DocumentCode
1090386
Title
Crashproof codes [flight software]
Author
Hess, Ronald K. ; Bass, David I. ; Baca, John B.
Volume
41
Issue
9
fYear
2004
Firstpage
48
Lastpage
53
Abstract
Boeing Co. and NASA have joined forces for the Active Aeroelastic Wing (AAW) Project to test the way a modified F/A-18 strike fighter uses its wings. The AAW was designed to be flexible enough to be twisted on demand in flight and it could herald nothing less than a revolution in aviation. The twisting can be used to control the plane´s roll, reducing and ultimately eliminating the need for ailerons and flaps and their associated hardware. AAW-equipped planes would result to increased fuel efficiency and improved maneuverability, able to execute sharper turns at higher speeds. A special flight software was developed to keep track of the plane´s speed, altitude, and attitude while monitoring the pilot´s controls for commands. Based on a set of rules known as control laws, the software must then translate any commands from the pilot into movements of the aircraft´s various control surfaces such as the rudders or, most significantly, the flaps that flex the AAWs. Despite its complex and critical job, the flight software is compact, consisting of only about 13,000 lines of source code written in the Ada language.
Keywords
aerospace computing; aerospace control; aerospace testing; avionics; military aircraft; program testing; Active Aerolastic Wing project; aviation; flight software; supersonic aircraft; Computer crashes; Vehicle crash testing;
fLanguage
English
Journal_Title
Spectrum, IEEE
Publisher
ieee
ISSN
0018-9235
Type
jour
DOI
10.1109/MSPEC.2004.1330810
Filename
1330810
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