咨询与建议

看过本文的还看了

相关文献

该作者的其他文献

文献详情 >Impact angle constrained fuzzy... 收藏

Impact angle constrained fuzzy adaptive fault tolerant IGC method for Ski-to-Turn missiles with unsteady aerodynamics and multiple disturbances

Impact angle constrained fuzzy adaptive fault tolerant IGC method for Ski-to-Turn missiles with unsteady aerodynamics and multiple disturbances

作     者:GUO Hang WANG Zheng FU Bin CHEN Kang FU Wenxing YAN Jie GUO Hang;WANG Zheng;FU Bin;CHEN Kang;FU Wenxing;YAN Jie

作者机构:Research Center for Unmanned System Strategy DevelopmentNorthwestern Polytechnical UniversityXi’an 710072China Unmanned System Research InstituteNorthwestern Polytechnical UniversityXi’an 710072China 

出 版 物:《Journal of Systems Engineering and Electronics》 (系统工程与电子技术(英文版))

年 卷 期:2022年第33卷第5期

页      面:1210-1226页

核心收录:

学科分类:1101[军事学-军事思想及军事历史] 08[工学] 080103[工学-流体力学] 0804[工学-仪器科学与技术] 0811[工学-控制科学与工程] 0701[理学-数学] 0801[工学-力学(可授工学、理学学位)] 0812[工学-计算机科学与技术(可授工学、理学学位)] 

基  金:supported by the National Natural Science Foundation of China(62003264). 

主  题:integrated guidance and control(IGC) impact angle constraint unsteady aerodynamics fault tolerant control(FTC) actuator failures 

摘      要:An impact angle constrained fuzzy adaptive fault tolerant integrated guidance and control method for Ski-to-Turn(STT)missiles subject to unsteady aerodynamics and multiple disturbances is proposed.Unsteady aerodynamics appears when flight vehicles are in a transonic state or confronted with unstable airflow.Meanwhile,actuator failures and multisource model uncertainties are introduced.However,the boundaries of these multisource uncertainties are assumed unknown.The target is assumed to execute high maneuver movement which is unknown to the missile.Furthermore,impact angle constraint puts forward higher requirements for the interception accuracy of the integrated guidance and control(IGC)method.The impact angle constraint and the precise interception are established as the object of the IGC method.Then,the boundaries of the lumped disturbances are estimated,and several fuzzy logic systems are introduced to compensate the unknown nonlinearities and uncertainties.Next,a series of adaptive laws are developed so that the undesirable effects arising from unsteady aerodynamics,actuator failures and unknown uncertainties could be suppressed.Consequently,an impact angle constrained fuzzy adaptive fault tolerant IGC method with three loops is constructed and a perfect hit-to-kill interception with specified impact angle can be implemented.Eventually,the numerical simulations are conducted to verify the effectiveness and superiority of the proposed method.

读者评论 与其他读者分享你的观点

用户名:未登录
我的评分