DocumentCode :
2632967
Title :
Adaptive altitude control for a small helicopter in a vertical flying stand
Author :
Dzul, Alejandro ; Lozano, Rogelio ; Castillo, Pedro
Author_Institution :
Div. de Estudios de Posgrado e Investigacion, Inst. Tecnologico de la Laguna, Mexico
Volume :
3
fYear :
2003
fDate :
9-12 Dec. 2003
Firstpage :
2710
Abstract :
In this paper, we focus on the design and implementation of a controller for a two degree-of-freedom system. This system is composed of a small-scale helicopter which is mounted on a vertical platform. The model is based on Lagrangian formulation and the controller is obtained by classical pole-placement techniques for the yaw dynamics and adaptive pole-placement for the altitude dynamics. Experimental results show the performance of such a controller.
Keywords :
adaptive control; aircraft control; control system synthesis; helicopters; pole assignment; position control; adaptive altitude control; altitude dynamics; pole-placement techniques; small helicopter; vertical flying stand; yaw dynamics; Adaptive control; Aerodynamics; Aerospace control; Control systems; Equations; Helicopters; Instruments; Programmable control; System identification; Tail;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2003. Proceedings. 42nd IEEE Conference on
ISSN :
0191-2216
Print_ISBN :
0-7803-7924-1
Type :
conf
DOI :
10.1109/CDC.2003.1273033
Filename :
1273033
Link To Document :
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