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Use of nonlinearities to compensate for the effects of a rate-limited servo on the response of an automatically controlled aircraft
Author:
Schmidt, Stanley F.
Year:
1955
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3387
Link:
https://digital.library.unt.edu/ark:/67531/metadc57354/
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