標題: Robust vertical takeoff and landing aircraft control via integral sliding mode
作者: Huang, YJ
Kuo, TC
Way, HK
電信工程研究所
Institute of Communications Engineering
公開日期: 1-七月-2003
摘要: Reduced equivalent systems have inherent closed-loop poles at the origin in the sliding mode for conventional sliding mode control (SMC). A systematic design strategy is developed for arbitrarily placing all SMC closed-loop poles. The speed control of a vertical takeoff and landing aircraft whose aerodynamic parameters vary considerably during flight is investigated. An outstanding output tracking performance and robustness against system parameter uncertainties and external disturbances are achieved.
URI: http://dx.doi.org/10.1049/ip-cta:20030593
http://hdl.handle.net/11536/27755
ISSN: 1350-2379
DOI: 10.1049/ip-cta:20030593
期刊: IEE PROCEEDINGS-CONTROL THEORY AND APPLICATIONS
Volume: 150
Issue: 4
起始頁: 383
結束頁: 388
顯示於類別:期刊論文


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