Fault-tolerant flight control of quad-rotor UAV based on sliding mode theory-Reference-Cited by-同舟云学术

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Fault-tolerant flight control of quad-rotor UAV based on sliding mode theory

Published:2018-06 Issue: Volume: Page:
ISSN:
Container-title:2018 Chinese Control And Decision Conference (CCDC)
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Author:

Xing Xiaojun,Ma Zhen,Chen Xiaoran,Huang Longliang

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/8396318/8407034/08407148.pdf?arnumber=8407148

Cited by 4 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. Composite nonlinear dynamic inversion control for quadrotor UAV with multi-source disturbances and actuator faults;2022 41st Chinese Control Conference (CCC);2022-07-25

2. A modified indirect vector control strategy for 3-phase wye-connected induction motor drives under open-phase fault;Electrical Engineering;2022-05-17

3. A Survey on Fault Diagnosis and Fault-Tolerant Control Methods for Unmanned Aerial Vehicles;Machines;2021-09-13

4. LSTM-Based Output-Constrained Adaptive Fault-Tolerant Control for Fixed-Wing UAV with High Dynamic Disturbances and Actuator Faults;Mathematical Problems in Engineering;2021-03-09

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