Schematic diagrams are given for both the four-channel electromechanical actuator and the single-channel power electronics breadboard. Detailed design data is also given on the gears used in the differential gearbox and a copy of the operations manual for the system is included. Performance test results are given for the EMA motor and its current source indicator, the drive control electronics, and the overall system. The power converter waveform test results are also summarized.
Electromechanical flight control actuator, volume 2
1978-01-01
Report
No indication
English
Electromechanical flight control actuator
Tema Archive | 1976
Electromechanical flight control actuator
NTRS | 1979
Electromechanical flight control actuator
NTRS | 1976