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Mars Observer orbit determination analysisResults are presented of a simulated orbit determination analysis for three phases of the Mars Observer mission (interplanetary cruise, orbit insertion, and mapping), together with a summary of orbital accuracies throughout the Mars Observer mission. The plan for achieving the navigation objectives of the Mars Observer mission is described. These objectives are to navigate the Mars Observer spacecraft to Mars and achieve accurate targeting at Mars; to propulsively maneuver the spacecraft into a 3-day period, capture orbit; to navigate the spacecraft into a 1.96-hr period low-altitude, nearly circular mapping orbit; and to maintain Mars Observer in the mapping orbit throughout the 687 days devoted for scientific data acquisition. Factors that will affect the spacecraft during each of the three phases are discussed.
Document ID
19920027834
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Esposito, Pasquale
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Roth, Duane
(JPL Pasadena, CA, United States)
Demcak, Stuart
(OAO Corp. Altadena, CA, United States)
Date Acquired
August 15, 2013
Publication Date
October 1, 1991
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 28
ISSN: 0022-4650
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
ISSN: 0022-4650
Accession Number
92A10458
Distribution Limits
Public
Copyright
Other

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