Integral terminal sliding mode fault tolerant control of quadcopter UAV systems

Author:

Nguyen Ngoc P.,Pitakwachara Phongsaen

Abstract

AbstractThe article presents an active fault-tolerant control scheme with an integral terminal sliding mode controller for the UAV systems. This scheme effectively addresses saturation issues, disturbances, and sensor and actuator faults. Initially, the quadcopter UAV's model is represented in state space form. Subsequently, an augmented system incorporating auxiliary states from sensor faults is developed. An adaptive sliding mode observer is proposed for estimating the actuator and sensor faults. The integral terminal sliding mode fault-tolerant control, designed for altitude and attitude regulation, relies on fault estimation data. In contrast, a cascade proportional-integral-derivative (PID) controller is employed for position control. Simulation results demonstrate the superiority of the proposed method over existing control algorithms.

Publisher

Springer Science and Business Media LLC

Reference45 articles.

1. Pitakwatchara, P. & Tuntivivat, S. Extending quadrotor motion capability by centrally coaxial tilting rotors. IEEE Robot. Autom. Lett. 8(9), 5360–5367 (2023).

2. Barghandan, S., Badamchizadeh, M. A. & Jahed-Motlagh, M. R. Improved adaptive fuzzy sliding mode controller for robust fault tolerant of a Quadrotor. Int. J. Control Autom. Syst. 15, 427–441. https://doi.org/10.1007/s12555-015-0313-7 (2017).

3. Freddi, A., Lanzon, A. & Longhi, S. A. A feedback linearization approach to fault tolerance in quadrotor vehicles. In Proceedings of the 18th World Congress the International Federation of Automatic Control, Milano, Italy, 28 August–2 September (2011).

4. Ma, L., Xu, N., Zhao, X., Zong, G. & Huo, X. ‘Small-gain technique based adaptive neural output-feedback fault-tolerant control of switched nonlinear systems with unmodeled dynamics’. IEEE Trans. Syst. Man Cybern. Syst. 51(2), 7051–7062 (2020).

5. Wang, B. & Zhang, Y. An adaptive fault-tolerant sliding mode control allocation scheme for multirotor helicopter subject to simultaneous actuator faults. IEEE Trans. Ind. Electron. 65, 4227–4236 (2018).

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3