Nonlinear Output Regulation with Input Delay and Application in AHV Attitude Control
Time delay phenomena exist almost everywhere in the actual world and are especially important in the control of an AHV. The small time delay usually ignored in control may cause quite obvious errors in the flight trajectory tracking, because of the extremely high flight speed. In this paper, a new f...
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| Main Authors: | Liang Cai, Qingxian Wu |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2017-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2017/6850909 |
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