DocumentCode :
2451888
Title :
Experimental evaluations of reference governor control schemes with applications to the constrained control of RC helicopters
Author :
Hirata, Kenji ; Minemura, Hiroshi
Author_Institution :
Dept. of Comput. Controlled Mech. Syst., Osaka Univ., Japan
Volume :
2
fYear :
2004
fDate :
2-4 Sept. 2004
Firstpage :
855
Abstract :
This paper investigates experimental evaluations of control schemes for systems with pointwise-in-time constraints on states and control inputs. Reference governor control strategies are applied to a RC (radio controlled) model helicopter control system. Practical effectiveness and also limitations in the presence of modeling uncertainties are evaluated through experiments of the yaw angle control in hovering motions of the helicopter.
Keywords :
aircraft control; helicopters; position control; constrained control; helicopter control system; pointwise-in-time constraint; radio controlled model; reference governor control; yaw angle control; Constraint theory; Control system synthesis; Control systems; Helicopters; Mathematical model; Radio control; State-space methods; Strain control; Tail; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications, 2004. Proceedings of the 2004 IEEE International Conference on
Print_ISBN :
0-7803-8633-7
Type :
conf
DOI :
10.1109/CCA.2004.1387475
Filename :
1387475
Link To Document :
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