Large rectangular plane mirrors are widely used in high-power laser systems and synchrotron radiation sources, their surface precision affecting optical system performance. High-precision measurement methods are required to match these mirrors. The oblique incidence absolute measurement technique based on the rotational averaging method is a commonly method for these mirrors. But this method is complex, requires two additional plane mirrors. And it is limited by the angle of incidence, making it impossible to achieve both large aperture and high-resolution measurement simultaneously. Moreover, the method requires disassembling the test mirror during measurement, which significantly complicates the setup and adjustment process. Addressing the aforementioned shortcomings, this paper presents a high-precision measurement method for large rectangular plane mirrors. This method combines subaperture stitching techniques with the absolute measurement approach using the double shear translation method. It divides the test mirror into multiple overlapping subapertures and applies the double shear translation method to conduct absolute measurement on each subaperture region sequentially. Subsequently, employs algorithm to stitch the results together to achieve a complete surface. This method balances large aperture and high-resolution measurement, eliminates the influence of the reference surface. During the measurement process, only translations of the test mirror are required, making setup and adjustment relatively straightforward. Experimental validation of this method has demonstrated its ability to achieve high-precision measurement of rectangular plane mirrors. This paper presents an effective approach for high-precision measurement of large rectangular plane mirrors.
As an important means of anti-ballistic missile weapons ,it is used for early detection of missiles, determination of missile parameters, determination of targets to be attacked by missiles, and provides advance warning for national strategic defence decisions. It plays an important role in ballistic missile defence system. The early warning satellites located in space are not limited by the curvature of the earth, they are condescending and have a wide coverage area, which can detect ballistic missiles moving in space early. Multi-band joint early warning has become an important development trend of space-based early warning. Space-based ultraviolet early warning is an effective early warning means that uses the ultraviolet radiation of missiles to detect missile targets in the active phase and re-entry phase. Based on the normalized detection rate, this paper deduces the formula for calculating the detection distance according to the sensitivity of the UV detector, and simulates the relationship between the system aperture and the detection distance ,as well as the relationship between the detection signal-to-noise ratio and the target temperature .The simulation results show that the system aperture of 50mm can meet the requirement of the signal-to-noise ratio of 6. With the increase of the target temperature ,the signal-to-noise ratio increases rapidly. According to the simulation results, a geostationary orbit space-based ultraviolet early warning system scheme is designed. The optical system adopts the off-axis total reflection type, and the working spectrum is 200~300nm, 220~290nm, 230~280nm, 255~275nm. For the spectrum segment ,four 9°×9° fields of view are spliced to achieve the requirement that the system’s field of view is not less than 18°×18°, ensuring global and earth limb coverage. Four cameras achieve full field of view coverage. Filters with different spectral are placed in front of the focal plane of each camera. The filters are installed on the filter wheel and driven by a motor to realize real-time monitoring of the world and obtain different spectral bands. Sections of experimental date to support background and target characterization studies. The structure design of this scheme is novel and has certain reference significance.
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