| 基于角速度观测器的卫星编队飞行相对姿态控制技术 |
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| 引用本文： | 高有涛,陆宇平,徐波. 基于角速度观测器的卫星编队飞行相对姿态控制技术[J]. 宇航学报, 2010, 31(7): 1782-1788. DOI: 10.3873/j.issn.1000-1328.2010.07.013 |
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| 作者姓名： | 高有涛 陆宇平 徐波 |
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| 作者单位： | (南京航空航天大学航天学院，南京 210016) |
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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
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| 关 键 词： | 卫星编队飞行 相对姿态 非线性观测器 积分反步法 |
| 收稿时间： | 2009-09-25 |
Relative Attitude Control Method for Satellite Formation Flight Based on Angular Velocity Observer |
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| GAO You-tao,LU Yu-ping,XU Bo. Relative Attitude Control Method for Satellite Formation Flight Based on Angular Velocity Observer[J]. Journal of Astronautics, 2010, 31(7): 1782-1788. DOI: 10.3873/j.issn.1000-1328.2010.07.013 |
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| Authors: | GAO You-tao LU Yu-ping XU Bo |
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| Affiliation: | GAO You-tao,LU Yu-ping,XU Bo(Dept. of Astronautics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China) |
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| Abstract: | 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. |
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| Keywords: | Satellite formation flight Relative attitude Nonlinear observer Integrator backstepping |
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