DocumentCode
2999563
Title
Research on servo tracking performance of flight simulator
Author
Tang, Zhiyong ; Ding, Yong ; Pei, Zhongcai
Author_Institution
Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. Of Aeronaut. & Astronaut., Beijing
fYear
2008
fDate
1-3 Sept. 2008
Firstpage
1834
Lastpage
1838
Abstract
Because the flight simulator works in different environment for simulating various flight attitudes, the different control algorithm is used for improving the dynamic and static performance. The neural network has good self-learning and self-adaptive, and PID has good robustness, so the adaptive controller based on neural network and PID is used to overcome the coupling inertia and imbalance torque when simulator worked in high speed or large range. And the friction compensation based model reference adaptive control is adopted in low speed status. It has good stability and precision because of using the Stribeck model and Lyapunov stability theory. In order to prove the effectiveness of this controller, experiments have been done.
Keywords
Lyapunov methods; aerospace control; model reference adaptive control systems; neurocontrollers; robust control; servomechanisms; three-term control; Lyapunov stability theory; PID; Stribeck model; flight simulator; friction compensation; model reference adaptive control; neural network; robustness; servo tracking; Adaptive control; Aerospace simulation; Attitude control; Friction; Neural networks; Programmable control; Robust control; Servomechanisms; Three-term control; Torque control; Flight Simulator; compound control; neural network;
fLanguage
English
Publisher
ieee
Conference_Titel
Automation and Logistics, 2008. ICAL 2008. IEEE International Conference on
Conference_Location
Qingdao
Print_ISBN
978-1-4244-2502-0
Electronic_ISBN
978-1-4244-2503-7
Type
conf
DOI
10.1109/ICAL.2008.4636456
Filename
4636456
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