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Maximal admissible mode decision delay in terminal guidance 被引量:1
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作者 Shengwen XIANG Tiancheng LI +2 位作者 Wei CHEN Hongqi FAN Qiang FU 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2019年第8期1959-1966,共8页
Mode decision-maker is a critical component in the logic-based Integrated Estimation and Guidance(IEG) system. For the best possible estimation and guidance performance, the mode decision delay of the mode decision-ma... Mode decision-maker is a critical component in the logic-based Integrated Estimation and Guidance(IEG) system. For the best possible estimation and guidance performance, the mode decision delay of the mode decision-maker should be limited to a range as small as possible. This paper presents a numerical method for computing the maximal admissible mode decision delay that varies with time-to-go. Particular attention has been paid to highly maneuvering target interception in terminal guidance. The results of this research offer useful guidelines for the design of the mode decision-maker in IEG systems. 展开更多
关键词 Highly maneuvering target INTERCEPTION Integrated Estimation and Guidance maximal admissible mode decision delay mode decision-MAKER Numerical methods
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