| 交会对接最终逼近段制导控制律设计方法研究 |
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| 引用本文： | 张万里,马广程,温奇咏,王常虹.交会对接最终逼近段制导控制律设计方法研究[J].宇航学报,2007,28(4):860-864. |
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| 作者姓名： | 张万里 马广程 温奇咏 王常虹 |
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| 作者单位： | 哈尔滨工业大学空间控制与惯性技术研究中心,哈尔滨,150001 |
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| 摘 要： | 针对空间交会对接最终逼近阶段要求较高的控制精度以及连续控制力（转矩）难于实现等问题，文中在制导律设计方面使用了一种基于Hill方程的直线型制导及其常值推力等效实现的策略，在姿态控制方面使用补偿线性化以及PWPF调节器实现的控制方法，对于以上两种制导控制律，利用半物理仿真平台对算法的有效性和可行性给予了验证。
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| 关 键 词： | 交会对接 直线型制导 补偿线性化 PWPF调节器 半物理仿真 |
| 文章编号： | 1000-1328（2007）04-0860-05 |
| 修稿时间： | 2007-03-302007-05-11 |
Research on the Method of a Guidance Law and Control Strategy for the Final Phase of Rendezvous and Docking |
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| ZHANG Wan-li,MA Guang-cheng,WEN Qi-yong,WANG Chang-hong.Research on the Method of a Guidance Law and Control Strategy for the Final Phase of Rendezvous and Docking[J].Journal of Astronautics,2007,28(4):860-864. |
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| Authors: | ZHANG Wan-li MA Guang-cheng WEN Qi-yong WANG Chang-hong |
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| Institution: | Space Control and Inertial Technology Research Center, WEN Qi-yong, WANG Chang-hong Harbin Institute of Technology, Harbin 150001, China |
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| Abstract: | In order to achieve the high precision of control and the implementation of continuous control force(torque) in the final phase of Rendezvous and Docking,a beeline guidance law based on the Hill equation is proposed in this paper with its realization by constant thrust.For the attitude control strategy here use a compensate linearization and PWPF regulator implementation.Then a semi-Physical simulation test of the arithmetic is given to verify the validity and feasibility of them. |
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| Keywords: | Rendezvous and docking Beeline guidance Compensate linearization PWPF regulator Seml-physical simulation fiat |
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