The invention relates to a space orientation computing method for a
numerical control bracket, which comprises the following steps of: 1,
processing three-dimensional digital analogy of each part; 2, defining a fixed mechanism and a moving mechanism in each digital analogy; 3, setting a drive command for a multiple axis movements of a
numerical control bracket; 4, simulating whether each axis movement accords with an actual condition; 5, correcting a movement zero point of the digital analogy of the
numerical control bracket; 6, enabling a spindle axes of an automatic drilling and riveting
machine to be coincident with a normal line of a riveting point and the riveting point to be coincident with the center of a pressure foot bush; 7, refreshing the digital analogy; 8, figuring out data of five axes of the numerical digital bracket and data of a lifting position and a rotating angle of a lower riveting head under the condition of automatic drilling and riveting on any point on the surface of an
airplane; 9, carrying out
collision checking and batch output on space orientation data; and 10, carrying out numerical control
programming to ensure that the automatic drilling and riveting
machine continuously operates. According to the space orientation computing method, the
numerical control system can automatically operate according to the space orientation data, and the
airplane on the numerical control bracket meets the working requirements of the automatic drilling and riveting
machine on the space.