首页> 外文会议>International Astronautical Congress >SPACE EXPLORATION SYMPOSIUM (A3) Moon Exploration - Poster session (2D):DESCRIPTION AND SIMULATION RESULTS FOR A GNSS SIGNAL-BASED NAVIGATION SYSTEM FOR A MISSION TO THE MOON
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SPACE EXPLORATION SYMPOSIUM (A3) Moon Exploration - Poster session (2D):DESCRIPTION AND SIMULATION RESULTS FOR A GNSS SIGNAL-BASED NAVIGATION SYSTEM FOR A MISSION TO THE MOON

机译:太空勘探研讨会(A3)月亮探索 - 海报会话(2D):基于GNSS信号的导航系统的描述和仿真结果为月球

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In the frame of an ESA activity, the objective of the Moon-GNSS study has been to determine the feasibility using weak-signal GNSS (GPS/Galileo) technology in future lunar exploration missions,to improve the navigation performance in terms of accuracy, cost reduction, robustness and autonomy. During the Moon-GNSS activity, the analysis and the identification of the navigation receiver requirements for the upcoming lunar exploration missions have been performed. An extensive simulation campaign has been carried out to assess the achievable performance (signal acquisition and tracking, raw data accuracy,navigation accuracy and robustness) and to provide with the due inputs for the derivation of the Moon-GNSS navigation receiver requirements. The architecture of the GNSS receiver module has been proposed and designed to achieve the low levels of sensitivity required. It is based on the ESA patented "Double-FFT Method" for an efficient implementation of the high-sensitivity processing. Besides, the synergies between GNSS signal/navigation processing and other navigation sensors have been analyzed, using the state of the art of sensors integration for space missions. A Proof-of-Concept demonstrator of the weak-signal Moon-GNSS navigation has been designed and implemented, showing the main functional and performance capabilities of the Moon-GNSS receiver. A test campaign representative of a real Moon-GNSS mission has been performed, covering all the mission phases representative of the real mission conditions in terms of dynamics and signal disturbances. The main conclusions are that a specifically designed GNSS receiver should be capable of receiving and processing GNSS signals coming from Earth during a lunar mission,and that the resulting GNSS measurements can be hybridized with other navigation sensors to improve the standard navigation performances. Furthermore, GNSS stand-alone navigation should be possible in some phases, allowing a dramatic reduction of the frequency of ground operations. A possible roadmap to eventually bring the Moon-GNSS navigation system into an operational status has been proposed and will be presented.
机译:在ESA活动的框架中,Moon-GNSS研究的目的是通过在未来的月球勘探任务中确定使用弱信号GNSS(GPS / GALILEO)技术的可行性,以提高准确性,成本方面的导航性能减少,鲁棒性和自主权。在月亮-GNSS活动期间,已经进行了分析和识别即将到来的月球勘探任务的导航接收机要求。已经进行了广泛的仿真活动,以评估可实现的性能(信号采集和跟踪,原始数据准确性,导航准确性和稳健性),并提供了用于Moon-GNSS导航接收器要求的推导的由于的由于的输入。 GNSS接收器模块的架构已经提出并设计以实现所需的低级别的灵敏度。它基于ESA专利的“双FFT方法”,用于高灵敏度处理的有效实现。此外,已经分析了GNSS信号/导航处理与其他导航传感器之间的协同作用,使用传感器的状态集成空间任务。设计并实施了弱信号Moon-GNSS导航的概念证明,展示了Moon-GNSS接收器的主要功能和性能和性能。已经进行了代表真正的月亮GNSS任务的测试活动,涵盖了代表动态和信号扰动方面的真正任务条件的所有任务阶段。主要结论是,专门设计的GNSS接收器应该能够在月球任务期间接收和处理来自地球的GNSS信号,并且所产生的GNSS测量可以与其他导航传感器杂交以改善标准导航性能。此外,GNSS独立导航应在某些阶段中进行,允许急剧降低地面操作的频率。最终将月亮GNSS导航系统提出并将呈现可能的路线图,并将呈现成功状态。

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