Off-axis TMA optical system for reducing processing and resetting difficulty
An optical system, off-axis technology, applied in the field of space optics, can solve problems such as difficulties, the system is difficult to achieve optical imaging indicators, etc., to achieve the effect of simple structure, overcoming the difficulty of processing and inspection, and convenient installation and adjustment
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[0015] Specific implementation mode 1. Combination figure 1 Describe this embodiment, an off-axis TMA optical system that reduces the difficulty of processing and assembly, including an infinite target 1, a primary reflector 2, a secondary reflector 3, a third reflector 4 and an imaging receiver 5, and the beam passes through infinity The target 1 is incident on the main reflector 2, is reflected by the main reflector 2 to the secondary reflector 3, is reflected by the secondary reflector 3 to the third reflector 4, and is received by the imaging receiver 5; the secondary reflector 3 is spherical surface, the main reflector 2 and the third reflector 4 are aspherical, and the quadratic coefficients of the main reflector 2 and the third reflector 4 are set to zero, and the main reflector 2 and the third reflector 4 are composed of Higher-order aspheric surfaces of sixth and eighth order.
specific Embodiment approach 2
[0016] Specific embodiment two, combine figure 2 , image 3 and Figure 4 This implementation mode is described. This implementation mode is an example of an off-axis TMA optical system that reduces the difficulty of processing and assembly described in the first specific implementation mode:
[0017] The parameters of the optical system of this embodiment are determined: the requirement is that the focal length f'=2000m, the relative aperture D / f'=1 / 8, D is the aperture of the optical system, the field of view angle is 17°, and the off-axis angle is 4.5°. The observation band of the system is 0.5 μm to 0.7 μm in the visible light band, and the imaging receiver is a TDI CCD with a pixel size of 10 μm. The satellite orbit height is 1000Km, the pixel resolution is 5m, the pixel size is 10μm, and the ground coverage width is 268Km.
[0018] The main structural parameters of the optical system are shown in Table 1.
[0019] Table 1
[0020]
[0021] It can be seen from Ta...
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