METHOD FOR POSITIONING AN ACCESS OR LOADING ASSEMBLY AGAINST THE FUSELAGE OF AN AIRCRAFT

A method for positioning an access or loading assembly against the fuselage of an aircraft during the loading or unloading process, in which at least two multichannel scanners are oriented toward the aircraft fuselage and disposed above one another at a distance from each other, each with several light emitting units and at least one detector. First, a reference position is determined by using the scanners, and then a current position of the aircraft fuselage relative to the access or loading assembly is determined at determined time intervals by the multichannel scanners. The current position is compared with the reference position to determine a deviation. In case of a deviation between the two positions, a signal is transmitted to the control system of the positioning drive for realigning the access or loading assembly and reducing the deviation. 本发明涉及种用于在装载或卸载过程中在飞机的机身上定位进入装置的方法，其中，进入装置包括具有控制器的定位驱动器，进入装置朝向飞机机身地具有至少两个彼此间隔开地上下叠置的、具有多个光发射单元和至少个探测器的多通道扫描仪，该方法具有以下步骤：在进入装置的对接状态中借助于两个多通道扫描仪确定进入装置的基准位置，在到达基准位置之后通