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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    Titel :

    Optimizing Accelerometer Orientations


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    NASA Aerospace Vehicle Flight Control Conference ; 1965



    Erscheinungsdatum :

    01.02.1965




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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