Optimizing evasive maneuvering of planes using a flight quality driven model

作     者：Chang LIU Shaoshan SUN Chenggang TAO Yingxin SHOU Bin XU 

作者机构：School of AutomationNorthwestern Polytechnical University Chengdu Aircraft Design & Research Institute of AVIC 

出 版 物：《Science China(Information Sciences)》 (中国科学:信息科学(英文版))

年 卷 期：2024年第67卷第3期

页      面：197-208页

核心收录：

学科分类：12[管理学] 1201[管理学-管理科学与工程(可授管理学、工学学位)] 1101[军事学-军事思想及军事历史] 081104[工学-模式识别与智能系统] 08[工学] 082601[工学-武器系统与运用工程] 0826[工学-兵器科学与技术] 0714[理学-统计学（可授理学、经济学学位）] 0835[工学-软件工程] 0701[理学-数学] 0811[工学-控制科学与工程] 0812[工学-计算机科学与技术（可授工学、理学学位）] 

基　　金：supported by National Natural Science Foundation of China (Grant No. 61933010) Natural Science Basic Research Plan in Shaanxi Province (Grant No. 2023JC-XJ-08) 

主　　题：optimal maneuver flying quality evasive strategy pursuit-evasion game air-to-air combat 

摘      要：This paper investigates the optimal evasive maneuver for a plane to avoid an incoming missile. To accurately model the system dynamics while improving computational efficiency, a simplified plane model based on flight quality is established. A missile model with proportional guidance is also *** problem of determining the optimal evasion plane maneuver is formulated. The Gauss pseudospectral method(GPM) is proposed as a solution to find the optimal maneuver. The optimized maneuver is validated by testing it on a high-fidelity 6-degree-of-freedom(6-DOF) model, which demonstrates the effectiveness of the proposed simplified plane model. The Monte Carlo method is employed to evaluate the capability of the plane to evade missiles in various scenarios and elucidate general principles for successful evasion.