Space optical communication miniaturized terminal static aberration correction method
A space optical communication and aberration correction technology, applied in optics, optical components, sustainable communication technology, etc., can solve problems such as poor spot quality and unfavorable tracking function, and achieve the effect of eliminating static aberration and improving spot quality
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specific Embodiment approach 1
[0018] Specific implementation mode one: refer to figure 1 Specifically explain this embodiment, the method for correcting static aberration of a miniaturized terminal for spatial optical communication described in this embodiment, the method includes:
[0019] Step 1: Build an all-optical path module, the all-optical path system includes three light paths:
[0020] Optical path 1: The incident beacon light passes through the telescope, the tracking system and the piezoelectric deformable mirror in turn. After passing through the piezoelectric deformable mirror, the beacon light passes through the first beam splitter and then shrinks the beam. After the beam shrinks, it enters the Shaker-Hart Man wave front detector;
[0021] Optical path 2: The incident light passes through the telescope, the tracking system and the piezoelectric deformable mirror in sequence. The beacon light after passing through the piezoelectric deformable mirror passes through the first beam splitter an...
specific Embodiment approach 2
[0025] Embodiment 2: This embodiment is a further description of Embodiment 1. The difference between this embodiment and Embodiment 1 is that the specific steps of Step 2 are:
[0026] Step 21: Turn on the telescope, and the telescope receives the opposite incident light;
[0027] Step 22: Apply an initial voltage u to the electrodes of the piezoelectric deformable mirror 0 ={0,0,...0};
[0028] Step two and three: use the pixels on the CCD2 to calculate the evaluation function J k (u k ),in,
[0029] I i is the center of the CCD2 disc, I i the diameter is λ is the wavelength of the beacon light, λ is 808nm, f is the focal length of the CCD2 front lens, f is 20mm, D is the lens aperture, D is 10mm, I o Remove the disk center I in CCD2 i the ring, I o the diameter is J is the evaluation function, k represents the kth iteration result, and u represents the control voltage vector of the piezoelectric deformable mirror;
[0030] Step 24: Randomly generate a disturb...
specific Embodiment approach 3
[0036] Embodiment 3: This embodiment is a further description of Embodiment 2. The difference between this embodiment and Embodiment 2 is the change δJ of the evaluation function k Expressed as:
[0037]
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