| 摘要 |
A method for determining the line of sight of an electro-optical device mounted in a spacecraft such as a satellite. The electro-optical device includes an electo-optical element that detects impinging light energy and produces electrical pulses corresponding to the light energy detected. The method involves providing the electro-optical device with a scan mirror which is rotated to scan space to detect the light produced by a suitably bright star. Once detected, the scan mirror selectively directs the light produced by the detected star toward the electro-optical element which produces electrical pulses in response to the light. A computer on-board the spacecraft then compares the electrical pulses outpputed by the electro-optical device to a predetermined output expected for the star, to determine the line of sight of the electro-optical device.
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