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Development Of A Digital Flight-Control SystemFeed-forward control path includes inversion of model of the aircraft. Report describes concept, development, tests of digital flight-control system for vertical-attitude-takeoff-and-landing aircraft. System based in airborne digital computer. Combines control of attitude and thrust in unified system for operation over full coupled ranges of velocity, altitude, attitude, and acceleration.
Document ID
19880000218
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Smith, G. Allan (NASA Ames Research Center, Moffett Field, Calif.)
Meyer, George (NASA Ames Research Center, Moffett Field, Calif.)
Date Acquired
August 13, 2013
Publication Date
April 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 4
ISSN: 0145-319X
Subject Category
Electronic Systems
Report/Patent Number
ARC-11778
Accession Number
88B10218
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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