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Computation of spacecraft signal raypath trajectories relative to the sunA computer program (CTS 41B) used to determine the trajectory of a spacecraft signal raypath was updated to increase its usefulness during solar conjunctions (CTS 41C). The closest point of approach of the raypath to the sun is projected onto the surface and the solar latitude and longitude calculated. A sample computation and plots are given for the 1976 Viking solar conjunction. Eventually it may be possible to predict the communication link performance degradation in the near sun region due to solar activity.
Document ID
19770014176
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cannon, R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Stelzried, C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 8, 2013
Publication Date
April 15, 1977
Publication Information
Publication: The Deep Space Network
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Accession Number
77N21120
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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