DocumentCode :
2828589
Title :
Identify flight control system based on least squares support vector machine
Author :
Zhong-jian Li ; Yin, De-Yi
Author_Institution :
Coll. of Autom., Northwestern Polytech. Univ., Xi´´an, China
Volume :
4
fYear :
2010
fDate :
22-24 Oct. 2010
Abstract :
As flight control system is highly non-linear, it´s difficult to get desired results using traditional identification ways. And based on statistical learning theory, support vector machine, is considered a kind of new and feasible nonlinear system identification approach. In this paper, applied least square support vector regression machines and Series - Parallel identification model of system identification to identify flight control system model Through the simulation, the model of flight control system is successfully identified The simulation results show that: the design of the identification model predicted a good performance, with very high accuracy, at the same time; it also can be very good to reflect the characteristics of flight control systems.
Keywords :
aerospace control; identification; least mean squares methods; nonlinear control systems; statistical analysis; support vector machines; flight control system; least square method; nonlinear system identification; series-parallel identification model; statistical learning theory; support vector machine; Elevators; Kernel; Statistical learning theory; Support vector machine; flight control system; identification;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Application and System Modeling (ICCASM), 2010 International Conference on
Conference_Location :
Taiyuan
Print_ISBN :
978-1-4244-7235-2
Electronic_ISBN :
978-1-4244-7237-6
Type :
conf
DOI :
10.1109/ICCASM.2010.5620099
Filename :
5620099
Link To Document :
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