Electromechanical actuation of primary flight control surfaces has been demonstrated by the development of an integrated rotary hingeline dual-redundant actuation unit. Improved system bandwidth was demonstrated after employing improved sensors and electronic controls. (Author)
Electromechanical Actuation Development Program (EADP). Power Control Development
1981
146 pages
Report
Keine Angabe
Englisch
Avionics , Aircraft , Electromechanical devices , Actuation , Control , Power , Actuators , Electronic equipment , Detectors , Bandwidth , Aerodynamic control surfaces , Flight control systems , Integrated systems , Pulses , Permanent magnets , Samarium , Research management , Electronic control , Power control
Electromechanical Actuation Development
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