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DYNAMIC ATTITUDE MEASUREMENT METHOD OF STAR SENSOR BASED ON GYRO'S PRECISE ANGULAR CORRELATION
DYNAMIC ATTITUDE MEASUREMENT METHOD OF STAR SENSOR BASED ON GYRO'S PRECISE ANGULAR CORRELATION
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机译:基于陀螺精确角相关的恒星传感器动态姿态测量方法
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摘要
The disclosure discloses a dynamic attitude measurement method of a star sensor based on gyro's precise angular correlation. On the basis that a dynamic compensation is performed on each of the measurement exposure frames of the star sensor and a fixed star matching vector matrix having dynamic error and noise influence is obtained in a prior art, a transform matrix between every two adjacent measurement frames of the star sensor is precisely measured by a unit including three gyros fixedly coupled with the star sensor. The transform matrix correlates the matched vector matrixes of the adjacent measurement frames of the star sensor. Finally, a correlated measurement equation is established with a series of correlated measurement frames, which is corresponding to processing a series of measurement frames as a single measurement frame.
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