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fei xian xing dong tai ni fang fa zai fei xing kong zhi lv she ji zhong de ying yong
Pages: 1236-1239
Year: Issue:  5
Journal: Computer Measurement & Control

Keyword:  nonlinear dynamic inversetime-scale separationflight controltrajectory track;
Abstract: 随着现代空战环境对战斗机的性能要求日益提高,传统的飞行控制方法已经难以满足这些要求。进行了非线性动态逆飞行控制律的设计研究及其应用。按照时标分离原理将飞机状态变量进行分组,针对各子系统的响应特点,采用层叠结构的动态逆控制器,设计了飞机四组状态变量的控制律。通过水平和垂直导引的算例进行仿真验证,结果表明飞机能较好的跟踪预定航迹,跟踪误差较小。
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