Research on Control Strategy of Two Dimensional Output Force Vibration Damping Electric Actuator
The main spiral blades of helicopter and other non fixed wing aircraft are in the asymmetric and unsteady aerodynamic environment for a long time, which will make the body produce large-scale multi-directional low-frequency vibration, which will become the main vibration source of the body. The line...
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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
IEEE
2021-01-01
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| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/9319654/ |
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