DocumentCode
2299037
Title
Rapid systems integration of navigation avionics
Author
Zetzl, Larry ; Fuller, Andrew ; Andrews, Roger
Author_Institution
Naval Avionics Center, Indianapolis, IN, USA
fYear
1991
fDate
20-24 May 1991
Firstpage
394
Abstract
The authors illustrate the techniques and philosophies of using simulations as a tool to help reduce the cost and schedule associated with navigation system integration. The ES-3A navigation integration is use to illustrate specific implementation considerations and lessons learned. The approach for this project was to reuse generic aircraft flight simulation software developed under previous programs and add avionics modules unique to this platform as needed. It is concluded that the DASL (Digital Avionics System Laboratory) has been a valuable asset in testing and integrating the ES-3A navigation and steering software. The lab offered a dynamic environment in which to test the entire navigation effort of the flight computer in high-risk situations which could not be tested during flight test. The environment made it possible to prove the fault-tolerance of the navigation and steering software prior to flight test
Keywords
aerospace computer control; aerospace simulation; aircraft instrumentation; computerised navigation; fault tolerant computing; program testing; software engineering; ES-3A navigation integration; aircraft flight simulation software; avionics modules; cost; dynamic environment; dynamic software integration; fault-tolerance; flight computer; flight test; navigation avionics; navigation software; static software integration; steering software; Aerospace electronics; Aircraft navigation; Computational modeling; Computer simulation; Costs; Hardware; Military computing; Performance evaluation; Software testing; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 1991. NAECON 1991., Proceedings of the IEEE 1991 National
Conference_Location
Dayton, OH
Print_ISBN
0-7803-0085-8
Type
conf
DOI
10.1109/NAECON.1991.165779
Filename
165779
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