Title :
A new hybrid tolerant controller design and its application to the flight control
Author :
Chen Jie ; Cunbao, M.A. ; Song Dong
Author_Institution :
Sch. of Aeronaut., Northwestern Polytech. Univ., Xi´an, China
Abstract :
A new hybrid tolerant controller design method for linear system with input disturbance and system uncertainty is presented. Based on the proper controller fault mode definition, the passive tolerant state feedback controller design method is derived for systems which contain non-parameter uncertainties. Theoretical analysis and simulation verify the conservation of the method above, and then a new hybrid tolerant control method is given for this problem, the proposed approach is evaluated by an aircraft example, and the conclusion is validated by the simulation.
Keywords :
aerospace control; control system synthesis; linear systems; state feedback; uncertain systems; fault mode definition controller; flight control application; input disturbance; linear system; new hybrid tolerant controller design; nonparameter uncertainties; passive tolerant state feedback controller design method; uncertainty system; Control systems; Educational institutions; Hafnium; Robustness; Stability criteria; Vectors; LMI; hybrid tolerant control; robust tolerant; state feedback;
Conference_Titel :
Information Security and Intelligence Control (ISIC), 2012 International Conference on
Conference_Location :
Yunlin
Print_ISBN :
978-1-4673-2587-5
DOI :
10.1109/ISIC.2012.6449714
