| BTT—90导弹的一种最优导引规律的设计与分析 |
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| 引用本文： | 杨涤,栾泽威.BTT—90导弹的一种最优导引规律的设计与分析[J].宇航学报,1989(1):10-18. |
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| 作者姓名： | 杨涤 栾泽威 |
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| 作者单位： | 哈尔滨工业大学
(杨涤，栾泽威，高晓明)，哈尔滨工业大学(吴瑶华) |
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| 摘 要： | 本文对BTT-90导弹的一种最优导引规律进行了设计和分析,并将其应用于BTT-90导弹的六自由度弹道仿真计算中,得到了令人满意的结果。仿真计算表明,这种导引规律具有较好的工程实用价值。导引规律由最优控制理论推得,它具有形式简单,物理意义明确的特点。理论质点弹道计算的结果,证明了将这种导引规律应用于BTT导弹的合理性和可实现性。
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| 关 键 词： | BTT导弹 最优导引规律 |
DESIGN AND ANALYSIS OF AN OPTIMAL GUIDANCE LAW FOR BTT-90 MISSILE |
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| Yang Di Luan ZeweiGao Xiaoming Wu Yaohua.DESIGN AND ANALYSIS OF AN OPTIMAL GUIDANCE LAW FOR BTT-90 MISSILE[J].Journal of Astronautics,1989(1):10-18. |
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| Authors: | Yang Di Luan ZeweiGao Xiaoming Wu Yaohua |
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| Institution: | Harbin Institute of Technology |
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| Abstract: | In this paper, a kind of guidance law for BTT-90 missile is designed and analysed. After that. it is applyed to 6-DOF trajectory s mulation of BTT-90 missilc. The satisfactory simulation result indicates that ihis guidance law has good enigneering value. This guidance law is derived by optimal control theory. It is simple in form and explicit in physical meaning. The simulation result of theoretical partic letrajectory proves that this guidance law is reasonable and realizable for BTT missiles. |
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| Keywords: | BTT missile Optimal guidance law |
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