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
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