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Real-time pilot guidance system for improved flight-test maneuversThe Dryden Flight Research Facility has developed a pilot trajectory guidance system that is intended to increase the accuracy of flight-test data and decrease the time required to achieve and maintain desired test conditions, or both. 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
19840032401
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Meyer, R. R., Jr.
(NASA Flight Research Center Edwards, CA, United States)
Schneider, E. T.
(NASA Flight Research Center Edwards AFB, CA, United States)
Date Acquired
August 12, 2013
Publication Date
November 1, 1983
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
AIAA PAPER 83-2747
Accession Number
84A15188
Distribution Limits
Public
Copyright
Other

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