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Fault Tolerant Control and Simulation of quadrotor Based on Adaptive Sliding Mode Control

Published: 14 October 2022 Publication History

Abstract

An adaptive integral sliding mode control strategy based on a nonlinear disturbance observer is proposed for fault-tolerant control of a quadrotor UAV under partial actuator failure and external disturbances. First, an adaptive integral sliding-mode controller (SMC) is designed to ensure the tracking performance of the quadrotor UAV in the presence of partial actuator failure. Then, a nonlinear disturbance observer is designed to estimate the external disturbance, and combined with the SMC to compensate for the external disturbance while reducing the discontinuous control gain. Finally, the effectiveness and superiority of the proposed control strategy are verified through comparative numerical simulations of the quadrotor UAV under different fault and external disturbance conditions.

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  1. Fault Tolerant Control and Simulation of quadrotor Based on Adaptive Sliding Mode Control

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    ICCIR '22: Proceedings of the 2022 2nd International Conference on Control and Intelligent Robotics
    June 2022
    905 pages
    ISBN:9781450397179
    DOI:10.1145/3548608
    Permission to make digital or hard copies of all or part of this work for personal or classroom use is granted without fee provided that copies are not made or distributed for profit or commercial advantage and that copies bear this notice and the full citation on the first page. Copyrights for components of this work owned by others than ACM must be honored. Abstracting with credit is permitted. To copy otherwise, or republish, to post on servers or to redistribute to lists, requires prior specific permission and/or a fee. Request permissions from [email protected]

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    Published: 14 October 2022

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