Abstract
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).
Translated title of the contribution | Experimental research on drop loading alleviation using on⁃off control for magneto⁃rheological landing gear |
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Original language | Chinese (Traditional) |
Article number | 229425 |
Journal | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
Volume | 45 |
Issue number | 12 |
DOIs | |
State | Published - 25 Jun 2024 |