The principal design features and operational experiences of the X-29 forward-swept-wing aircraft and F-18 high alpha research vehicle (HARV) automated test systems are discussed. It is noted that operational experiences in developing and using these automated testing techniques have highlighted the need for incorporating target system features to improve testability. Improved target system testability can be accomplished with the addition of nonreal-time and real-time features. Online access to target system implementation details, unobtrusive real-time access to internal user-selectable variables, and proper software instrumentation are all desirable features of the target system. Also, test system and target system design issues must be addressed during the early stages of the target system development. Processing speeds of up to 20 million instructions/s and the development of high-bandwidth reflective memory systems have improved the ability to integrate the target system and test system for the application of automated testing techniques. It is concluded that new methods of designing testability into the target systems are required.


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    Title :

    Flight control system design factors for applying automated testing techniques


    Additional title:

    Faktoren beim Flugregelungssystementwurf für den Einsatz automatischer Prüftechniken


    Contributors:
    Sitz, J.R. (author) / Vernon, T.H. (author)


    Publication date :

    1990


    Size :

    13 Seiten, 10 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English







    Automated flight control functional testing

    LO JODI JO YEE / GALLO NICOLAS LUCAS / MOORE JOHNNY ROSS | European Patent Office | 2022

    Free access