DocumentCode
2728182
Title
Research of the aerodynamic parameter estimation for the small unmanned aerial vehicle
Author
Li Chao ; Dou Xiuxin ; Wu Liaoni
Author_Institution
Xiamen Univ., Xiamen, China
fYear
2013
fDate
12-14 June 2013
Firstpage
1917
Lastpage
1920
Abstract
Aircraft parameter estimation is an important problem in aircraft dynamics and control. As standard methods for aircraft parameter estimation, output-error method and equation-error method in the frequency domain are described and examined. The analysis was based on flight data. It was found that the output-error and equation-error method in frequency domain are in statistical agreement. By comparison, the equation-error method has excellent prediction capability similar to the output-error method.
Keywords
aerodynamics; aircraft control; autonomous aerial vehicles; parameter estimation; vehicle dynamics; aerodynamic parameter estimation; aircraft control; aircraft dynamics; aircraft parameter estimation; equation-error method; flight data; frequency domain; output-error method; prediction capability; small unmanned aerial vehicle; statistical agreement; Aircraft; Equations; Frequency-domain analysis; Mathematical model; Maximum likelihood estimation; Parameter estimation; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Automation (ICCA), 2013 10th IEEE International Conference on
Conference_Location
Hangzhou
ISSN
1948-3449
Print_ISBN
978-1-4673-4707-5
Type
conf
DOI
10.1109/ICCA.2013.6565091
Filename
6565091
Link To Document