A generalized mission design scheme which utilizes a standard mission profile for all OMV rendezvous operations, recognizes typical operational constraints, and minimizes propellant penalties due to nodal regression effects was developed. This scheme has been used to demonstrate a unified guidance and navigation maneuver processor (the UMP), which supports all mission phases through station-keeping. The initial demonstration version of the Orbital Rendezvous Mission Planner (ORMP) was provided for evaluation purposes, and program operation was discussed.


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    Title :

    Automatic Rendezvous and Docking Systems Functional and Performance Requirements


    Publication date :

    1985


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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