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多星编队飞行的分散式耦合控制技术研究 被引量：2

Decentralized Coupled Control for Multi-Satellite Formation Flight
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摘要 以多星编队飞行为研究对象,建立了多星编队飞行的分散式相对姿态动力学和运动学模型,结合卫星编队飞行相对位置的非线性动力学模型,利用Backstepping方法设计多星编队飞行的分散式耦合控制器。采用了一种选择性控制策略,能够保证多星编队飞行的控制效率和抗故障能力。数值仿真结果表明了所设计的分散式耦合控制器的有效性。 Decentralized relative attitude dynamics and kinematics models of multi-satellite formation flight are established. The Backstepping method is used to design the coupled controller based on the nonlinear relative position dynamics and the decentralized relative attitude dynamics of multi-satellite formation flight. A selective control strategy is suggested to guarantee the control efficiency and the mission-failure safety of multi-satellite formation flight. Numerical simulations have demonstrated the effectiveness of the decentralized coupled controller.
作者 高有涛 徐波 陆宇平
机构地区 南京航空航天大学航天学院 南京大学天文与空间科学学院
出处 《宇航学报》 EI CAS CSCD 北大核心 2012年第9期1248-1254,共7页 Journal of Astronautics
基金 国家自然科学基金(11078001) 国家高技术研究发展计划(2012AA121602) 中央高校基本科研业务费专项基金(NS2012132)
关键词 多星编队飞行 分散式耦合控制 BACKSTEPPING控制 选择控制策略 Multi-satellite formation flight Decentralized coupled control Backstepping control Selective control strategy
分类号 V448.2 [航空宇航科学与技术—飞行器设计]
作者简介 高有涛（1983-），男，博士，讲师，主要从事卫星编队飞行动力学建模与控制、人造卫星精密定轨等研究。通信地址：江苏省南京市白下区御道街29号航天学院（210016）电话：（025）84896521—6207E—mail：flgao@nuaa．edu．cn
  • 相关文献

参考文献16

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二级参考文献90

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共引文献33

同被引文献28

  • 1王功波,郗晓宁,刘磊.小卫星编队在轨释放方案优化设计[J].宇航学报,2008,29(2):440-443. 被引量：3
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引证文献2

二级引证文献11

宇航学报
2012年 第9期

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