DocumentCode :
358483
Title :
Lessons learned on the T-38 avionics upgrade program
Author :
Kish, Brian A. ; Deems, John ; Dunlop, Dawn ; Fitz, Eric
Author_Institution :
445th Fligh Test Squadron, Edwards AFB, CA, USA
Volume :
2
fYear :
2000
fDate :
2000
Firstpage :
49
Abstract :
Avionics testing is a major portion of all current aircraft flight-test programs. Lessons learned from the T-38 Avionics Upgrade Program are given. While the details are unique to the T-38 Avionics Upgrade Program, the lessons apply to all flight-test programs. Since no formal technical report was done for this program, this paper also serves as a written account of the program´s evolution. Four problem areas are listed which lead to the following lessons learned: do not let flying get ahead of data analysis. If the software does not work in software-in-the-loop facilities, it will not work in the airplane. However, software that works in software-in-the-loop facilities may not work in the airplane. Properly instrument the test aircraft based on its mission. Apply common sense logic when using existing drawings. If something does not look right, the drawing could actually be wrong. Incorporate operationally representative maneuvers in development test and evaluation. Test things one-by-one in development test and evaluation (i.e. use the scientific method of isolating one variable)
Keywords :
aircraft testing; military aircraft; military avionics; T-38 avionics upgrade program; aircraft flight-test programs; avionics testing; data analysis; development evaluation; development test; operationally representative maneuvers; software-in-the-loop facilities; Aerospace electronics; Aircraft navigation; Aircraft propulsion; Airplanes; Communication system control; Electric variables control; Electronic equipment testing; Instruments; System testing; Writing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
0-7803-5846-5
Type :
conf
DOI :
10.1109/AERO.2000.878213
Filename :
878213
Link To Document :
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