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星载TDI CCD动态成像全物理仿真系统设计

张刘 孙志远 金光

光学精密工程2011,Vol.19Issue(3):641-650,10.
光学精密工程2011,Vol.19Issue(3):641-650,10.DOI:10.3788/OPE.20111903.0641

星载TDI CCD动态成像全物理仿真系统设计

Design of physical simulation system for TDI CCD dynamic imaging

张刘 1孙志远 1金光2

作者信息

  • 1. 中国科学院,长春光学精密机械与物理研究所,吉林,长春,130033
  • 2. 中国科学院,研究生院,北京,130039
  • 折叠

摘要

Abstract

A ground-based physical TDI CCD imaging simulation system is developed, which consists of a high precision satellite 3-axis attitude control simulation subsystem based on a 3-axis air bearing table, and a TDI CCD imaging simulation subsystem whose TDI image procedure is simulated by software using an area-array CCD. The designed system realizes the simulation of satellite 3-axis attitude control with a maximum pointing accuracy of 0. 1° and a attitude steady accuracy of 0.01 (°)/s, and implements an imaging simulation of 4-stage to 16-stage TDI CCD with the integration time of 0. 1 s.Furthermore, the effect of satllite 3-axis attitude on the TDICCD photography is researched and the correction of the modeling theory for a space TDI CCD image motion model is proved. Experiment results show that the physical experiment results are in accordance with those of mathematical simulation and theoretical analysis,which justifies the feasibility of system design and the validity of image motion theory.

关键词

TDI CCD/物理仿真系统/姿态控制/像移

Key words

TDI CCD/ physical simulation system/ attitude control/ image motion

分类

航空航天

引用本文复制引用

张刘,孙志远,金光..星载TDI CCD动态成像全物理仿真系统设计[J].光学精密工程,2011,19(3):641-650,10.

基金项目

吉林省科技发展计划资助项目(No.20090102) (No.20090102)

国家自然科学青年基金项目资助(No.61008046) (No.61008046)

光学精密工程

OA北大核心CSCDCSTPCD

1004-924X

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