The invention relates to the technical field of aircraft assembly, in particular to a calibration auxiliary method for installation of aircraft avionics equipment, and the method comprises the steps: calculating the simulated pose coordinates of an adjustment point through avionics equipment simulated pose coordinate calculation based on a pitch angle and a roll angle; solving an optimal gasket specification type selection scheme of the adjustment points through pose adjustment optimization; and finally, adjusting the gasket according to the optimal scheme. Through the method, the problems of low efficiency, high labor intensity and large personal error can be effectively solved.
本发明涉及飞机装配技术领域,特别是涉及一种飞机航电设备安装的校准辅助方法,通过基于俯仰角和横滚角的航电设备模拟位姿坐标解算,计算调整点的模拟位姿坐标;通过位姿调整优化,求解调整点的垫圈规格选型最优方案;最终按最优方案实施垫圈调整。通过本方法,能有效解决效率低、劳动强度大和人为误差大的问题。
Calibration auxiliary method for installation of aircraft avionics equipment
一种飞机航电设备安装的校准辅助方法
2021-06-04
Patent
Elektronische Ressource
Chinesisch
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 / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung |
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