DocumentCode :
2672711
Title :
Neutral speed stability control law of aircraft design based on fractional Order PIλDμ
Author :
Na, Gao ; Zhi-hong, Qu ; Hai-tao, Wang
Author_Institution :
Xi´´an Railway Vocational & Tech. Inst., Xi´´an, China
fYear :
2012
fDate :
23-25 May 2012
Firstpage :
2802
Lastpage :
2805
Abstract :
Considering flaws of neutral speed stability control law owing to using the PID controller in modern aircraft, the control law is redesigned using fractional order PIλDμ controller. Firstly, fractional order calculus definition is introduced. Secondly, merits of PIλDμ controller are analyzed via comparing with PID controller; based on Oustaloup approximation algorithm analysis and modification, fractional order Laplace operator module is developed and the fractional order PIλ controller is designed. Finally, PIλ controller is applied to design the neutral speed stability control law. Simulation results show that the fractional order PIλ controller can improve aircraft´s neutral speed stability performances.
Keywords :
Laplace transforms; aircraft control; control system synthesis; stability; three-term control; velocity control; Oustaloup approximation algorithm analysis; PID controller; aircraft design; aircraft neutral speed stability performances; fractional order Laplace operator module; fractional order PIλDμ controller design; fractional order calculus definition; neutral speed stability control law; Aerospace control; Aircraft; Calculus; Fractional calculus; Frequency domain analysis; Stability criteria; Fractional order calculus; Neutral speed stability of aircraft; Oustaloup algorithm; PIλDμ controller;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference (CCDC), 2012 24th Chinese
Conference_Location :
Taiyuan
Print_ISBN :
978-1-4577-2073-4
Type :
conf
DOI :
10.1109/CCDC.2012.6244447
Filename :
6244447
Link To Document :
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