摘要
The approximate reverse of a nonlinear system was extracted by its approximate linearized model and the fuzzy control was employed to restrain the effect the error produces on the system so as to guarantee the terminal performance of the system, thus constituting a plan of dynamic reverse and fuzzy integrated control. This method was applied to the attitude control of unmanned helicopters and it can remove uncertain effects unmanned helicopters bring about and provide better robustness.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 1133-1135 |
| 页数 | 3 |
| 期刊 | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
| 卷 | 29 |
| 期 | 12 |
| 出版状态 | 已出版 - 12月 2003 |