Combined adaptive and non-adaptive attitude control of a helicopter

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[1] Inoue, Akira
[2] Deng, Mingcong
[3] Nakao, Seiji
[4] Harima, Takanori
[5] Ueki, Nobuyuki
来源
Inoue, A. (inoue@suri.sys.okayama-u.ac.jp) | / Society of Instrument and Control Engineers, SICE卷 / Society of Instrument and Control Engineers (SICE)期
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Theoretical; (THR);
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摘要
In this paper, a combined adaptive and non-adaptive attitude controller is proposed and we applied it to attitude control of 2 degrees of freedom helicopter system. That is, a nonlinear MIMO control method based on adaptive sliding mode control and non-adaptive nonlinear controls is proposed control and experiment is done by using the helicopter experimental system. © 2005 SICE.
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