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Accuracy of determining the state of a lunar satellite and the lunar gravitational field.Tracking geometry and dynamics of lunar satellite, estimating orbital elements and lunar gravitational field parameters through earth based range and range rate observations
Document ID
19670038478
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Compton, H. R.
Tolson, R. H.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 66-39
Report Number: AIAA PAPER 66-39
Accession Number
67A17207
Distribution Limits
Public
Copyright
Other
Keywords
TRACKING STUDY
LUNAR SATELLITE
LUNAR GRAVITATIONAL EFFECT
ORBIT CALCULATION

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