In order to solve the single degree of freedom solar panels tilted orbits in the general limitations of the problem of orientation, a common approach is to provide support for satellite attitude adjustment. For earth observation satellites, satellite attitude generally only required to keep pointing to the ground to make the payload, ie the satellite pitch angle and roll angle is limited and yaw angle of the satellite is not required. Therefore, the satellite yaw angle can be adjusted to assist the solar panels of orientation.

Solar panels day orientation program.doc

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