DocumentCode
1992921
Title
Flight Simulator Fidelity Evaluation Automated Test System Analysis
Author
Wang, Chunguang ; Han, Junwei ; Li, Guixian ; Jiang, Hongzhou
Author_Institution
Harbin Inst. of Technol., Harbin
Volume
2
fYear
2008
fDate
21-22 Dec. 2008
Firstpage
726
Lastpage
728
Abstract
An automated test system for evaluating flight simulator fidelity has been implemented. The system is designed to automatically test statically and dynamically the performance of flight simulator. The testing item file is designed, the file parser supporting for batch command file formats is presented, trim function and the flying part of the test are completed, evaluation way is presented. The ability to act on virtual pilot is the most important contributor to the test efficiencies of the automated test system.
Keywords
aerospace simulation; aircraft testing; program compilers; program diagnostics; program testing; automated test system analysis; batch command file format; file parser; flight simulator fidelity evaluation; trim function; Aerospace engineering; Aerospace simulation; Aerospace testing; Aircraft propulsion; Analytical models; Automatic testing; Computational modeling; Delay effects; Educational technology; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Education Technology and Training, 2008. and 2008 International Workshop on Geoscience and Remote Sensing. ETT and GRS 2008. International Workshop on
Conference_Location
Shanghai
Print_ISBN
978-0-7695-3563-0
Type
conf
DOI
10.1109/ETTandGRS.2008.352
Filename
5070465
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