| 椭圆轨道编队常值推力构形变化控制方法 |
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| 引用本文： | 于萍,张洪华.椭圆轨道编队常值推力构形变化控制方法[J].宇航学报,2006,27(1):1-5,20. |
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| 作者姓名： | 于萍 张洪华 |
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| 作者单位： | 北京控制工程研究所,北京,100080 |
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| 摘 要： | 采用T-H方程作为椭圆轨道编队的动力学描述，推导了常值推力作用下的椭圆轨道编队的构形变化控制方法。通过合理的选择控制量的作用时刻，可达到大量节约燃料的目的。结合该构形控制方法给出了燃料均衡与燃料最优的解决方案；最后，给出的仿真算例说明了本文设计方法的有效性。
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| 关 键 词： | 椭圆轨道 编队控制 燃料最优 燃料均衡 |
| 文章编号： | 1000-1328（2006）01-0001-05 |
| 收稿时间： | 2005-03-04 |
| 修稿时间： | 2005-03-042005-08-26 |
Constant Thrust Control for Spacecraft Formation in Eccentric Orbits |
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| YU Ping,ZHANG Hong-hua.Constant Thrust Control for Spacecraft Formation in Eccentric Orbits[J].Journal of Astronautics,2006,27(1):1-5,20. |
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| Authors: | YU Ping ZHANG Hong-hua |
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| Institution: | Beijing Institute of Control Engineering, Beijing 100080, China |
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| Abstract: | Based on the Tschauner-Hempel equation the constant thrust control algorithm for spacecraft formation in eccentric orbits was put forward. The control time is optimized in order to economize fuel, The problems of total fuel minimization and fuel equalization were considered. Simulation results were also given to verify the effectiveness of the algorithms proposed above. |
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| Keywords: | Eccentric orbit Formation control Fuel minimization Fuel equalization |
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