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State-vector control applied to lateral stability of high-performance aircraftState vector control applied to problem of lateral stability augmentation of high performance aircraft
Document ID
19650018213
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Oehman, W. I. (NASA Langley Research Center Hampton, VA, United States)
Suddath, J. H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1964
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-2894
Report Number: NASA-TN-D-2894
Accession Number
65N27814
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY AUGMENTATION
STATE VECTOR
LATERAL STABILITY

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