A general theory of the design of flight vehide instruments and sensors is developed, and methods of calculating their static and dynamic characteristics, instrument errors, and reliability reartings are prosented. A general method for calculating the characteristics and errors of instruments and sensors, based on an analysis of structural circuits, is presented. This method gives a clear idea of the role of transforming elements in the formation of the resulting characteristics and errors of instruments and sensors.


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    Title :

    Flight vehicle instruments and senscrs


    Additional title:

    Titel russisch


    Contributors:


    Publication date :

    1970


    Size :

    1 Seite, 154 Quellen


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Russian




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