In-orbit monitoring method for 6 freedom change between space three-linear array CCD camera lens
A degree of freedom, three-line array technology, applied in the field of aerospace satellite photogrammetry, can solve problems such as complicated process, inability to perform real-time monitoring, and long time consumption
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[0029] Such as figure 1 , 2 Shown is a flow chart and a schematic diagram of the monitoring method of the present invention. figure 2 Middle: 4 and 11 represent camera lens B and camera lens A respectively, 2 is the measurement bracket, the measurement bracket is located on the camera lens B, and is used to rigidly fix the laser reflection receiving device. The laser reflection receiving device includes a plane mirror 3, a second surface Array CCD12 and the third array CCD1. The laser emitting and receiving device is located on the camera lens A, and the laser emitting and receiving device includes a semiconductor laser light source 10 (other laser light sources can also be selected), a fiber coupler 9, a half-mirror 5 and the first area array CCD6, and the 9 is an optical fiber coupling 7 is a collimator (three), used to collimate the three lasers, and 8 is an optical fiber (four).
[0030] Since the measurement bracket is rigidly fixed with a lens B to be tested of the a...
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