DocumentCode :
2988297
Title :
The Development of a high performance UAV for flight control research
Author :
Grady, Nickolas ; Frye, Michael ; Qian, Chunjiang
Author_Institution :
University of Texas of San Antonio, Department of Electrical Engineering, Nonlinear Control Research Laboratory, USA
fYear :
2006
fDate :
7-9 April 2006
Firstpage :
57
Lastpage :
61
Abstract :
This paper summarizes the Phase I Airframe Development of an undergraduate research project for the Raptor 90 remote-controlled helicopter. The purpose of the project is to introduce the fundamentals of dynamics and control for rotorcraft to undergraduate engineers interested in control system theory. Follow on research for the Raptor 90 will include instrumentation and flight-testing for data collection. Controller development will be investigated using a dynamic model simulation of the Raptor 90 helicopter.
Keywords :
Aerodynamics; Aerospace control; Control systems; Engines; Fuels; Helicopters; Instruments; Nonlinear dynamical systems; Unmanned aerial vehicles; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Region 5 Conference, 2006 IEEE
Conference_Location :
San Antonio, TX, USA
Print_ISBN :
978-1-4244-0358-5
Electronic_ISBN :
978-1-4244-0359-2
Type :
conf
DOI :
10.1109/TPSD.2006.5507462
Filename :
5507462
Link To Document :
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