SpaceNaute®:先进空间发射器惯性参考系统的HRG技术突破

F. Delhaye, J. Girault
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引用次数: 6

摘要

空间发射方要求稳定、高精度的惯性控制系统来将卫星精确地送入轨道,特别是当目标是超同步椭圆地球静止转移轨道时。作为欧洲惯性导航领域的领导者,赛峰电子与防务公司掌握了所有惯性技术(环形激光陀螺、光纤陀螺和半球谐振器陀螺)。在阿丽亚娜6开发准备的框架内,权衡分析提供最先进的空间发射INS导致基于HRG技术的SpaceNaute®惯性参考。在欧洲航天局(ESA)的监督下,ArianeGroup进行了深入的选择过程,SpaceNaute®从竞争对手提出的基于RLG和FOG的解决方案中脱颖而出。本文介绍了SpaceNaute®独特的SWaP(尺寸、重量和功率)突破,揭示了SpaceNaute®所选惯性传感器的关键性能特征,以及如何将HRG优势融入到产品中。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
SpaceNaute®: HRG technological breakthrough for advanced space launcher inertial reference system
Space launchers are demanding robust and highly accurate INS to stage or inject satellites precisely into orbit, especially when the goal is the supersynchronous elliptical geostationary transfer orbit. As European leader of inertial navigation, Safran Electronics & Defense masters all inertial technologies (Ring Laser Gyro, Fiber Optic Gyro and Hemispherical Resonator Gyro). In the frame of the preparation of the Ariane 6 development, a trade-off analysis to offer the most advanced Space Launcher INS lead to the SpaceNaute® inertial reference based on the HRG technology. After a deep selection process conducted by ArianeGroup under European Space Agency (ESA) supervision, SpaceNaute® was selected against RLG and FOG based solutions proposed by the competitors. This paper describes the unique SWaP (Size, Weight and Power) breakthrough of SpaceNaute®, unveils key performance characteristics of the selected inertial sensors for SpaceNaute® and how HRG benefits are capitalized into the product.
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