| 空空导弹的一种优化复合控制方案研究 |
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| 引用本文： | 梁晓庚,张焱,王锡泉.空空导弹的一种优化复合控制方案研究[J].航天控制,1995(1). |
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| 作者姓名： | 梁晓庚 张焱 王锡泉 |
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| 摘 要： | 通过研究空空导弹推力矢量和气动复合控制与一般气动控制方式，讨论了新一代近距格斗型空空导弹的一种控制模式，并参照某型导弹的数学模型及有关气动参数对两种控制方式进行了数字仿真。结果表明，在新一代格斗型空空导弹上采用复合控制方式可明显地改善导弹的总体性能。
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| 关 键 词： | 空对空导弹，复合控制系统，推力，控制 |
Research on optimal compound control for air-to-air missile |
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| Liang Xiaogeng,Zhang Yan,Wang Xiquan.Research on optimal compound control for air-to-air missile[J].Aerospace Control,1995(1). |
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| Authors: | Liang Xiaogeng Zhang Yan Wang Xiquan |
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| Institution: | Liang Xiaogeng;Zhang Yan;Wang Xiquan 471009 |
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| Abstract: | Through the study Of air-to-air missile's two control modes,i.e.,(1)the general aerodynamic control and(2)the aerodynamic and thrust vector control,this paper discurses a new dog-fight air-to-air missile's control method.Based on the mathematic model of a certain air-to-air missile and its aerodynamic paramters,some digital simulation results are given.The results show that the aerodynamic and thrust veclor control method will improve foe air-to-air missile's overall performance obviously. |
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| Keywords: | Air-to-air missile Compound control system Thrust Control |
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