Adaptive Observer-based Fault-Tolerant Control for Actuator Faults in Quadrotor UAV
Author:
Affiliation:
1. Cadi Ayyad University,Faculty of Science and Technology,LSEEET Laboratory, Department of Applied Physics,Marrakesh,Morocco
2. Ecole Royale De L’Air,Marrakesh,Morocco
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10520739/10520740/10520809.pdf?arnumber=10520809
Reference12 articles.
1. MODELLING AND STABILIZING CONTROL LAWS DESIGN BASED ON BACKSTEPPING FOR AN UAV TYPE-QUADROTOR
2. Dynamic Modelling and Experimental Identification of Four Rotors Helicopter Parameters
3. Actuator Fault Tolerant Control of Variable Pitch Quadrotor Vehicles
4. Sliding Mode Fault Tolerant Control for a Quadrotor with Varying Load and Actuator Fault
5. An integral TSMC-based adaptive fault-tolerant control for quadrotor with external disturbances and parametric uncertainties
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