摘要
A controller is designed by establishing the nonlinear model and the ARMAX model of system for the self-tuning of landing gear. The self-tuning control is realized in combination with parameter identification. The simulation results show that the control scheme can improve the absorber capability of landing gear.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 237-241 |
| 页数 | 5 |
| 期刊 | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
| 卷 | 25 |
| 期 | 3 |
| 出版状态 | 已出版 - 5月 2004 |
学术指纹
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