| 非合作目标追踪与相对状态保持控制技术研究 |
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| 引用本文： | 苏晏,李克行,黎康.非合作目标追踪与相对状态保持控制技术研究[J].空间控制技术与应用,2010,36(6):51-55. |
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| 作者姓名： | 苏晏 李克行 黎康 |
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| 作者单位： | [1]北京控制工程研究所,北京100190 [2]空间智能控制技术重点实验室,北京100190 |
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| 摘 要： | 基于考虑J2摄动影响的改进Hill方程数学描述,将最优机动问题转化为标准线性规划问题,为在轨服务系统对非合作目标的接近过程进行路径规划,针对卫星跟踪以及悬停的特殊相对运动状态设计控制方法,实现近距离相对轨道的精确控制.最后通过数学仿真验证方案的正确性和有效性.
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| 关 键 词： | 非合作目标 追踪 悬停 轨道控制 |
Control Technology for Relative States Tracking and Holding to Uncooperative Spacecraft |
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| SU Yan,LI Kehang,LI Kang.Control Technology for Relative States Tracking and Holding to Uncooperative Spacecraft[J].Aerospace Contrd and Application,2010,36(6):51-55. |
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| Authors: | SU Yan LI Kehang LI Kang |
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| Institution: | 1.Beijing Institute of Control Engineering,Beijing 100190,China;2.Science and Technology on Space Intelligent Control Laboratory,Beijing 100190,China) |
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| Abstract: | Based on the improved Hill equation in consideration of the J2 disturbance,the optimal maneuvering problem is converted into a standard linear programming problem a path is programmed for on-orbit servicing system approaching to an uncooperative object.Based on the special relative motion of tracking and hovering,a control method is designed to achieve relative orbit control accurately.Finally,validity and effectiveness are verified by mathematic simulation. |
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| Keywords: | uncooperative object tracking hovering orbit control |
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