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Lateral stability augmentation of supersonic aircraft using multichannel optimal feedback control.Lateral stability augmentation of supersonic aircraft using linear multichannel state-vector optimal feedback control
Document ID
19670061426
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bass, R. W.
Stoner, J. W.
Taylor, F. J.
Date Acquired
August 3, 2013
Publication Date
January 22, 1966
Subject Category
Aircraft
Accession Number
67A40155
Distribution Limits
Public
Copyright
Other
Keywords
OPTIMAL CONTROL
STABILITY AUGMENTATION
STATE VECTOR
SUPERSONIC AIRCRAFT
LATERAL STABILITY
FEEDBACK CONTROL SYSTEM

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