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Accuracy of determining the state of a lunar satellite and the lunar gravitational field by using earth based range and range-rate observations.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
19660039158
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Compton, H. R.
Tolson, R. H.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 66-39
Report Number: AIAA PAPER 66-39
Accession Number
66A18448
Distribution Limits
Public
Copyright
Other
Keywords
TRACKING STUDY
LUNAR GRAVITATIONAL EFFECT
LUNAR SATELLITE
ORBIT CALCULATION

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