An imaging system with 15° field of view telecentric three mirrors coaxial
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 presses figure 2 The structure shown is implemented. Among them, select the image side focal length f′=-720mm, the relative aperture D / F=1 / 4, the off-axis angle of the field of view is 8°, and the radius of curvature of the apex of the reflection surface of the main mirror 6 is R 1 =-1846.21236mm, the radius of curvature of the vertex of the reflective surface of the secondary mirror 7 R 2 = -566.92974mm, the radius of curvature R of the vertex of the reflection surface of the three mirrors 8 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 from the three mirrors 8 to the image plane 10 3 = -666.26761mm, the aspheric coefficient e of the reflective surface of the main mirror 6 1 2 = 4.44886, e 1 4 =2.56243e-011, the aspheric coefficient e of the reflective surface of the secondary mirror 7 2 2 =0, the aspheric coefficient e o...
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