Share Email Print

Proceedings Paper

Frame transfer CCD driving circuit design for space camera
Format Member Price Non-Member Price
PDF $17.00 $21.00

Paper Abstract

Micro-satellite is characterized by miniaturized structure and low cost, so it is a good choice to use area array CCD space camera as image system on micro-satellite. FT-18 is a monochrome frame transfer image sensor offering 1024×1024 pixels with excellent antiblooming and variable electronic shuttering. The main components of driving circuit for FT-18 include power supply unit, microcontroller unit, clock signal generator unit, and analog-to-digital (A/D) converter. The microcontroller unit controls startup sequence of all voltage, the exposure time of CCD and the working status of A/D converter; the clock signal generator unit generates sequence signals for CCD and A/D converter; the A/D converter converts the output of FT-18 to a 12-bit digital output. Special attention should be paid to the reliability of this camera for it will work in a condition different from ground. The camera may suffer from vacuum discharge, particle radiation, strong shock, hypergravity and so on. All these should be considered in the design of space camera, and enough environment tests should be done to ensure it can work normally in space.

Paper Details

Date Published: 28 November 2007
PDF: 7 pages
Proc. SPIE 6833, Electronic Imaging and Multimedia Technology V, 68331H (28 November 2007); doi: 10.1117/12.756652
Show Author Affiliations
Xin-hua Chen, Suzhou Univ. (China)
Jian-kang Zhou, Suzhou Univ. (China)
Wang Zhou, Suzhou Univ. (China)
Wei-min Shen, Suzhou Univ. (China)

Published in SPIE Proceedings Vol. 6833:
Electronic Imaging and Multimedia Technology V
Liwei Zhou; Chung-Sheng Li; Minerva M. Yeung, Editor(s)

© SPIE. Terms of Use
Back to Top
Sign in to read the full article
Create a free SPIE account to get access to
premium articles and original research
Forgot your username?