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The athermalization design of an airborne all-day star sensor optical system

机译:机载全日星传感器光学系统的热化设计

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With the continuous development of navigation technology, celestial navigation system has gradually become the essential of celestial navigation system with its advantages of autonomy is strong, good concealment and high precision. The key component of the astronomical navigation system is the all-day star sensor. With the improvement of navigation accuracy, higher requirements have been put forward for the design of all-day star sensor, which is required to be able to work normally within 24 hours. The temperature range of the star sensor working on the airborne platform is very wide, and the temperature has a great impact on the imaging performance of the star sensor, thus affecting the positioning accuracy of navigation. Therefore, it is of great practical significance to ensure that its optical performance does not change within such a wide range of temperature, so as to significantly improve its navigation and positioning accuracy.
机译:随着导航技术的不断发展,天体导航系统逐渐成为天主教的必要条件,其自主权具有强大,隐藏性良好,精度高。天文导航系统的关键组成部分是全天的星传感器。随着导航精度的提高,全天星传感器的设计提出了更高的要求,这是必须在24小时内正常工作。在机载平台上工作的星传感器的温度范围非常宽,温度对星传感器的成像性能产生了很大影响,从而影响了导航的定位精度。因此,确保其光学性能在如此宽范围内的光学性能不变,以显着提高其导航和定位精度。

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