| 具有终端角度约束的机动再入飞行器的最优制导律 |
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| 引用本文： | 陈海东,余梦伦,董利强.具有终端角度约束的机动再入飞行器的最优制导律[J].航天控制,2002,20(1):6-11. |
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| 作者姓名： | 陈海东 余梦伦 董利强 |
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| 作者单位： | 北京宇航系统工程设计部,北京,100076 |
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| 摘 要： | 对具有终端角度约束的机动再入飞行器的最优制导律进行了研究,提出了一种角度反馈形式的最优制导律,并与已有的角速度反馈形式的最优制导律进行了比较研究,所得到的结论对机动再入飞行器制导律的选择具有参考价值。
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| 关 键 词： | 最优导引规律 机动再入飞行器 研究 |
| 修稿时间： | 2001年6月1日 |
An Optimal Guidance Law of Maneuvering Reentry Vehicles with Terminal Angular Constraint |
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| Chen Haidong Yu Menglun Dong Liqiang Beijing Institute of Astronautical Systems Engineering,CALT,Beijing.An Optimal Guidance Law of Maneuvering Reentry Vehicles with Terminal Angular Constraint[J].Aerospace Control,2002,20(1):6-11. |
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| Authors: | Chen Haidong Yu Menglun Dong Liqiang Beijing Institute of Astronautical Systems Engineering CALT Beijing |
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| Institution: | Chen Haidong Yu Menglun Dong Liqiang Beijing Institute of Astronautical Systems Engineering,CALT,Beijing 100076 |
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| Abstract: | The optimal guidance law of maneuverable reentry vehicles with terminal angular constraint is studied and an optimal guidance law in angular feedback form is derived in this paper. The comparison with an existed optimal guidance law in angular velocity feedback form is also made. The conclusion from this paper is valuable for the selection of guidance law of maneuverable reentry vehicles. |
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| Keywords: | Optimal guidance law Maneucerable reentry vehicle Research |
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