Development of Fault Tolerant Flight Control System For Handling Actuator Stuck Faults-Reference-Cited by-同舟云学术

Development of Fault Tolerant Flight Control System For Handling Actuator Stuck Faults

Published:2023-07-27 Issue: Volume: Page:161-171
ISSN:0972-950X
Container-title:Journal of Aerospace Sciences and Technologies
language:
Short-container-title:joast

Author:

K. Nagarathna,Deodhare Girish S.

Abstract

This paper presents the PID based fault tolerant controller for controlling the aircraft in normal flight conditions and actuator stuck failure condition. It has been demonstrated that the PID controller is capable to control the aircraft under LSTAB and RSTAB stuck failure conditions. Also, the robustness of the controller is demonstrated by analyzing the performance of the model under variation of the operating point of the model in the neighborhood of the trim point.

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