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康珅, 单家元. 航天器分布式有限时间编队方法[J]. 深空探测学报(中英文), 2017, 4(4): 390-394. DOI: 10.15982/j.issn.2095-777.2017.04.0013
引用本文: 康珅, 单家元. 航天器分布式有限时间编队方法[J]. 深空探测学报(中英文), 2017, 4(4): 390-394. DOI: 10.15982/j.issn.2095-777.2017.04.0013
KANG Shen, SHAN Jiayuan. Distributed Finite-Time Control Method for Formation Flying[J]. Journal of Deep Space Exploration, 2017, 4(4): 390-394. DOI: 10.15982/j.issn.2095-777.2017.04.0013
Citation: KANG Shen, SHAN Jiayuan. Distributed Finite-Time Control Method for Formation Flying[J]. Journal of Deep Space Exploration, 2017, 4(4): 390-394. DOI: 10.15982/j.issn.2095-777.2017.04.0013

航天器分布式有限时间编队方法

Distributed Finite-Time Control Method for Formation Flying

  • 摘要: 以二阶积分环节作为单体航天器动力学模型,在固定通信拓扑的基础上,假设每个航天器仅获取相邻航天器的速度位置信息,设计了分布式有限时间跟踪控制算法,并证明了算法的有效性。在该算法的基础上,采用了虚拟结构和阶级控制方法,使第一阶级航天器接受虚拟领队形成的虚拟结构信息,次级航天器接受上一级航天器信息,给出了有限时间编队方法,并通过数值仿真验证了该编队算法。

     

    Abstract: In this paper,a dynamic model of single spacecraft is simulated by a double integrator and the communication topology is assumed fixed. Based on the information exchanges among neighbors,the distributed finite-time control protocol is designed and mathematically verified. Adopt the presented control protocol and combined with virtual structure and hierarchical protocol,the formation algorithm is designed,where in a group spacecraft on a lower level takes orders from spacecraft on a higher level. The numerical simulation is conducted,verifying the effectiveness of the proposed method.

     

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