The embodiment of the invention provides a servo load moment calculation method and equipment applied to an aircraft and a storage medium. The method comprises the steps of: acquiring a static load parameter of an air rudder in the aircraft, and determining a static load of the air rudder according to the static load parameter; acquiring a dynamic load parameter of the air rudder, and determininga dynamic load of the air rudder according to the dynamic load parameter; and determining a servo load moment of an aircraft servo system according to the static load and the dynamic load. According to the servo load moment calculation method and equipment applied to the aircraft and the storage medium provided by the embodiment of the invention, the control precision of the servo system can be improved.
本申请实施例提供一种应用于飞行器的伺服负载力矩计算方法、设备及存储介质,其中,方法包括:获取飞行器中空气舵的静态载荷参数,并根据所述静态载荷参数确定空气舵的静载荷;获取空气舵的动态载荷参数,并根据所述动态载荷参数确定空气舵的动载荷;根据所述静载荷和动载荷确定飞行器伺服系统的伺服负载力矩。本申请实施例提供的应用于飞行器的伺服负载力矩计算方法、设备及存储介质能够提高伺服系统的控制精度。
Servo load moment calculation method and equipment applied to aircraft and storage medium
应用于飞行器的伺服负载力矩计算方法、设备及存储介质
2020-12-25
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 / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung |
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