Active fault-tolerant control for near space vehicles based on reference model adaptive sliding mode scheme

Author:

Zhao Jing1,Jiang Bin1,Chowdhury Fahmida N.2,Shi Peng345

Affiliation:

1. College of Automation Engineering; Nanjing University of Aeronautics and Astronautics; Nanjing 210016 Jiangsu China

2. The National Science Foundation; 4201 Wilson Boulevard Arlington VA 22230 USA

3. Department of Computing and Mathematical Sciences; University of Glamorgan; Pontypridd CF37 1DL UK

4. School of Engineering and Science; Victoria University; Melbourne VIC 8001 Australia

5. School of Electrical and Electronic Engineering; University of Adelaide; Adelaide SA 5005 Australia

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Signal Processing,Control and Systems Engineering

Reference39 articles.

1. Xu GX Liu HT Nonlinear fault-tolerant flight control design applied to a loss-of-thrust aircraft AIAA Guidance, Navigation, and Control Conference 2011

2. Fault accommodation for near space hypersonic vehicle with actuator fault;Xu;International Journal of Innovative Computing, Information and Control,2011

3. Robust Model-Based Fault Diagnosis for Dynamic Systems

4. Diagnosis and Fault-Tolerant Control

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2. Robust fault-tolerant control design for hypersonic vehicle with input saturation and actuator faults;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-08-28

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4. Discrete finite-time robust fault-tolerant high-order sliding mode control of uncertain quadruped robot: an experimental assessment;International Journal of Intelligent Robotics and Applications;2021-02-01

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