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基于角速度观测器的卫星编队飞行相对姿态控制技术 被引量：3

Relative Attitude Control Method for Satellite Formation Flight Based on Angular Velocity Observer
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摘要 建立了卫星编队飞行的相对姿态动力学和运动学模型。利用积分反步法,设计了能够保证控制系统稳定性的控制器和角速度观测器,使得卫星编队飞行控制系统在不安装星载角速度测量设备的情况下仍能保持对理想相对姿态的跟踪,利用Lyapunov稳定性理论证明了系统的指数稳定性。 The dynamics and kinematics of the relative attitude of satellite formation flight are derived. According to the integrator backstepping method,a controller and an angular velocity observer are designed. Based on the observer,the control system can keep tracking the desired relative attitude without the angular velocity measurements. The exponent stability of the closed-loop system is proved by using the Lyapunov stability theory.
作者 高有涛 陆宇平 徐波
机构地区 南京航空航天大学航天学院
出处 《宇航学报》 EI CAS CSCD 北大核心 2010年第7期1782-1788,共7页 Journal of Astronautics
基金 国家863基金资助项目(2008AA12Z301)
关键词 卫星编队飞行 相对姿态 非线性观测器 积分反步法 Satellite formation flight Relative attitude Nonlinear observer Integrator backstepping
分类号 V412.4 [航空宇航科学与技术—航空宇航推进理论与工程]
  • 相关文献

参考文献10

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二级参考文献13

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共引文献2

同被引文献44

  • 1武延鹏,尤政,任大海.卫星姿态角速度的高增益观测器[J].清华大学学报（自然科学版）,2004,44(8):1017-1020. 被引量：2
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引证文献3

二级引证文献10

宇航学报
2010年 第7期

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