Abstract Application prospects, a functional diagram and algorithms for processing informative signals from a vortex aerodynamic angle and true airspeed sensor are considered. The requirements for transducers of pressure pulsations downstream of vortex generators are formed, a technique and connection of these transducers to the sensor circuit diagram are described. A technique is presented to analyze individual and resultant errors of the aerodynamic angle and true airspeed channels.
System engineering design of a vortex aerodynamic angle and true airspeed sensor
Russian Aeronautics (Iz VUZ) ; 56 , 3 ; 291-296
2013-07-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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