Bounded Linear-Quadratic Differential Game Guidance Law for Dual-Thruster Controlled Missiles
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概要
著者
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Qi Naiming
Department Of Aerospace Engineering Harbin Institute Of Technology
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Lu Rui
Department Of Aerospace Engineering Harbin Institute Of Technology
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Liu Yanfang
Department Of Aerospace Engineering Harbin Institute Of Technology
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ZHOU Qihang
Department of Aerospace Engineering, Harbin Institute of Technology
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Zhou Qihang
Department Of Aerospace Engineering Harbin Institute Of Technology
関連論文
- Dynamic Influence of Propellant Sloshing Estimation Using Hybrid: Mechanical Analogy and CFD
- Bounded Differential Game Guidance Law for Interceptor Missiles with Aero Fins and Reaction Jets
- Bounded Linear-Quadratic Differential Game Guidance Law for Dual-Thruster Controlled Missiles
- Differential Game Guidance Law for Interceptor Missiles with a Time-varying Lateral Acceleration Limit