rd, Jan., 2'/> Control Strategy of Lunar Lander-Relay Satellite Antenna Acquisition and Tracking for Chang’e-4 Lunar Exploration Mission
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Control Strategy of Lunar Lander-Relay Satellite Antenna Acquisition and Tracking for Chang’e-4 Lunar Exploration Mission

机译:Chang娥四号探月任务的月球着陆器中继卫星天线获取和跟踪控制策略

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Chang’e-4 lunar lander and "Yutu-2" rover safely landed on the farside of the Moon on 3rd, Jan., 2019. It is the first unmanned spacecraft to softly land on the lunar farside and carried out in-situ and rover exploration there. However, the lunar farside is beyond the communication range of the ground stations on the Earth due to the synchronous rotation of the Moon. Therefore, how to implement reliable relay communication between the Earth and the Moon is crucial for the whole mission. The relay satellite "Queqiao" was launched and is orbiting around the lunar Lagrange point 2 stably for over a year, which is to setup relay communication link between the lunar farside and the Earth. A high-gain antenna (HGA) configured on the lunar lander is utilized in Chang’e-4 lunar mission for transmitting scientific data collected on the lunar farside to the relay satellite and the data is send back to Earth via the relay communication link. Whereas errors such as the positioning and landing attitude error, pointing error of the HGA, timing difference etc. may influence the accuracy of lunar lander-relay satellite antenna acquisition and tracking thus may cause the interruption on communication link. In this paper, based on detailed analysis of the interruption items and uncertainties of HGA pointing, a control strategy of lunar lander-relay satellite HGA acquisition and tracking is proposed for reliable relay communication for Chang’e-4 lunar mission. According to different conditions, strategies of "fast scanning in large-scale" and "slow scanning in small-scale" are designed. Also criterions and basic requirements on the ground for implementation are depicted. Finally, verification results are demonstrated. The control strategy mentioned in this paper is widely used for narrow-beam HGA pointing of lunar exploration mission and is of bright prospect on application for space exploration missions in the coming future.
机译:’娥四号月球着陆器和“玉兔2”号漫游者安全地降落在3月的月球另一端 rd ,2019年1月。这是第一架软着陆在月球远端的无人飞行器,并在那里进行了实地和漫游探测器的探索。但是,由于月球的同步旋转,月球的另一端超出了地球上地面站的通信范围。因此,如何在月球之间实现可靠的中继通信对于整个任务至关重要。中继卫星“ Q桥”已发射,并在拉格朗日2号登月点附近稳定运行了一年以上,目的是在月球远端与地球之间建立中继通信链路。在Chang娥四号的月球任务中使用了配置在月球着陆器上的高增益天线(HGA),用于将在月球远端收集的科学数据传输到中继卫星,然后将数据通过中继通信链路发送回地球。而诸如定位和着陆姿态误差,HGA的指向误差,时间差等误差可能会影响月球着陆器中继卫星天线的获取和跟踪精度,从而可能导致通信链路中断。本文在详细分析了HGA指向的中断项和不确定性的基础上,提出了月球着陆器卫星HGA获取和跟踪的控制策略,以实现Chang娥四号月球任务的可靠中继通信。根据不同的条件,设计了“大规模快速扫描”和“小规模缓慢扫描”的策略。还描述了实地实施的标准和基本要求。最后,证明了验证结果。本文提到的控制策略被广泛应用于月球探测任务的窄波束HGA指向,在未来的太空探测任务中具有广阔的应用前景。

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