摘要
The magneto-rheological buffer of the landing gear is a semi-active damper designed based on the magneto-rheological effect. It can adjust the damping level of the buffer by varying the current of the exciting coil,thereby alleviating the landing load of the landing gear. We design a magneto-rheological buffer with on-off control and test the circuit dynamic response of the magneto-rheological buffer. To solve the time delay problem of the circuit response,an on-off controller with local negative feedback is proposed and designed to adjust the excitation coil current of the magneto-rheological buffer to alleviate the drop load. The effectiveness of alleviating the landing load is validated through the drop test. The results show that using the on-off control strategy with local negative feedback,we can reduce the peak value of the drop load by 10. 3%,compared with the case in which the exciting coil is not energized (i. e. ,the oleo-pneumatics buffer).
投稿的翻译标题 | Experimental research on drop loading alleviation using on⁃off control for magneto⁃rheological landing gear |
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源语言 | 繁体中文 |
文章编号 | 229425 |
期刊 | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
卷 | 45 |
期 | 12 |
DOI | |
出版状态 | 已出版 - 25 6月 2024 |
关键词
- drop loading alleviation
- feedforward control
- landing gear
- magneto-rheological buffer
- on-off control