Space-ray-tracing-based method for designing secondary mirror hood and square-tapered extinction cone
A technology of ray tracing and design method, which is applied in the field of aerospace remote sensing, can solve problems such as occlusion, and achieve the effects of volume reduction, size minimization, and weight reduction
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[0058] For the visible spectrum, the field of view in the X direction is ±1.0°, the field of view in the Y direction is -1~-0.6°, and the RC system with an entrance pupil diameter of 359.6mm is used for the extinction cone of the secondary mirror hood and the central hole of the square conical primary mirror. Joint design.
[0059] Such as figure 1 Shown, concrete steps of the present invention are as follows:
[0060] (1) According to figure 2 As shown, a Cartesian rectangular coordinate system is established;
[0061] (2) Based on the tracing results of the four auxiliary rays in the meridional and sagittal planes, the boundary of the extinction cone of the central hole of the square conical primary mirror is calculated
[0062] build as image 3 The equations of the four auxiliary rays R1, R2, R3 and R4 shown are:
[0063]
[0064]
[0065]
[0066]
[0067] Tracing the 4 auxiliary rays in Fred, the linear equations l1', l2', l3' and l4' of the 4 rays refl...
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