Abstract We consider the aircraft system hardware and software to measure the angular deflections of control surfaces. The experimental studies of a photoelectric transducer for converting the control surface angular deflections into digital codes are performed. The mathematical models are obtained to describe a dependence of measuring errors on the coordinates of emitter arrangement. The optimal emitter arrangement is determined using the mathematical models and a pilot model of the aircraft system proposed has been developed.
Aircraft system for measuring the angular deflections of control surfaces
Russian Aeronautics (Iz VUZ) ; 56 , 4 ; 418-422
2013-10-01
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aircraft system for measuring the angular deflections of control surfaces
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