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Development of a microcomputer based integrated design system for high altitude long endurance aircraftA microcomputer-based integration of aircraft design disciplines has been applied theoretically to sailplane, microwave-powered aircraft, and High Altitude Long-Endurance (HALE) aircraft configurational definition efforts. Attention is presently given to the further development of such integrated-discipline approaches through the incorporation of AI techniques; these are then applied to the aforementioned case of the HALE. The windFrame language used, which is based on HyperTalk, will allow designers to write programs using a highly graphical, user interface-oriented environment.
Document ID
19890015788
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hall, David W.
(Hall (David) Consulting Sunnyvale, CA, United States)
Rogan, J. Edward
(Hall (David) Consulting Sunnyvale, CA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1989
Publication Information
Publication: NASA. Langley Research Center, Recent Advances in Multidisciplinary Analysis and Optimization, Part 1
Subject Category
Aircraft Design, Testing And Performance
Accession Number
89N25159
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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