A detailed analysis of space shuttle navigation for each of the major mission phases is presented. A covariance analysis program for prelaunch IMU calibration and alignment for the orbital flight tests (OFT) is described, and a partial error budget is presented. The ascent, orbital operations and deorbit maneuver study considered GPS-aided inertial navigation in the Phase III GPS (1984+) time frame. The entry and landing study evaluated navigation performance for the OFT baseline system. Detailed error budgets and sensitivity analyses are provided for both the ascent and entry studies. (Author)


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    Title :

    Space Shuttle Navigation Analysis


    Contributors:

    Publication date :

    1976


    Size :

    230 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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