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Preliminary design of sliding mode controller for angular positional tracking of an aircraft

Sliding mode controllers are known to be robust to parameter changes and capable of rejecting disturbances. Most sliding mode controllers were implemented on aircraft models that were derived based on the aircraft's body axes. The aircraft model in this paper are derived from an energy based...

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书目详细资料
Main Authors:	Jones, Lim Jen Nee, Tan, Chee Pin, Man, zhihong, Akmeliawati, Rini
格式:	Conference or Workshop Item
语言:	English
出版:	2009
主题:	TJ212 Control engineering
在线阅读:	http://irep.iium.edu.my/14158/1/ascc2009_jn.pdf http://irep.iium.edu.my/14158/
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