Adaptive finite time fault tolerant control for the quadrotor unmanned aerial vehicles based on time‐triggered strategy
Author:
Affiliation:
1. School of Electronic and Information Engineering University of Science and Technology Liaoning Anshan Liaoning China
2. Department R&D department FulScience Automotive Electronics Co., Ltd. Changchun Jilin China
Funder
Liaoning Provincial Education Department
Publisher
Wiley
Subject
Applied Mathematics,Control and Optimization,Software,Control and Systems Engineering
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/oca.2930
Reference29 articles.
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2. HamayunMT EdwardsC AlwiH.Integral sliding mode fault tolerant control incorporating on‐line control allocation. Proceedings of the 2010 11th International Workshop on Variable Structure Systems (VSS) 2010 100–105.10.1109/VSS.2010.5544704.
3. ParisiniT PolycarpouM SanguinetiM VemuriA.Robust parametric and non‐parametric fault diagnosis in nonlinear input‐output systems. Proceedings of the 36th IEEE Conference on Decision and Control 1997 Vol.5 4481–4482.10.1109/CDC.1997.649672.
4. Nonlinear Adaptive Fault-Tolerant Quadrotor Altitude and Attitude Tracking With Multiple Actuator Faults
5. A fault tolerant tracking control for a quadrotor UAV subject to simultaneous actuator faults and exogenous disturbances
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