A sliding mode controller for aircraft simulated entry into spin
In this paper, two controllers are presented for commanded departure of an aircraft into spin. The first controller is designed based on the information obtained from the bifurcation analysis results of the aircraft model and trial and error simulation experiments. The second controller is a nonline...
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| Main Authors: | , |
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| 其他作者: | |
| 格式: | Article |
| 語言: | English |
| 出版: |
2013
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| 在線閱讀: | https://hdl.handle.net/10356/107141 http://hdl.handle.net/10220/17829 http://dx.doi.org/10.1016/j.ast.2012.10.011 |
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| 機構: | Nanyang Technological University |
| 語言: | English |