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Astra: Interdisciplinary study on enhancement of the end-to-end accuracy for spacecraft tracking techniques

机译:Astra:关于提高航天器跟踪技术的端到端精度的跨学科研究

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Navigation of deep-space probes is accomplished through a variety of different radio observables, namely Doppler, ranging and Delta-Differential One-Way Ranging (Delta-DOR). The particular mix of observations used for navigation mainly depends on the available onboard radio system, the mission phase and orbit determination requirements. The accuracy of current ESA and NASA tracking systems is at level of 0.1 mm/s at 60 s integration time for Doppler, 1-5 m for ranging and 6-15 nrad for Delta-DOR measurements in a wide range of operational conditions. The ASTRA study, funded under ESA's General Studies Programme (GSP), addresses the ways to improve the end-to-end accuracy of Doppler, ranging and Delta-DOR systems by roughly a factor of 10. The target accuracies were set to 0.01 mm/s at 60 s integration time for Doppler, 20 cm for ranging and 1 nrad for Delta-DOR. The companies and universities that took part in the study were the University of Rome Sapienza, ALMASpace, BAE Systems and Thales Alenia Space Italy. The analysis of an extensive data set of radio-metric observables and dedicated tests of the ground station allowed consolidating the error budget for each measurement technique. The radio-metric data set comprises X/X X/Ka and Ka/Ka range and Doppler observables from the Cassini and Rosetta missions. It includes also measurements from the Advanced Media Calibration System (AMCS) developed by JPL for the radio science experiments of the Cassini mission. The error budget for the three radio-metric observables was consolidated by comparing the statistical properties of the data set with the expected error models. The analysis confirmed the contribution from some error sources, but revealed also some discrepancies and ultimately led to improved error models. The error budget reassessment provides adequate information for building guidelines and strategies to effectively improve the navigation accuracies of future deep space missions. We report both on updated error budget for radio-metric observables and the system configurations proposed for the upgrade of ESA's tracking and orbit determination systems.]
机译:深空探测器的导航是通过多种不同的无线电观测来完成的,即多普勒测距和Delta差分单向测距(Delta-DOR)。用于导航的观测值的特定组合主要取决于可用的机载无线电系统,任务阶段和确定轨道的要求。当前的ESA和NASA跟踪系统的精确度在60 s的多普勒积分时间,在1-5 m的测距和在Delta-DOR测量的6-15 nrad的积分时间下,在各种操作条件下均达到0.1 mm / s的水平。由ESA的常识计划(GSP)资助的ASTRA研究提出了将多普勒,测距和Delta-DOR系统的端到端精度提高大约10倍的方法。目标精度设定为0.01 mm对于多普勒,积分时间为60 s / s,对于测距为20 cm,对于Delta-DOR为1 nrad。参与这项研究的公司和大学是罗马的萨皮恩扎大学,ALMASpace,BAE Systems和意大利的Thales Alenia Space。对大量可测量的辐射测量数据集的分析以及对地面站的专用测试,可以合并每种测量技术的误差预算。辐射度数据集包括X / X X / Ka和Ka / Ka范围以及卡西尼号和罗塞塔任务的多普勒观测值。它还包括JPL为卡西尼号任务的无线电科学实验而开发的高级媒体校准系统(AMCS)的测量结果。通过将数据集的统计属性与预期的误差模型进行比较,可以合并三个辐射度可观测值的误差预算。分析证实了一些错误源的贡献,但也揭示了一些差异,最终导致改进了错误模型。错误预算的重新评估为制定指导方针和策略提供了足够的信息,以有效提高未来深空任务的导航精度。我们既报告了辐射测量可观测物的更新错误预算,也报告了为升级ESA的跟踪和轨道确定系统而建议的系统配置。]

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