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A Viking satellite orbit trim strategyOne strategy is submitted for meeting the varied and stringent requirements of the Viking Project on the control of the satellite orbit to obtain reconnaissance and to prepare for lander release. To satisfy these requirements, different orbit trim maneuver strategies were developed for two typical Viking missions. In addition, a summary of recent numerical results is included to show that this strategy satisfies the mission requirements which have been identified.
Document ID
19720003206
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hintz, G. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 6, 2013
Publication Date
October 1, 1971
Publication Information
Publication: JPL Quar. Tech. Rev., Vol. 1, No. 3
Subject Category
Space Vehicles
Accession Number
72N10855
Distribution Limits
Public
Copyright
Public Use Permitted.
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