A special purpose digital data acquisition system is built for stall/spin flight research. A Schweizer 2-32 sailplane is used as the test vehicle. Computer hardware and its architecture are described. Concepts of system failure detection are considered in the design. Special instrumentation developed for the high angle of attack flight is presented. A representative flight time history of a maneuver also is shown. The flight data will be used for the identification of aerodynamic parameters.
Data acquisition for stall/spin flight research
1983-10-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
NTIS | 1989
|A microprocessor-based data-acquisition system for stall/spin research
Tema Archiv | 1983
|