Volume 33 Issue 2
Mar.  2013
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Article Navigation >  Chinese Journal of Space Science  > 2013  >  33(2): 200-206
Liu Shi, Zhang Guoyu, Sun Gaofei, Wang Lingyun. Design of dynamic star simulator based on LCOS optical splicing technology[J]. Chinese Journal of Space Science, 2013, 33(2): 200-206. doi: 10.11728/cjss2013.02.200
Citation: Liu Shi, Zhang Guoyu, Sun Gaofei, Wang Lingyun. Design of dynamic star simulator based on LCOS optical splicing technology[J]. Chinese Journal of Space Science, 2013, 33(2): 200-206. doi: 10.11728/cjss2013.02.200
shu

Design of dynamic star simulator based on LCOS optical splicing technology

doi: 10.11728/cjss2013.02.200 cstr: 32142.14.cjss2013.02.200
  • 1.

    OptoElectronic Engineering, Changchun University of Science and Technology, Changchun 130022

  • 2.

    Jilin Engineering Research Center of Photoelectric Measurement & Control Instruments, Changchun 130022

  • Received Date: 2011-12-01
  • Rev Recd Date: 2012-11-21
  • Publish Date: 2013-03-15
    Abstract
  • The technical scheme of a dynamic star simulator based on the LCOS optical splicing technology is proposed in order to meet the demands of a star sensor in spacecraft engineering. Optical system parameters of the simulator are calculated by the specification of a LCOS. The two LCOS optical splicing principle and scheme are introduced in detail, method of the dynamic star map realization is given, and its error is analyzed. The simulating results indicate that field of view is of 10.2° × 10.2°, star magnitude simulated is of 2～6.5, the single star field angle is less than 20", and the star diagonal distance error is less than 22". The experimental result can satisfy the system requirements of big field of view, wide magnitude range and update rate, etc.

     

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