论文标题

用于未来空间重力任务的混合静电 - 原子加速度计

Hybrid electrostatic-atomic accelerometer for future space gravity missions

论文作者

Zahzam, Nassim, Christophe, Bruno, Lebat, Vincent, Hardy, Emilie, Huynh, Phuong-Anh, Marquet, Noémie, Blanchard, Cédric, Bidel, Yannick, Bresson, Alexandre, Abrykosov, Petro, Gruber, Thomas, Pail, Roland, Daras, Ilias, Carraz, Olivier

论文摘要

长期观察地球的重力场具有增强的时间和空间分辨率是未来卫星重力任务的主要目标。提高此类任务中存在的加速度计的性能是探索的主要途径之一。在这种情况下,我们建议研究与最先进的静电加速度计(EA)和基于冷原子干涉法的有希望的量子传感器相关联的混合加速度计的原始概念。为了评估该仪器的性能潜力,已经进行了数值模拟,以确定其在重力场检索期间的影响。利用冷原子干涉仪(CAI)的长期稳定性,已经表明,杂交传感器的漂移减少可能导致重力场检索的改善。然而,一旦考虑到重力场的时间变化和相关的混叠效应,这种收益就会消失。然后需要改进的去敏模型或一些特定的卫星星座,以最大程度地提高加速度计性能增益的影响。为了评估轨道中可实现的加速度性能,已经开发了混合加速度计的数值模拟器,并给出了初步结果。仪器模拟器已通过在地面上运行的混合实验室原型来重现实现的性能来部分验证。卫星旋转影响对CAI的问题也已经通过仪器性能模拟和实验示范进行了研究。已经表明,所提出的配置,其中EA的证明量充当CAI的参考镜,似乎是一种有希望的方法,可以减轻卫星旋转。初步的设计以及初步错误,质量,音量和电力消耗预算。

Long term observation of temporal Earth's gravity field with enhanced temporal and spatial resolution is a major objective for future satellite gravity missions. Improving the performance of the accelerometers present in such missions is one of the main path to explore. In this context, we propose to study an original concept of a hybrid accelerometer associating a state-of-the-art electrostatic accelerometer (EA) and a promising quantum sensor based on cold atom interferometry. To assess the performance potential of such instrument, numerical simulations have been performed to determine its impact in term of gravity field retrieval. Taking advantage of the long term stability of the cold atom interferometer (CAI), it has been shown that the reduced drift of the hybrid sensor could lead to improved gravity field retrieval. Nevertheless this gain vanishes once temporal variations of the gravity field and related aliasing effects are taken into account. Improved de-aliasing models or some specific satellite constellations are then required to maximize the impact of the accelerometer performance gain. To evaluate the achievable acceleration performance in orbit, a numerical simulator of the hybrid accelerometer has been developed and preliminary results are given. The instrument simulator has been in part validated by reproducing the performance achieved with a hybrid lab prototype operating on ground. The problematic of satellite rotation impact on the CAI has been also investigated both with instrument performance simulations and experimental demonstrations. It has been shown that the proposed configuration, where the EA's proof-mass acts as the reference mirror for the CAI, seems a promising approach to allow the mitigation of satellite rotation. A preliminary design has been elaborated along with a preliminary error, mass, volume and electrical power consumption budget.

扫码加入交流群

加入微信交流群

微信交流群二维码

扫码加入学术交流群,获取更多资源