Telecentric imaging system with field of view of 15 degrees and three coaxial reflectors
An imaging system and mirror technology, applied in the field of space optics, can solve problems such as not being able to meet the requirements of the field of view width, and achieve the effects of less difficulty in system processing and assembly, easy system assembly, and reduced complexity
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[0012] The invention according to figure 2 The structure shown is implemented. Among them, the focal length of the image side is selected as f ′=-720mm, the relative aperture D / F=1 / 4, the off-axis angle of the field of view is 8°, and the curvature radius R of the apex of the primary mirror 6 reflective surface is 1 =-1846.21236mm, the curvature radius R of the vertex of the reflective surface of secondary mirror 7 2 =-566.92974mm, the vertex curvature radius R of the three mirrors and eight reflective surfaces 3 =-809mm, the distance d from the primary mirror 6 to the secondary mirror 7 1 =-404.5mm, the distance d from the secondary mirror 7 to the third mirror 8 2 =404.5mm, the distance d between the three mirrors 8 and the image plane 10 3 =-666.26761mm, the aspheric coefficient e of the primary mirror 6 reflective surface 1 2 =4.44886, e 1 4 =2.56243e-011, the aspheric coefficient e of the reflective surface of secondary mirror 7 2 2 =0, the aspheric coefficient...
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