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Iterative guidance applied to generalized missions.Iterative guidance mode /IGM/ applied to effective gravity vector prediction, acceleration measurement of noise sensistivity and energy limitations
Document ID
19690037512
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Buckelew, V. L.
Chandler, D. C.
Horn, H. J.
Date Acquired
August 5, 2013
Publication Date
January 1, 1969
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 67-620
Report Number: AIAA PAPER 67-620
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, GUIDANCE, CONTROL AND FLIGHT DYNAMICS CONFERENCE
Location: HUNTSVILLE, ALA.
Start Date: August 14, 1967
End Date: August 16, 1967
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A15501
Distribution Limits
Public
Copyright
Other

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