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
Link To Document :
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