The invention discloses control equipment of an aircraft horizontal stabilizer trim actuator and a control method of the control equipment. The control equipment can be connected with the actuator through a plurality of plugs. The control equipment comprises two alternating current signal generators, a feedback processor, a steering control power supply, a driving power supply and a control power supply; the steering control power supply, the driving power supply and the control power supply are respectively connected with the servo motor through switches; the first alternating current signal generator is connected with a command RVDT through a switch; the second AC signal generator is connected with the monitoring RVDT through the switch. The feedback processor is respectively connected with the command RVDT and the monitoring RVDT; the feedback processor is connected with the steering control power supply. Setting a reference angle of the servo motor; and the feedback processor converts the reference angle into a voltage control signal and transmits the voltage control signal to the steering control power supply so as to control the servo motor to move according to a set angle. The control equipment provided by the invention is high in integration level, the control method is simple, the working efficiency is improved, and the error rate is low.
本申请公开了飞机水平安定面配平作动器的控制设备及其控制方法,控制设备能够通过多个插头与作动器连接;控制设备包括两个交流信号发生器、反馈处理器、转向控制电源、驱动电源和控制电源;转向控制电源、驱动电源和控制电源分别通过开关与伺服电机连接;第一交流信号发生器通过开关与命令RVDT连接;第二交流信号发生器通过开关与监控RVDT连接;反馈处理器分别与命令RVDT和监控RVDT连接;反馈处理器与转向控制电源连接。设定伺服电机的参考角度;反馈处理器将参考角度转换为电压控制信号并传输至转向控制电源,以控制伺服电机按设定角度运动。本申请提供的控制设备集成度高,控制方法简单,增加工作效率且错误率低。
Control equipment and control method of aircraft horizontal stabilizer trim actuator
飞机水平安定面配平作动器的控制设备及其控制方法
09.05.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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