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Real-time pilot guidance system for improved flight test maneuversThe Dryden Flight Research Facility of the NASA Ames Research Center has developed a pilot trajectory guidance system that increases the accuracy of flight-test data and decreases the time required to achieve and maintain desired test conditions. The system usually presented to the pilot computed differences between reference or desired and actual flight state conditions. The pilot then used a cockpit display as an aid to acquire and hold desired test conditions. This paper discusses various flight-test maneuvers and the quality of data obtained using the guidance system. Some comparisons are made between the quality of maneuvers obtained with and without the system. Limited details of the guidance system and algorithms used are included. In general, the guidance system improved the quality of the maneuvers and trajectories flown, as well as allowing trajectories to be flown that would not have been possible without the system. This system has moved from the developmental stage to full operational use in various Dryden research and test aircraft.
Document ID
19840008108
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Meyer, R. R., Jr.
(NASA Ames Research Center Moffett Field, CA, United States)
Schneider, E. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-TM-84922
NAS 1.15:84922
H-1204
Report Number: NASA-TM-84922
Report Number: NAS 1.15:84922
Report Number: H-1204
Meeting Information
Meeting: AIAA 2nd Flight Test Conf.
Location: Las Vegas, NV
Country: United States
Start Date: November 16, 1983
End Date: November 18, 1983
Accession Number
84N16176
Funding Number(s)
PROJECT: RTOP 505-31-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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