DocumentCode
1967132
Title
LXI addresses aircraft flight control system simulation test
Author
Chaoyou, Zhi ; Zhenshui, Li ; Xia, Li
Author_Institution
First Aircraft Inst., Xi´´an
fYear
2007
fDate
17-20 Sept. 2007
Firstpage
511
Lastpage
516
Abstract
The increase for requirements in reusability and flexibility has created new challenge in the development of aircraft flight control system simulation test. Incorporating LXI devices as a part of a system not only can provide an additional level of flexibility and capability for the specific application, but also can support custom requirements with minimal cost and testing time. This paper describes our research and development efforts in the application of LXI devices in aircraft flight control system simulation test, the paper specifies the measurement and test system hardware architecture and software architecture. The interchangeable virtual instruments (IVI) tools and architectural elements enable user to develop software systems that is independent of the underlying instruments. The paper also described how IVI drivers and associated IVI shared components are used to develop a system. An example program using instruments based on LXI to acquisition data is presented.
Keywords
aerospace computing; aerospace simulation; aircraft control; control engineering computing; virtual instrumentation; LXI devices; aircraft flight control system simulation test; interchangeable virtual instruments; Aerospace control; Aerospace simulation; Aircraft; Application software; Costs; Instruments; Research and development; Software measurement; Software testing; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Autotestcon, 2007 IEEE
Conference_Location
Baltimore, MD
ISSN
1088-7725
Print_ISBN
978-1-4244-1239-6
Electronic_ISBN
1088-7725
Type
conf
DOI
10.1109/AUTEST.2007.4374261
Filename
4374261
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