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Tail motion model identification for control design of an unmanned helicopter

Author
Morcego, B.; Saldívar, E.; Nejjari, F.
Type of activity
Presentation of work at congresses
Name of edition
Research, Development and Education on Unmanned Aerial Systems
Date of publication
2011
Presentation's date
2011-12-01
Book of congress proceedings
Research, Development and Education on Unmanned Aerial Systems
First page
1
Last page
11
Repository
http://hdl.handle.net/2117/14899 Open in new window
URL
http://www.red-uas.com/ Open in new window
Abstract
This paper explains the methodology developed to design the yaw control system (heading control system) of the α-SAC UAV. The problem of modeling and controlling the tail motion of this UAV along a desired trajectory is considered. First, the response data of the system are collected during special flight test and a linear time invariant model is extracted by identification techniques. Then, the control system is designed and implemented using a PID feedback/feedforward control method. The tech...
Citation
Morcego, B.; Saldívar, E.; Nejjari, F. Tail motion model identification for control design of an unmanned helicopter. A: Research, Development and Education on Unmanned Aerial Systems. "Research, Development and Education on Unmanned Aerial Systems". Sevilla: 2011, p. 1-11.
Group of research
CS2AC-UPC - Supervision, Safety and Automatic Control
SAC - Advanced Control Systems
SIC - Smart Control Systems

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