Integral terminal sliding mode fault tolerant control of quadcopter UAV systems

Abstract The 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...

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Bibliographic Details
Published in:	Scientific Reports
Main Authors:	Ngoc P. Nguyen, Phongsaen Pitakwachara
Format:	Article
Language:	English
Published:	Nature Portfolio 2024-05-01
Subjects:	Sliding mode control Actuator fault estimation Sensor fault estimation Fault tolerant control Adaptive control Nonlinear system
Online Access:	https://doi.org/10.1038/s41598-024-61273-2

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