The embodiment of the invention discloses a method, device and equipment for determining the deflection angle of an aircraft control surface and a medium. The method comprises the following steps: acquiring each group of measurement data of a gyroscope mounted on an aircraft control surface aiming at the flight attitude of the aircraft in real time; and according to every two groups of measurement data with adjacent measurement time, respectively determining the deflection angle of the control surface of the aircraft. According to the technical scheme, the deflection angle of the control surface of the aircraft can be determined by utilizing the measurement data obtained by the gyroscope on the control surface of the aircraft, a measurement shaft of the gyroscope is not required to be parallel to a rotating shaft of the control surface of the aircraft when the gyroscope is mounted, and the gyroscope is simple in mounting process and convenient to operate. And the accuracy of the aircraft control surface deflection angle determined by the gyroscope measurement data is also high.
本发明实施例公开了一种飞机舵面偏转角度的确定方法、装置、设备及介质。该方法包括:实时获取安装在飞机舵面上的陀螺仪针对飞机飞行姿态的各组测量数据;根据测量时间相邻的每两组测量数据,分别确定飞机舵面偏转角度。在上述技术方案中,利用飞机舵面上的陀螺仪得到的测量数据即可确定飞机舵面偏转角度,在安装陀螺仪时无需要求陀螺仪的测量轴与飞机舵面转轴平行,陀螺仪的安装过程简单,通过陀螺仪测量数据确定的飞机舵面偏转角度的精确度也高。
Method, device and equipment for determining deflection angle of airplane control surface and medium
飞机舵面偏转角度的确定方法、装置、设备及介质
2023-01-13
Patent
Elektronische Ressource
Chinesisch
IPC: | G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / 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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