The invention provides an aircraft axis boresight system and method. The boresight method comprises the steps that laser emitted by a laser emitter is filtered; the laser axis fixing device is used for splitting the laser beam; the two area-array cameras are used for imaging reflected and transmitted laser spots respectively; and the calculation module calculates the spatial centroid coordinates of the reflected and transmitted laser spot images and obtains a boresight result. The laser emitted by the laser assembly has good directionality, and the two area-array cameras can image reflected laser spots and transmitted laser spots at the same time, so that the robustness is improved; the transverse deviation and the longitudinal deviation between the coordinates of the cross section of the inlet of the fixed-axis channel after mirror image transformation of the spatial centroid coordinates of the reflected laser spot image and the spatial centroid coordinates of the transmitted laser spot image are calculated, so that the target correction precision is high; and video stream data of reflecting and transmitting laser spots are processed, and a target correction result is fed back in real time, so that the target correction efficiency is relatively high.
本发明提出了一种飞机轴线校靶系统与方法,校靶方法为:对激光发射器发射的激光进行滤光;激光定轴装置对激光束进行分光;两台面阵相机对反射和透射激光光斑分别进行成像;计算模块计算反射和透射激光光斑图像的空间质心坐标并获取校靶结果。本发明激光器组件发射的激光具有较好的定向性,且两台面阵相机能够对反射激光光斑和透射激光光斑同时进行成像,提高了鲁棒性;通过计算反射激光光斑图像的空间质心坐标进行镜像变换后位于定轴通道入口横截面处的坐标,以及透射激光光斑图像的空间质心坐标之间的横向偏差和纵向偏差,具有较高的校靶精度;处理的是反射、透射激光光斑的视频流数据并实时反馈校靶结果,具有较高的校靶效率。
Aircraft axis boresight system and method
一种飞机轴线校靶系统与方法
2024-11-19
Patent
Electronic Resource
Chinese
IPC: | G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen / 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 |
Aircraft boresight device and aircraft boresight method using same
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