An airborne data acquisition system around an airborne computer was realized. A standard interface unit was developed for interfacing the computer with various different sensor systems. All parts of a computer-controlled avionics data acquisition system (CADAS) were installed in standard instrumentation racks to enable full system integration and testing in the laboratory for each individual project. Two CADAS applications are discussed. The first application was the prototype evaluation of a multi-DME position reference system for the calibration of radio navigation aids and radars. The second application was the evaluation of a measurement method of the aircraft performance, during a dynamic maneuver.
A Computer-Controlled Avionics-Data Acquisition System
1978
32 pages
Report
Keine Angabe
Englisch
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