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aeroservoelastic stabilization technique refinement for hypersonic flight vehiclesConventional gain-stabilization techniques introduce low frequency effective time delays which can be troublesome from the viewpoint of SSTOV vehicles' flying qualities. These time delays can be alleviated through a blending of gain-stabilization and phase-stabilization techniques; the resulting hybrid phase stabilization (HPS) for the low-frequency structural modes has been noted to have greater residual response than a conventional gain-stabilizer design. HPS design procedures are presently refined, and residual response metrics are developed.
Document ID
19930038293
Document Type
Conference Paper
Authors
Cheng, Peter Y.
(NASA Langley Research Center Hampton, VA, United States)
Chan, Samuel Y.
(McDonnell Aircraft Co. Saint Louis, MO, United States)
Myers, Thomas T.
(NASA Langley Research Center Hampton, VA, United States)
Klyde, David H.
(NASA Langley Research Center Hampton, VA, United States)
Mcruer, Duane T.
(Systems Technology, Inc. Hawthorne, CA, United States)
Date Acquired
August 16, 2013
Publication Date
December 1, 1992
Subject Category
AIRCRAFT STABILITY AND CONTROL
Report/Patent Number
AIAA PAPER 92-5014
Meeting Information
AIAA, International Aerospace Planes Conference(Orlando, FL)
Funding Number(s)
CONTRACT_GRANT: NAS1-18763
Distribution Limits
Public
Copyright
Other