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Linear feedback guidanceDetermination of closed loop guidance function with linear, time-variable feedback studied by behavior of motion equations
Document ID
19660021236
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dickey, L. R. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
November 30, 1965
Subject Category
Navigation
Report/Patent Number
NASA-TM-X-53362
Report Number: NASA-TM-X-53362
Accession Number
66N30526
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FEEDBACK
GUIDANCE SYSTEM
MOTION EQUATION
LINEAR SYSTEM
CLOSED LOOP SYSTEM

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