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%.
The Digital Data Acquisition System for the Flight Testing of the Fokker F29 Aircraft
1981
30 pages
Report
Keine Angabe
Englisch
Avionics , Aircraft , Digital systems , Flight test instruments , Fokker aircraft , Transport aircraft , Aircraft performance , Analog to digital converters , Certification , Channels (Data transmission) , Checkout , Data acquisition , Digital transducers , Inertial reference systems , Multiplexing , Telemetry , User requirements , Foreign technology
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