The feasibility of using an electromechanical actuator (EMA) as the primary flight control equipment in aerospace flight is examined. The EMA motor design is presented utilizing improved permanent magnet materials. The necessary equipment to complete a single channel EMA using the single channel power electronics breadboard is reported. The design and development of an improved rotor position sensor/tachometer is investigated.
Electromechanical Flight Control Actuator
1979
129 pages
Report
Keine Angabe
Englisch
Electromechanical flight control actuator
Tema Archiv | 1976
Electromechanical flight control actuator
NTRS | 1976
Electromechanical flight control actuator
NTRS | 1979
AIRCRAFT FLIGHT CONTROL SYSTEM INCLUDING ELECTROMECHANICAL ACTUATOR
Europäisches Patentamt | 2020
|Aircraft flight control system including electromechanical actuator
Europäisches Patentamt | 2022
|