Composite nonlinear dynamic inversion control for quadrotor UAV with multi-source disturbances and actuator faults

Author:

Xiao Liang1,Zhao Zhenhua1,Cao Dong1,Zu Jiakui1

Affiliation:

1. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing,China,211106

Funder

Natural Science Foundation of China

Natural Science Foundation of Jiangsu

China Postdoctoral Science Foundation

Postdoctoral Science Foundation of Jiangsu

Fundamental Research Funds for the Central Universities

Publisher

IEEE

Reference16 articles.

1. Sliding mode control of Quad-rotor UAV based on extended state Observer;zhao;Command Control and simulation,2020

2. Robust dynamic inversion control for quad-rotors unmanned vehicle based on sliding mode disturbance observation and compensation;chen;Systems Engineering and Electronics,2018

3. Adaptive prescribed performance control of quadrotor with unknown actuator fault;zhao;Control and Decision,2021

4. Study on Active Fault Tolerant Flight Control Systems for Quadrotor UAV with Actuator Failures

5. Active fault-tolerant control for a quadrotor helicopter against actuator faults and model uncertainties

Cited by 1 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. Reinforcement Learning-based Fault-Tolerant Control for Unmanned Aerial Vehicles;2024 39th Youth Academic Annual Conference of Chinese Association of Automation (YAC);2024-06-07

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