Title :
Robust regulation of helicopter model based on the highest derivative in feedback
Author :
Roman Czyba;Michal Serafin
Author_Institution :
Department of Automatic Control, Silesian University of Technology, Gliwice, Poland
Abstract :
The problem of robust regulation of a helicopter laboratory model is considered. The applied model has two degrees of freedom and was constructed by HUMUSOFT. This paper presents the design of continuous- time controller based on higher order output derivatives in the feedback loop. The problem of forming desired output transients for nonlinear time-varying plants under conditions of the incomplete information is discussed. The control task is formulated as a tracking problem for output variables, where decoupled output transients are accomplished in spite of incomplete information about varying parameters of the system and external disturbances. Experiments results for tracking a reference signal are presented, and confirm the effectiveness of the proposed method and theoretical expectations.
Keywords :
"Robustness","Helicopters","Mathematical model","Feedback loop","Control systems","Aerodynamics","Control system synthesis","Laboratories","Vehicle dynamics","Sliding mode control"
Conference_Titel :
Advanced intelligent mechatronics, 2007 IEEE/ASME international conference on
Print_ISBN :
978-1-4244-1263-1
Electronic_ISBN :
2159-6255
DOI :
10.1109/AIM.2007.4412518