Share Email Print

Proceedings Paper

Design concept for a secondary-payload Earth observation camera
Author(s): Klaus Janschek; Valerij Tchernykh; Sergey V. Dyblenko
Format Member Price Non-Member Price
PDF $14.40 $18.00
cover GOOD NEWS! Your organization subscribes to the SPIE Digital Library. You may be able to download this paper for free. Check Access

Paper Abstract

The concept of the small, medium resolution Earth observation camera (14 - 20 m per pixel) using a joint transform optical correlator is proposed. The camera is intended to be used as a secondary payload for low orbit, 3-axis stabilized spacecraft, including ones with moderate attitude stability. The optical correlator is used for a real-time determination of the camera pointing motion for posteriori correction of the image distortions due to attitude unstability. A wide angle lens and long assembly of the line sensors in the focal plane permit to change the view direction without need to move the satellite or camera elements. A possible layout of the optoelectronic unit is described and the results of simulated experiments, expected performances and size estimations are given.

Paper Details

Date Published: 28 December 1999
PDF: 9 pages
Proc. SPIE 3870, Sensors, Systems, and Next-Generation Satellites III, (28 December 1999); doi: 10.1117/12.373166
Show Author Affiliations
Klaus Janschek, Dresden Univ. of Technology (Germany)
Valerij Tchernykh, Ufa State Aviation Technical Univ. (Germany)
Sergey V. Dyblenko, Ufa State Aviation Technical Univ. (Germany)

Published in SPIE Proceedings Vol. 3870:
Sensors, Systems, and Next-Generation Satellites III
Hiroyuki Fujisada; Joan B. Lurie, Editor(s)

© SPIE. Terms of Use
Back to Top