In the report the data acquisition system for the Fokker 100 test aircraft will be described: its capacity, its electrical lay-out, its real time presentation facilities and its performance parameters. Two important subsystems, the take-off and landing performance measuring system and the automatic noise measuring system will be highlighted. In an early stage it was decided to keep the data acquisition systems for both test aircraft identical. The savings on the design costs and the possibility to use each aircraft for most of the flight tests counterbalance the extra cost in instrumentation. It is concluded that very powerful data acquisition systems have been designed and installed in the Fokker 100 test aircraft, which perform to their specifications.


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    Title :

    Data Acquisition System for the Fokker 100 Test Aircraft


    Contributors:

    Publication date :

    1987


    Size :

    17 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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