DocumentCode
3136769
Title
Numerical analysis of the terminal approach carrier disturbance model
Author
Li, Xinfei ; Zhang, Zhi ; Zhu, Qidan
Author_Institution
Coll. of Autom., Harbin Eng. Univ., Harbin, China
fYear
2012
fDate
5-8 Aug. 2012
Firstpage
2235
Lastpage
2239
Abstract
In order to study carrier landing disturbance which is the most resource of carrier landing deviation, The filters of free-air turbulence components are presented by used of the method which transfers spatial power spectrum to temporal power spectrum. The method of changing transfer function to spatial state is proposed to solve the problem of temporal-varying parameters in the random component of carrier airwake. The Simulation model is constructed in Matlab. It is result that: the simulation model of carrier landing disturbance is effective, and a method of improving symmetrical characteristic of carrier landing disturbance is recommended.
Keywords
military aircraft; military systems; naval engineering; numerical analysis; wakes; Matlab; carrier airwake; carrier landing deviation; carrier landing disturbance model; changing transfer function; free air turbulence component; numerical analysis; simulation model; spatial power spectrum; spatial state; temporal power spectrum; temporal varying parameter; Aircraft; Analytical models; Atmospheric modeling; Educational institutions; Marine vehicles; Mathematical model; Transfer functions; carrier landing; carrier landing disturbance; carrier-based aircraft; spatial power spectrum; state spatial; transfer function;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation (ICMA), 2012 International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4673-1275-2
Type
conf
DOI
10.1109/ICMA.2012.6285691
Filename
6285691
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