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