Volume 47 Issue 7
Jul.  2018
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Mu Yongji, Wan Yuan, Liu Jiqiao, Hou Xia, Chen Weibiao. Optomechanical analysis and optimization of spaceborne lidar telescope primary mirror[J]. Infrared and Laser Engineering, 2018, 47(7): 718002-0718002(7). doi: 10.3788/IRLA201847.0718002
Citation: Mu Yongji, Wan Yuan, Liu Jiqiao, Hou Xia, Chen Weibiao. Optomechanical analysis and optimization of spaceborne lidar telescope primary mirror[J]. Infrared and Laser Engineering, 2018, 47(7): 718002-0718002(7). doi: 10.3788/IRLA201847.0718002

Optomechanical analysis and optimization of spaceborne lidar telescope primary mirror

doi: 10.3788/IRLA201847.0718002
  • Received Date: 2018-02-05
  • Rev Recd Date: 2018-03-03
  • Publish Date: 2018-07-25
  • Based on the fabricated and assembled lidar telescope, the structure of its primary mirror subsystem was presented. The effects on the primary mirror surface of the mismatch among the assembling points on the second supporting board and the malfunction of the flexible supporting foot on the first board were analyzed. The optomechanical analysis was conducted through establishing the finite element model of the primary mirror, the analyzing results were compared with the measured wave front map during the assembling. According to the analysis, the mismatch of the assembling points on the second baseplate was the main reason to deform the primary mirror surface. The primary mirror subsystem structure was optimized through integrated optomechanical analysis. And the expected root mean square deformation of the primary mirror should be decreased from 0.3 to 0.087, which meets the specification requirement of 0.15.
  • [1] Guo Y, Gu X, Yang S. Method to minimize the gravity sag of a facing ground 1 m flat mirror[C]//SPIE, 2006, 6148:61480D.
    [2] Huang Q, Gao Q, Yu J. FEM analysis of ultra thin mirror supporting structure effect on surface deformation in gravity field[C]//SPIE, 2006, 6148:61480W.
    [3] Lin Y C, Chang S T, Lee L J, et al. The gravity effect of optomechanical design on optical aberration for a remote sensing instrument[C]//34th Asian Conference on Remote Sensing, 2013, 5:4682-4686.
    [4] Cheng Zhifeng, Liu Fuhe, Xun Xianchao. Opto-mechanical design and analysis of dual-band sharing aperture imaging system[J]. Infrared Laser Engineering, 2015, 44(11):3366-3372. (in Chinese)
    [5] Stephen M M, Shelly C, William B H, et al. Structural, thermal, optical and gravitational modelling for LISA[J]. Classical and Quantum Gravity, 2004, 21(5):S603.
    [6] Liu J, Li B, Sun D, et al. Simulation analysis of on-orbit adjustment and compensation for large aperture optical system[C]//International Symposium on Advanced Optical Manufacturing and Testing Technologies:Large Mirrors and Telescopes, 2014, 9280(6):1045-1063.
    [7] Zhao L, Shao Y. Summary of thermal control and thermal-optical analysis for space optical system[J]. Spacecraft Recovery Remote Sensing, 2001, E83-A(5):835-841.
    [8] Zhang Yaoping, Fan Junqi, Long Guoyun. Finite element simulation of thermal distortions of deformable mirror with laser irradiation[J]. Infrared Laser Engineering, 2016, 45(11):1136002. (in Chinese)
    [9] Malacara D. Optical Shop Testing[M]. 3rd ed. New Jersey:John Wiley Sons, Inc, 2007.
    [10] 潘君骅. 光学非球面的设计、加工与检验[M]. 苏州:苏州大学出版社, 2004.
    [11] Doyle K B, Genberg V L, Michels G J. Integrated optomechanical analysis of adaptive optical systems[C]//SPIE, 2004:5178.
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Optomechanical analysis and optimization of spaceborne lidar telescope primary mirror

doi: 10.3788/IRLA201847.0718002
  • 1. Key Laboratory of Space Laser Communication and Detection Technology,Shanghai Institute of Optics and Fine Mechanics,Chinese Academy of Sciences,Shanghai 201800,China;
  • 2. University of Chinese Academy of Sciences,Beijing 100049,China

Abstract: Based on the fabricated and assembled lidar telescope, the structure of its primary mirror subsystem was presented. The effects on the primary mirror surface of the mismatch among the assembling points on the second supporting board and the malfunction of the flexible supporting foot on the first board were analyzed. The optomechanical analysis was conducted through establishing the finite element model of the primary mirror, the analyzing results were compared with the measured wave front map during the assembling. According to the analysis, the mismatch of the assembling points on the second baseplate was the main reason to deform the primary mirror surface. The primary mirror subsystem structure was optimized through integrated optomechanical analysis. And the expected root mean square deformation of the primary mirror should be decreased from 0.3 to 0.087, which meets the specification requirement of 0.15.

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