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A theoretical method of determining the control gearing and time lag necessary for a specified damping of an aircraft equipped with a constant-time-lag autopilot
Document ID
19930082984
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gates, Ordway B , Jr
Schy, Albert A
Date Acquired
August 29, 2013
Publication Date
March 1, 1951
Report/Patent Number
NACA-TN-2307
Report Number: NACA-TN-2307
Accession Number
93R12274
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONTROLS - STABILITY
MATHEMATICS - TRANSFORMS
CONTROLS - FREQUENCY RESPONSE
STABILITY, LATERAL
CONTROLS - LAG
CONTROLS, PROPORTIONAL
OSCILLATIONS, LATERAL
AIRPLANES - FREQUENCY RESPONSE
STABILITY, DIRECTIONAL
AUTOMATIC PILOTS

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