| 飞船的双冲量最优交会 |
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| 引用本文： | 潘科炎.飞船的双冲量最优交会[J].航天控制,1991(2). |
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| 作者姓名： | 潘科炎 |
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| 作者单位： | 北京控制工程研究所 |
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| 摘 要： | 本文利用作者在文献中所介绍的Clohessy—Wiltshire方法,在线性引力模型的假设下,求得了实现双冲量交会的最优解析解,即实现交会所需施加的两次冲量之和最小。数字仿真表明,本分析是正确的。
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| 关 键 词： | 航天器 ~+最优交会 |
OPTIMAL RENDEZVOUS BETWEEN TWO SPACECRAFTS USING TWO IMPULSES |
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| Pan Keyan Beijing Institute of Control Engineering.OPTIMAL RENDEZVOUS BETWEEN TWO SPACECRAFTS USING TWO IMPULSES[J].Aerospace Control,1991(2). |
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| Authors: | Pan Keyan Beijing Institute of Control Engineering |
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| Institution: | Pan Keyan Beijing Institute of Control Engineering |
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| Abstract: | The eptimal analytic solution that minimizes the sum of the applied impulses necessary to ren- dezvous is obtained for the Clohessy-Wiltshire equations presented by authors in the reference1] with a linear gravity model assumption.Numerical computations are conducted to verify the optimal solution algorithm. |
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| Keywords: | Spacecraft ~+Optimal rendezvous |
| 本文献已被 CNKI 等数据库收录！ |
