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| Design of Midcourse Guidance Law of Air Defence Missile Intercepting High Speed Maneuvering Target with Big Diving Angle |
| SHU Chuanliang, ZHU Di, ZHONG Yongjian, MENG Wanli, HAO Lianying |
| Shanghai Electro-mechanical Engineering Institute, Shanghai 201109, China |
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| Guide |
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Abstract This paper makes analysis of the characteristics of high speed maneuvering target with large diving angle and the disadvantages of interception of this kind of targets by the missile using traditional proportional guidance. It suggests a real-time prediction measure for this kind of targets and introduces a guidance method of quasi-counter trajectory interception. Simulation tests have also been carried out to verify the effectiveness of this method.
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Received: 25 July 2018
Published: 14 January 2019
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2019, Vol. 2 
