| 轨道维持与机动的最优控制 |
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| 引用本文： | 韩潮,付红勋.轨道维持与机动的最优控制[J].航天控制,2000(4). |
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| 作者姓名： | 韩潮 付红勋 |
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| 作者单位： | 北京航空航天大学!北京100083 |
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| 摘 要： | 从航天器的轨道运动学方程出发 ,运用线性离散系统最优控制理论 ,提出了一种用于航天器轨道维持与轨道机动的最优控制方法 ,建立了相关的最优控制模型并给出了求解该模型的算法。仿真计算结果表明 ,本文提出的最优控制方法是正确和可行的
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| 关 键 词： | 航天器 轨道保持 轨道机动 最佳控制 |
Optimal Control of Orbit Maintenance and Maneuver |
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| Han Chao\ Fu Hongxun Beijing University of Aeronautics and Astronautics,Beijing.Optimal Control of Orbit Maintenance and Maneuver[J].Aerospace Control,2000(4). |
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| Authors: | Han Chao\ Fu Hongxun Beijing University of Aeronautics and Astronautics Beijing |
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| Institution: | Han Chao\ Fu Hongxun Beijing University of Aeronautics and Astronautics,Beijing 100083 |
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| Abstract: | This paper provides a new optimal control method for orbital maintenance and maneuver,which begins with the kinetics equation of spacecraft and is based on the linear discrete optimal control theory,establishes the relative optimal control model and gives its solution.The simulation results show that the given optimal control method in this paper is correct and feasible. |
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| Keywords: | Spacecraft\ Orbital keeping\ Orbital maneuver\ Optimal control |
| 本文献已被 CNKI 等数据库收录！ |
