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Method and device for correcting the thermoelastic effects, notably for a space telescope and telescope comprising such a device
Method and device for correcting the thermoelastic effects, notably for a space telescope and telescope comprising such a device
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机译:用于校正热弹性效应的方法和设备,特别是用于太空望远镜的热弹性效应和包括该设备的望远镜
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摘要
The method involves determining a prior correction of thermoelastic effects by using a prior model (26) i.e. periodic predictive model, of variations of the thermoelastic effects on an orbital scale and an algorithm (25) for determining correction fed by programming data (41) of a space satellite prior to flight of the satellite. Control messages of a correction unit (30) are established for correcting the performance parameters of a telescope (1) based on the determined correction in the flight state, where the performance parameters comprise stability of a line of sight of the telescope. An independent claim is also included for a correction device for correcting thermoelastic effects on performance parameters of a telescope on board a space satellite.
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