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HiMAT highly maneuverable aircraft technology, flight reportFlight verification of a primary flight control system, designed to control the unstable HiMAT aircraft is presented. The initial flight demonstration of a maneuver autopilot in the level cruise mode and the gathering of a limited amount of airspeed calibration data.
Document ID
19830015023
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:170245
NASA-CR-170245
H1-9-17
Report Number: NAS 1.26:170245
Report Number: NASA-CR-170245
Report Number: H1-9-17
Accession Number
83N23294
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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