Design of Eccentric Mass-Type Vibration-Damping Electric Actuator Control System for Non-Fixed-Wing Aircraft
The main spiral blade of non-fixed wing aircraft will produce periodic vibration force when rotating, which will not only reduce the service life of airborne equipment, but also greatly affect the working state of pilots. Due to the narrow damping band of passive damping device, it is difficult to m...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
IEEE
2020-01-01
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| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/9284434/ |
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