Need and justification for automatic, in-flight, thorough built-in test capabilities in advanced avionics systems is discussed and the need for a systems design approach is stressed. The role of an airborne digital computer for sequencing, conducting and evaluating the built-in test and the great flexibility of this computer, its characteristics, program and interface are developed and applicable test methods and design techniques are illustrated by typical examples. Short comings of methods used to continuously monitor all functions in flight and alternate builtin test methods are covered; evaluation logic and time-sharing of tests are discussed.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Automatic Built-in Test of Advanced Avionics Systems Part II: Design Technioues for Automatic Built-in-Test


    Contributors:


    Publication date :

    1966-07-01


    Size :

    1395363 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    F-15 avionics built-in-test

    Lang, L.E. | Tema Archive | 1978


    Avionics built-in-test effectiveness and life cycle cost

    PALAZZO, C. / ROSENFELD, M. | AIAA | 1983


    Built-In-Test software for an ADA avionics hot bench

    Moody, B.L. / Hensley, D.A. / Bennett, J.W. | Tema Archive | 1987