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“鹊桥二号”中继星测控系统设计与验证

Design and Verification of TT&C System for Queqiao-2 Relay Satellite

  • 摘要: 针对地面站无法对月球背面或极区等探测器直接测量的情况,以及在现有测控体制和地月距离下难以提升遥测速率和测量精度的情况下,“鹊桥二号”中继星测控系统设计了地−星−器−星−地四程测量链路实现地面站对月球不可见探测器的实时测量,以及进行高斯滤波最小频移键控(Gaussian Minimum Shift Keying,GMSK) + 伪随机码(Pseudo-random Noise,PN)体制测控体制验证。“鹊桥二号”中继星发射以来测控系统长期稳定执行测控通信任务,四程测量仿真结果证明能实现对着陆器的米级定位精度,采用GMSK +PN测控体制在地月距离下经计算能够实现厘米级的测距精度。上述工作情况及仿真验证结果表明“鹊桥二号”中继星测控系统方案满足测控任务需求,可为后续深空探测和探月任务测控系统设计提供参考。

     

    Abstract: Based on the situations where ground stations can’t directly measure hunar far-side or polar regions, and where current tracking and control systems face limitations in improving telemetry rates and measurement accuracy dueto the Earth-Moon distance, the Queqiao-2 relay satellite’s TT&C system is designed to achieve a four-way measurement chain-Earth-satellite-probe-satellite-Earth-enabling real-time tracking and measurement of lunar spacecraft that are not directly visible from Earth. Additionally this system serves to validate a GMSK+PN-based tracking and control communication scheme. Since the in-orbit launch of the Queqiao-2 relay satellite, the TT&C syatem has consistently and stably perfomed TT&C tasks. Simulation results of the four-way meaurement demonstrate that it can achieve meter-level positioning accuracy for the lander. Calculation of the new TT&C scheme indicates that it can achieve centineter-level ranging accuracy at the Earth-Moon distance. The actual operational perfomance and simulation verification results demonstrate that the Queqiao-2 relay satellite’s TT&C system design meets the mission requirements and can provide reference for the design of TT&C systems for future deep space exploration and lunar exploration missions.

     

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