Adaptive Backstepping Sliding Mode Based Fault-Tolerant Cooperative Control for Multiple UAVs under Thrust Loss Faults and Input Saturation
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics,College of Automation Engineering,Nanjing,China,211106
2. Concordia University,Industrial and Aerospace Engineering,Department of Mechanical,Montreal,Canada,QC H3G 1M8
Funder
National Natural Science Foundation of China
Natural Science Foundation of Jiangsu Province
China Postdoctoral Science Foundation
Fundamental Research Funds for the Central Universities
Natural Sciences and Engineering Research Council of Canada
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10185661/10185641/10185848.pdf?arnumber=10185848
Reference19 articles.
1. Formation Control of Multi-robots Using Backstepping Sliding Mode Control
2. Design of a Fixed-Wing UAV Controller Based on Adaptive Backstepping Sliding Mode Control Method
3. Adaptive fault-tolerant tracking control of flying-wing unmanned aerial vehicle with system input saturation and state constraints
4. Distributed Fractional-Order Finite-Time Control for Multiple Unmanned Aerial Vehicles
5. Backstepping Sliding Mode Control for Quadrotor Unmanned Aerial Vehicle with Unknown Disturbance and Input Constraint
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