This paper presents tests of Electromechanical Actuators (EMA) designed in the Department of Avionics and Control at the Rzeszow University of Technology. Also, the architecture of the laboratory stand as well as testing methods and obtained results are described. Furthermore, the paper discusses the in-flight test results of the complete set of servos installed as a part of the experimental Fly-By-Wire (FBW) control system on board of the PZL-110 “Koliber” aircraft.
Laboratory and Preliminary In-Flight Tests of Electromechanical Actuators
Sae Technical Papers
General Aviation Technology Conference & Exhibition ; 2006
30.08.2006
Aufsatz (Konferenz)
Englisch
Electromechanical flight actuators for advanced flight vehicles
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