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Because the satellite comes under influences from all kinds of disturbance and some of them can not be absorbed by
flywheel control system during the circulation, attitude of satellite is disturbed, which results in pixel excursion of the
scan mirror image, and image quality is affected. It is necessary to be compensated. Spacecraft motion compensation
means that the influences of attitude disturbance are eliminated through producing scan mirror motion control
compensation signal according to compensation arithmetic. It can be realized by using real-time compensation method
and model predictor method. This paper studies real-time spacecraft motion compensation method. The valid arithmetic
of spacecraft motion compensation and practicable technology project are proved through simulation. The research
provides theoretical principles and practicable references to develop the new generation Chinese geostationary
meteorological satellite.
Yankai Cui andZhigang Wang
"Study on spacecraft motion compensation technology for Chinese geostationary meteorological satellite remote sensing image", Proc. SPIE 6795, Second International Conference on Space Information Technology, 67952B (10 November 2007); https://doi.org/10.1117/12.774213
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Yankai Cui, Zhigang Wang, "Study on spacecraft motion compensation technology for Chinese geostationary meteorological satellite remote sensing image," Proc. SPIE 6795, Second International Conference on Space Information Technology, 67952B (10 November 2007); https://doi.org/10.1117/12.774213