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An investigation of the stability of a system composed of a subsonic canard airframe and a canted-axis gyroscope automatic pilot
Document ID
19930082667
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gardiner, Robert A
Zarovsky, Jacob
Ankenbruck, H O
Date Acquired
August 29, 2013
Publication Date
January 1, 1950
Report/Patent Number
NACA-TN-2004
Report Number: NACA-TN-2004
Accession Number
93R11957
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY & CONTROL - MISSILES - NAVY CTV-2 GORGON 2-C
AUTOMATIC PILOTS
MISSILES, GUIDED - TAIL-FIRST
INSTRUMENTS - GYROSCOPES
CONTROLS, SERVO
STABILITY & CONTROL - MISSILES
AUTOMATIC PILOTS - DIEHL UNI-PILOT

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