The invention provides a man-machine interaction accelerator calibration method, which comprises the following steps of S1, acquiring data acquired by an accelerator angle sensor, and transmitting the data to an avionics system; s2, the voltage value output by the accelerator angle sensor is restored to an accelerator angle value; s3, the accelerator angle value is sent to a liquid crystal display to be displayed through an AFDX bus; and S4, inputting a voltage value corresponding to the accelerator angle value through the electromechanical information processing system to calibrate the accelerator. According to the calibration method, an avionics system man-machine interaction interface on the aircraft is used, electromechanical system data are operated to carry out accelerator calibration easy to operate, ground crew can maintain the aircraft conveniently, and efficiency is improved.
本发明提供了一种人机交互的油门标定方法,所述方法包括如下步骤:S1:采集油门角度传感器采集的数据,将其输送至航电系统;S2:将油门角度传感器输出的电压值还原为油门角度值;S3:将油门角度值通过AFDX总线发送至液晶显示器显示;S4:通过机电信息处理系统输入油门角度值对应的电压值,以进行油门标定。该标定方法,使用飞机上航电系统人机交互界面,操作机电系统数据进行易操作的油门标定,便于地勤人员维护飞机,提高效率。
Man-machine interaction accelerator calibration method
一种人机交互的油门标定方法
2022-03-18
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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