| 摘要 |
The sun search method for a satellite stabilized in three axes according to the invention uses a sun sensor device with a visual field possibly containing gaps, and a rotational speed gyro which measures in a measuring axis that is oriented arbitrarily. A regulating law with the form +E,uns tau +EE =-k+E,uns GGT+EE omega is used (+E,uns tau +EE =regulating torque, k=amplification factor, +E,uns G+EE =directional vector of measuring axis of rotational speed gyro, +E,uns omega +EE =rotational speed vector of the satellite). A rotational wheel momentum +E,uns H+EE which is not parallel to the measuring axis, is generated with the aid of an additional flywheel device.
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