| 飞船安全交会对接的最优控制律设计 |
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| 引用本文： | 荆武兴,杨涤,吴瑶华.飞船安全交会对接的最优控制律设计[J].航天控制,1993(3). |
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| 作者姓名： | 荆武兴 杨涤 吴瑶华 |
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| 作者单位： | 哈尔滨工业大学
(荆武兴，杨涤)，哈尔滨工业大学(吴瑶华) |
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| 摘 要： | 本文考虑飞船与空间站交会对接时,最后逼近阶段中的安全控制问题,控制执行机构为常值推力的反作用推力器。采用分散最优控制方案,给出了一种近似时间-燃料最优的反馈开关控制律,仿真结果验证了此控制律的可行性。
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| 关 键 词： | 会合 对接 最优控制 |
Optimal Control Law Design for Safe Rendezvous and Docking of Between Two Spacecrafts |
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| Jing Wuxing,Yan Di,Wu Yaohua Harbin Institute of Technology.Optimal Control Law Design for Safe Rendezvous and Docking of Between Two Spacecrafts[J].Aerospace Control,1993(3). |
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| Authors: | Jing Wuxing Yan Di Wu Yaohua Harbin Institute of Technology |
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| Institution: | Jing Wuxing;Yan Di;Wu Yaohua Harbin Institute of Technology |
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| Abstract: | Safe control problems during the final phase of rendezvous and docking between twospacecrafts are studied Controls are assumed to be constant. A near time--optimal feedbackcontrol law is presented by using decentralized optimal control scheme. Simulation results areshown to illustrate effectiveness of the control law. |
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| Keywords: | Rendezvous Docking Optimal control |
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