Techniques proposed to compensate guidance errors in aided-inertial guidance systems for long-term, low-thrust space missions are rotation of accelerometers with respect to inertially stabilized platform, statistical filtering of redundant position and/or velocity information and output of inertially fixed accelerometers, and combination of statistical filtering and rotation of accelerometers; effectiveness of techniques is analyzed; analytical and numerical results.


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    Title :

    Theory of error compensation in Astro-Inertial-Guidance systems for low-thrust space missions


    Additional title:

    Progress Astronautics Aeronautics


    Contributors:
    Dusek, H.M. (author)


    Publication date :

    1964


    Size :

    20 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :