DocumentCode
581835
Title
Modeling of VSTOL aircraft lift lose in hover based on system identification method
Author
Zhan, Tu ; Jihong, Zhu
Author_Institution
Dept. of Comput. Sci. & Technol., Tsinghua Univ., Beijing, China
fYear
2012
fDate
25-27 July 2012
Firstpage
1843
Lastpage
1847
Abstract
In this paper we provide a system identification method to model VSTOL aircraft lift lose in hover. Compared with the conventional empirical formula calculation method, this approach avoids the problem of determining mechanism parameters and without considering the change of nozzle pressure ratio. The whole identification system consists of six-component balance, strain gauge force sensors, flight control system and upper computer. Collecting the system input and output signals, the model of VSTOL aircraft lift lose in hover can be identified.
Keywords
aircraft control; force sensors; identification; strain gauges; VSTOL aircraft lift lose modelling; empirical formula calculation method; flight control system; hover; six-component balance; strain gauge force sensors; system identification method; upper computer; Aircraft; Atmospheric modeling; Computational modeling; Computer science; Educational institutions; Electronic mail; System identification; Lift lose; System identification; VSTOL aircraft; Vertical takeoff and landing;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2012 31st Chinese
Conference_Location
Hefei
ISSN
1934-1768
Print_ISBN
978-1-4673-2581-3
Type
conf
Filename
6390224
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