An integrated measuring, recording and data processing system for the evaluation and certification tests of the Fokker F29 aircraft is described. The on board digital data acquisition system user requirements are discussed. The system can measure and record more than 1400 parameters over a wide range of sampling rates. Several data acquisition units are located remotely. The system handles ARINC-429 digital data buses. Dynamic measurement of aircraft performance and accurate trajectory determination are possible. User requirements include a mission success probability of 99%.


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    Title :

    The Digital Data Acquisition System for the Flight Testing of the Fokker F29 Aircraft


    Contributors:

    Publication date :

    1981


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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