Abstract
The paper is devoted to a particular algorithm of the Earth image edges detennination with respect to creation of the visible range static Earth Horizon Sensor. The possibility of designing the Earth Sensor using given algorithm which has an accuracy of 6 arcmin is confirmed on the basis of computer simulation results. The paper contributes to the progress of attitude sensors and relates to: spacecraft attitude detennination and control; high precision pointing control systems; engineering technology in on-board processing, etc.
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