Design of Eccentric Mass-Type Vibration-Damping Electric Actuator Control System for Non-Fixed-Wing Aircraft-Reference-Cited by-同舟云学术

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Design of Eccentric Mass-Type Vibration-Damping Electric Actuator Control System for Non-Fixed-Wing Aircraft

Published:2020 Issue: Volume:8 Page:219415-219429
ISSN:2169-3536
Container-title:IEEE Access
language:
Short-container-title:IEEE Access

Author:

Hao Zhenyang^ORCID,Wang Tao^ORCID,Cao Xin^ORCID,Zhang Qiyao

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

General Engineering,General Materials Science,General Computer Science

Link

http://xplorestaging.ieee.org/ielx7/6287639/8948470/09284434.pdf?arnumber=9284434

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Adaptive Fuzzy Filter-based L ₁ Adaptive Controller Design for Electromechanical Actuator Containing Uncertainties and Disturbances;IETE Journal of Research;2024-08-29

2. Evaluating Mass‐Spring‐Damper Systems and Models for Reinforcing Engineering Designs;Industrial and Manufacturing Designs;2024-07-03

3. Robust self‐adaptive fuzzy controller for load‐frequency control of islanded airport microgrids considering electric aircraft energy storage and demand response;IET Renewable Power Generation;2024-01-10

4. Novel Powertrain Vibration Controller With Six Rules-Based Fuzzy Inference for Time-Fluctuated Control Period;IEEE Access;2024

5. Efficient Tuning Scheme of Mode-Switching-Based Powertrain Oscillation Controller Considering Nonlinear Backlash;IEEE Access;2023

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