Title :
Adaptive fault compensation for aircraft flight systems with actuator faults
Author :
Yuying Guo ; Youmin Zhang ; Bin Jiang
Author_Institution :
Sch. of Inf. Eng., Southwest Univ. of Sci. & Technol., Mianyang, China
Abstract :
In this paper, an adaptive fault compensation scheme is investigated for aircraft flight systems in the presence of non-measurable rate on the actuator second-order dynamics. The proposed fault compensation scheme is a combination between multiple model and adaptive reconfiguration control. By means of the designed method, the system output can track that of reference model asymptotically, and desired performance of the developed scheme is demonstrated by simulation studies on the lateral dynamic model of a Boeing 747 airplane.
Keywords :
actuators; adaptive control; aircraft control; compensation; vehicle dynamics; Boeing 747 airplane; actuator fault; actuator second-order dynamics; adaptive fault compensation scheme; adaptive reconfiguration control; aircraft flight system; lateral dynamic model; Actuators; Adaptation models; Aircraft; Atmospheric modeling; Educational institutions; Vectors; Actuator Fault; Fault Compensation; Flight Control System; Multiple Model;
Conference_Titel :
Control and Decision Conference (CCDC), 2013 25th Chinese
Conference_Location :
Guiyang
Print_ISBN :
978-1-4673-5533-9
DOI :
10.1109/CCDC.2013.6561825
