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Iterative guidance applied to generalized missions.Iterative guidance mode /IGM/ applied to effective gravity vector prediction, acceleration measurement of noise sensitivity and energy limitations
Document ID
19670057280
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Buckelew, V. L.
Chandler, D. C.
Horn, H. J.
Date Acquired
August 3, 2013
Publication Date
August 1, 1967
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 67-620
Report Number: AIAA PAPER 67-620
Accession Number
67A36009
Distribution Limits
Public
Copyright
Other
Keywords
ITERATIVE SOLUTION
MISSION PLANNING
TRAJECTORY OPTIMIZATION
GUIDANCE AND CONTROL
GRAVITATIONAL EFFECT

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