Volume 47 Issue 12
Jan.  2019
Turn off MathJax
Article Contents

Zhao Yuchen, He Xin, Zhang Kai, Liu Qiang, Cui Yongpeng, Meng Qingyu. Optical design of miniaturized and large field of view off-axis optical system based on freeform surface[J]. Infrared and Laser Engineering, 2018, 47(12): 1218001-1218001(7). doi: 10.3788/IRLA201847.1218001
Citation: Zhao Yuchen, He Xin, Zhang Kai, Liu Qiang, Cui Yongpeng, Meng Qingyu. Optical design of miniaturized and large field of view off-axis optical system based on freeform surface[J]. Infrared and Laser Engineering, 2018, 47(12): 1218001-1218001(7). doi: 10.3788/IRLA201847.1218001

Optical design of miniaturized and large field of view off-axis optical system based on freeform surface

doi: 10.3788/IRLA201847.1218001
  • Received Date: 2018-07-17
  • Rev Recd Date: 2018-08-19
  • Publish Date: 2018-12-25
  • With the increasing development of space technology, space optical system with the characteristics of high-performance, miniaturization has become a new hotspot research in space optical fields. Off-axis three-mirror optical system has the advantage of high quality image, large field of view and high level of lightweight etc., which can better suit the application of miniaturized and low-cost space optical system and has broad application prospects. Based on the Gaussian optics and three-mirror aberration theory, the off-axis three-mirror with freeform surface of tertiary mirror was designed. The focal length was 1 550 mm, field of view was 3.60.45, relative aperture was 1:6.2, degrees of freedom and image quality were increased efficiently by the introduction of freeform surface. The design results show that system has a better performance in effective field of view, modulation transfer function value is above 0.43@111 lp/mm, wave-front error maximum value is 0.049 (=632.8 nm), RMS wave-front error value is 0.034 , maximum grid distortion value is 0.9%, and the imaging quality is complete symmetrical about the tangential plane. The total length of the optical system is less than f'/3.1, the height is less than f'/4.1, and is easily implemented because of the relatively loose tolerance about processing and assembling. The obtained results have a certain reference value for miniaturized space optical system.
  • [1] Ye Zhao, Li Xiwei, Wang Chao, et al. Survey of technological development of optical payload for micro-nano satellite[J]. Spacecraft Engineering, 2016, 25(6):122-130. (in Chinese)
    [2] Lampton M L, Sholl M J, Levi M E. Off-axis telescopes for dark energy investigations[C]//SPIE, 2010, 7731:77311G.
    [3] Zhao Wencai. Design of improved off-axis TMA optical systems[J]. Optics and Precision Engineering, 2011, 19(12):2837-2842. (in Chinese)
    [4] Ma Dingkun, Kuang Yin, Yang Xinquan. Development actual state and trends of nano-satellite[J]. Space Electronic Technology, 2017(3):42-45. (in Chinese)
    [5] Meng Qingyu, Wang Hongyuan, Wang Kejun, et al. Off-axis three-mirror freeform telescope with a large linear field of view based on an integration mirror[J]. Applied Optics, 2016, 55(32):8962-8970.
    [6] Gong Dun, Wang Hong. Optical design of large field and low distortion coaxial three mirror system with free-form surface[J]. Acta Optica Sinica, 2014, 34(7):0700001. (in Chinese)
    [7] Fuerschbach K, Rolland J P, Thompson K, P. A new family of optical systems employing -polynomial surfaces[J]. Optical Express, 2011, 19(22):21919-21928.
    [8] Meng Qingyu, Wang Hongyuan, Wang Yan, et al. Off-axis three-mirror freeform optical system with large linear field of view[J]. Infrared and Laser Engineering, 2016, 45(10):1018002. (in Chinese)
    [9] Zhang X, Zheng L G, He X, et al. Design and fabrication of imaging optical systems with freeform surfaces[J]. SPIE Optical Engineering Applications International Society for Optics and Photonics, 2012, 8486:848607.
    [10] Pan Junhua. Design, Fabrication and Testing of the Aspherical Optical Surfaces[M]. Suzhou:Soochow University Press, 2004:10-37. (in Chinese)
    [11] Li Peimao, Wang Xia, Jin Weiqi, et al. Dual-band infrared optical system design and image quality evaluation[J]. Infrared and Laser Engineering, 2013, 42(11):2882-2888. (in Chinese)
    [12] Chen Yonghe, Chen Hongda, Fu Yutian. Optical design of small-sized camera in visible for micro-satellite[J]. Infrared and Laser Engineering, 2015, 44(7):2087-2092. (in Chinese)
    [13] Xue Donglin, Zheng Ligong, Zhang Feng. Off-axis three-mirror system based on freeform mirror[J]. Optics and Precision Engineering, 2011, 19(12):2813-2820.
    [14] Wang Wei. Optical design of off-axis reflective system with freeform surface[D]. Nanjing:Nanjing University of Science and Technonogy, 2016:8-14. (in Chinese)
  • 加载中
通讯作者: 陈斌, bchen63@163.com
  • 1. 

    沈阳化工大学材料科学与工程学院 沈阳 110142

  1. 本站搜索
  2. 百度学术搜索
  3. 万方数据库搜索
  4. CNKI搜索

Article Metrics

Article views(710) PDF downloads(114) Cited by()

Related
Proportional views

Optical design of miniaturized and large field of view off-axis optical system based on freeform surface

doi: 10.3788/IRLA201847.1218001
  • 1. Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China

Abstract: With the increasing development of space technology, space optical system with the characteristics of high-performance, miniaturization has become a new hotspot research in space optical fields. Off-axis three-mirror optical system has the advantage of high quality image, large field of view and high level of lightweight etc., which can better suit the application of miniaturized and low-cost space optical system and has broad application prospects. Based on the Gaussian optics and three-mirror aberration theory, the off-axis three-mirror with freeform surface of tertiary mirror was designed. The focal length was 1 550 mm, field of view was 3.60.45, relative aperture was 1:6.2, degrees of freedom and image quality were increased efficiently by the introduction of freeform surface. The design results show that system has a better performance in effective field of view, modulation transfer function value is above 0.43@111 lp/mm, wave-front error maximum value is 0.049 (=632.8 nm), RMS wave-front error value is 0.034 , maximum grid distortion value is 0.9%, and the imaging quality is complete symmetrical about the tangential plane. The total length of the optical system is less than f'/3.1, the height is less than f'/4.1, and is easily implemented because of the relatively loose tolerance about processing and assembling. The obtained results have a certain reference value for miniaturized space optical system.

Reference (14)

Catalog

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return