文章基本信息

标题：Design and Optimization of Two-Loop Pilot forTactical Missi
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作者：Xitong Sun ; Xingbai Luo ; Min Gao 等
期刊名称：Engineering Letters
印刷版ISSN：1816-093X
电子版ISSN：1816-0948
出版年度：2021
卷号：29
期号：1
页码：278-287
语种：English
出版社：Newswood Ltd
摘要：The specific scheme of two-loop attitude controlsystem was formulated based on the design principle of attitudecontrol system with the damping circuit as the inner loop andthe overload control loop as the outer one. As required by theformulated scheme, the damping loop is designed firstly, ofwhich the stability and the dynamic response quality areimproved by adjusting the damping coefficient and the additionof the correction network. After that, the design andoptimization of the overload control loop are implemented. Withthe same design method, gain coefficient and correction networkare introduced to reduce overshoot of overload response curve,shorten response time and improve efficiency. Besides, thevalidity of the overload control loop is tested with square waveas input to reflect the real overload command signal.
关键词：Damping Loop; Overload Control Loop; Attitude Contro