| 卫星进入和离开编队机动轨迹规划及控制 |
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| 引用本文： | 孙东,周凤岐,周军.卫星进入和离开编队机动轨迹规划及控制[J].航天控制,2003,21(4):11-17. |
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| 作者姓名： | 孙东 周凤岐 周军 |
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| 作者单位： | 西北工业大学航天工程学院,西安,710072 |
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| 摘 要： | 本文研究卫星编队重新配置机动中在碰撞避免约束条件下故障星离开编队以及备份星进入编队的轨迹规划及控制策略,研究表明选择机动的启动时刻不但能够构成所需要的编队构型,而且可以节省燃料、实现碰撞避免,以太阳同步轨道卫星编队为对象进行的仿真显示控制策略是简单、有效的。
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| 关 键 词： | 编队飞行 机动 轨迹规划 |
| 修稿时间： | 2003年3月11日 |
Trajectory Planning and Control for Satellite Formation Flying Maneuver of Leaving and Joining |
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| Sun Dong,Zhou Fengqi,Zhou Jun College of Astronautics Northwestern Polytechnic University,Xi'an.Trajectory Planning and Control for Satellite Formation Flying Maneuver of Leaving and Joining[J].Aerospace Control,2003,21(4):11-17. |
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| Authors: | Sun Dong Zhou Fengqi Zhou Jun College of Astronautics Northwestern Polytechnic University Xi'an |
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| Institution: | Sun Dong,Zhou Fengqi,Zhou Jun College of Astronautics Northwestern Polytechnic University,Xi'an 710072 |
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| Abstract: | With the constraint of collision avoidance, trajectory planning and cotrol for
satellite formation flying is presented by which fault satellite leaves the formation and new
satellite join in the formation. For saving the fuel and avoiding collision, the start time of
maneuver must be selected carefully. Then sun synchronization orbit satellite formation is sim-
ulated. The result of simulation demonstrates validity of control scheme. |
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| Keywords: | Formation flying Maneuver Trajectory planning |
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