Conventional accelerometer orientations obtain only a portion of the system performance available from the accelerometers. Therefore, the use of optimum nonorthogonal and redundant accelerometer orientations can result in significantly improved performance. This paper develops a general formulation of the accelerometer orientation optimization problem, presents solutions for certain special cases, and includes the results of examples to demonstrate the potential of non-conventional orientations.


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    Title :

    Optimizing Accelerometer Orientations


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    NASA Aerospace Vehicle Flight Control Conference ; 1965



    Publication date :

    1965-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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