The invention relates to aircraft sensor system synchronization. Methods, apparatus, systems, and computer program products (1222) for operating an aerial imaging system (200) are disclosed. A first height (226) of the first aircraft (204) is determined by the computer system (210) using a first image (212) of a keypoint (220) generated by the first aircraft (204) during flight and a stereoscopic depth triangulation (224). The first height (226) is compared by the computer system (210) with a second height (230) of the second aircraft (206) determined by the second aircraft (206) to form a comparison result (232). An offset (238) between the first height (226) and the second height (230) is determined by the computer system (210) using the comparison result (232). At least one of the first height (226) or the second height (230) is adjusted based on the offset (238). A plurality of images of a region from a first aircraft (204) at a first altitude (226) and from a second aircraft (206) at a second altitude (230) are obtained.

    本申请题为“飞行器传感器系统同步”。本申请公开了用于操作航空成像系统(200)的方法、设备、系统和计算机程序产品(1222)。第一飞行器(204)的第一高度(226)由计算机系统(210)使用由第一飞行器(204)在飞行期间生成的关键点(220)的第一图像(212)和立体深度三角测量(224)来确定。由计算机系统(210)将第一高度(226)与由第二飞行器(206)确定的第二飞行器(206)的第二高度(230)进行比较,以形成比较结果(232)。第一高度(226)和第二高度(230)之间的偏移量(238)由计算机系统(210)使用该比较结果(232)来确定。基于偏移量(238)调整第一高度(226)或第二高度(230)中的至少一个。获得来自在第一高度(226)处的第一飞行器(204)和来自在第二高度(230)处的第二飞行器(206)的地区的多个图像。


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    Titel :

    Aircraft sensor system synchronization


    Weitere Titelangaben:

    飞行器传感器系统同步


    Beteiligte:

    Erscheinungsdatum :

    2022-06-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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