytical Formation Keeping Control Strategy for Micro-satellites
王有亮; 郑建华; 李明涛
Source Publication空间科学学报
Keyword编队飞行 构型维持 平均相对运动 匀变速运动模型 单边极限环
Other AbstractFormation keeping is the foundation of satellite formation flying. J2 term and atmospheric drag are the main perturbations for the low Earth orbit satellites, which can cause the long-term change of relative velocity and formation drift. Firstly, the mean relative velocity is used to denote the drift rate of satellite formation, and the analytical representation between the mean relative velocity and impulse maneuver is derived. Then the mean relative acceleration is developed, and the relative motion under the main perturbations is equivalent to a uniformly accelerated motion. Finally, it is combined with the single side limit cycle control method, and an analytical formation keeping control strategy based on the inter-satellite ranging information is designed. The numerical simulation results indicate that the strategy is simple and effective, which is easy to implement in engineering and suitable to the autonomous control for micro-satellites especially.
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Document Type期刊论文
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GB/T 7714
王有亮,郑建华,李明涛. 微小卫星编队飞行解析构型维持控制方法[J]. 空间科学学报,2018,38(6):925-933.
APA 王有亮,郑建华,&李明涛.(2018).微小卫星编队飞行解析构型维持控制方法.空间科学学报,38(6),925-933.
MLA 王有亮,et al."微小卫星编队飞行解析构型维持控制方法".空间科学学报 38.6(2018):925-933.
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