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Dynamic stability and handling qualities tests on a highly augmented, statically unstable airplaneThis paper describes some novel flight tests and analysis techniques in the flight dynamics and handling qualities area. These techniques were utilized during the initial flight envelope clearance of the X-29A aircraft and were largely responsible for the completion of the flight controls clearance program without any incidents or significant delays. The resulting open-loop and closed-loop frequency responses and the time history comparison using flight and linear simulation data are discussed.
Document ID
19880064225
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gera, Joseph
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Bosworth, John T.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Aircraft Stability And Control
Accession Number
88A51452
Distribution Limits
Public
Copyright
Other

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