ROBUST DYNAMIC INVERSION DESIGN OF MANEUVERABLE FLIGHT COMMAND TRACKING SYSTEMS

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https://hkxb.buaa.edu.cn/CN/abstract/abstract11488.shtml

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http://hdl.handle.net/11603/35917

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UMBC Mathematics and Statistics Department

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Author/Creator ORCID

https://orcid.org/0000-0003-2172-4182

Date

1998-10-25

Type of Work

journal articles
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Citation of Original Publication

Jinglai, Shen, and Gao Jinyuan. “ROBUST DYNAMIC INVERSION DESIGN OF MANEUVERABLE FLIGHT COMMAND TRACKING SYSTEMS” 19, no. 5 (October 25, 1998): 592–96. https://hkxb.buaa.edu.cn/CN/abstract/abstract11488.shtml

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Abstract

The design of a maneuverable flight command tracking system using nonlinear dynamic inversion is briefly introduced at first. And then a robust controller to improve the robustness of dynamic inversion is designed using the method of μ analysis and synthesis. The detailed design process and results are presented. Simulations show that the robust dynamic inversion controller yields good results.