Fast Actuator Fault Detection, Identification, and Accommodation for a Quadrotor with Arbitrary Faults Through Direct Computation of Thrusts

Author:

Song Yongkyu,Lee Sumin,Cho Dong-Hoon,Chung Jae-Whan,Cho In-je

Publisher

Elsevier BV

Reference16 articles.

1. Nonlinear L1 adaptive control of an airplane with structural damage;K Ahmadi;Proc InstMech Eng Part G J Aerosp Eng,2017

2. Experimental test of a two-stage Kalman filter for actuator fault detection and diagnosis of an unmanned quadrotor helicopter;M H Amoozgar;Journal of Intelligent & Robotic Systems,2013

3. Nonlinear Robust adaptive control of an airplane with structural damage;D Asadi;Proc Inst Mech Eng Part G J Aerosp Eng,2020

4. Fault-tolerant trajectory tracking control of a quadcopter in presence of a motor fault;D Asadi;Int J Aeronaut Space Sci,2021

5. Actuator Fault Detection, Identification, and Control of a Multirotor Air Vehicle Using Residual Generation and Parameter Estimation Approaches;D Asadi;International Journal of Aeronautical and Space Sciences,2023

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