| STT反舰导弹末端机动的控制方案比较研究 |
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| 引用本文： | 李聪颖,于进勇,李亮,顾文锦.STT反舰导弹末端机动的控制方案比较研究[J].科技导报(北京),2008,26(22). |
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| 作者姓名： | 李聪颖 于进勇 李亮 顾文锦 |
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| 作者单位： | 海军航空工程学院战略导弹工程系，海军航空工程学院研究生管理大队，海军航空工程学院控制工程系 |
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| 基金项目： | 航空科学基金
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| 摘 要： | 进行末端机动,有利于增大反舰导弹的突防概率。本文按照轨迹形态,将反舰导弹的末端机动分为平面机动与非平面机动两类,讨论了几种可能的控制方案,分析了它们的优缺点。采用降维方法,简化了控制指令设计。给出并比较了在几种控制指令下的末端机动实现公式,进行了具体的控制指令设计,并给出了质心、姿态角复合指令控制的一体化公式。仿真结果表明了控制方案设计的有效性。本文所研究的控制方法,适用于海军超音速、亚音速反舰导弹的末端机动控制。
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| 关 键 词： | 导航 制导与控制 末端机动 过载控制 姿态控制 |
Comparison Study on Several Control Schemes for Terminal Maneuvering STT Anti-vessel Missiles |
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| LI Congying,YU Jinyong,LI Liang,GU Wenjin.Comparison Study on Several Control Schemes for Terminal Maneuvering STT Anti-vessel Missiles[J].Science & Technology Review,2008,26(22). |
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| Authors: | LI Congying YU Jinyong LI Liang GU Wenjin |
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| Abstract: | Terminal maneuvering is effective to increase the probability of anti-vessel missiles to break through antimissile defense.Terminal maneuvering of anti-vessel missiles was classified as planar maneuvering and non-planar maneuvering.Several probable control schemes were discussed.Dimensionality reduction was made based on some assumptions to simplify control instructiondesign.Realization formulas of terminal maneuvering and corresponding control instructions were given.Integrated formula of centroid and attitude Angle Hybrid Control was given.Simulation results showed the effective of these control schemes.The control schemes can also be used to other naval supersonic and subsonic anti-vessel missiles. |
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| Keywords: | navigation guidance and control terminal maneuvering overload control attitude control |
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