The Mars Observer mission will study Mars from a low-altitude orbit unlike that of any previous mission. During interplanetary cruise, propulsive maneuvers are required to satisfy limits on the probability of impact with Mars and to ensure capture. After Mars capture, the Observer must be brought to an accurate, near-circular mapping orbit through a series of maneuvers. Propulsive maneuver strategies have been developed to meet these needs. This paper describes the methods used in the analysis, the control capabilities, and the associated expected velocity changes for the mission.


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    Title :

    Maneuver analysis for the Mars Observer mission


    Contributors:

    Conference:

    AAS/AIAA Astrodynamics Conference 1989 ; 1989 ; Stowe, VT, United States


    Publication date :

    1990-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


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