DocumentCode :
1090477
Title :
Measuring Aircraft Carrier Flexure in Support of Autonomous Aircraft Landings
Author :
Petovello, Mark G. ; O´Keefe, Kyle ; Lachapelle, Gérard ; Canno, M. Elizabeth
Author_Institution :
Dept. of Geomatics Eng., Univ. of Calgary, Calgary, AB
Volume :
45
Issue :
2
fYear :
2009
fDate :
4/1/2009 12:00:00 AM
Firstpage :
523
Lastpage :
535
Abstract :
This paper quantifies the experimental measurements of aircraft carrier flexure (deformation) at sea in support of the United States Department of Defense sea-based Joint Precision Approach and Landing System (JPALS) that aims to deliver automatic landing capabilities to inbound aircraft aboard aircraft carriers. The methodology for measuring ship flexure using the Global Positioning System (GPS) and inertial sensors is described. Results indicate that flexure on the aircraft carrier used for testing has a standard deviation of approximately 1-2 cm. For the ship tested, the most significant flexure effects are in the port/starboard direction and correlate best with roll or lateral acceleration.
Keywords :
aircraft landing guidance; aircraft carrier flexure; automatic landing capabilities; autonomous aircraft landings; Aircraft; Global Positioning System; Life estimation; Marine vehicles; Position measurement; Sea measurements; Sensor phenomena and characterization; Sensor systems; Testing; US Department of Defense;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.2009.5089539
Filename :
5089539
Link To Document :
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