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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: “鹊桥二号”中继星测控系统作为中继节点可实现地面站对月球探测器的测定轨,在现有测控体制和地月距离情形下,难以提升遥测速率和测量精度,需重新设计并进行深空环境的测控体制验证,采用S频段统一载波体制实现星地常规测控任务,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,并配置高斯滤波最小频移键控(Gaussian Minimum-Shift Keying,GMSK) + 伪随机码(Pseudo Number,PN)测控体制应答机对其进行应用验证。月球四程测量仿真和试验结果表明测控新体制不仅可实现对探测器的米级定位精度,还能实现地月距离厘米级的测距精度。在轨工作情况表明中继星测控系统方案满足了测控任务指标需求,为后续探月工程任务测控系统和深空测控系统设计提供了参考。

     

    Abstract: Queqiao-2 relay satellite’s TT&C system can act as a relay node to enable the ground station to perform orbit determination of the lunar probe. Under the existing T&C system and the Earth-Moon distance, it is difficult to improve the telemetry rate and measurement accuracy. Therefore, it is necessary to design and verify a new TT&C system under deep-space conditions. A unified S-band carrier system was adopted to perform routine TT&C tasks between the satellite and the ground station. A four-way measurement link(ground station-satellite-probe-satellite-ground station)was designed to enable real-time measurement of lunar probes that are not visible from the ground station. Additionally, a GMSK + PN TT&C transponder was configured for application verification. Simulation results of the four-way lunar measurement demonstrate that it can achieve meter-level positioning accuracy for the lander. Estimations of the new TT&C system indicate that it can achieve centimeter-level ranging accuracy at the Earth-Moon distance. The actual operational performance and simulation verification results demonstrates that the TT&C system design of the relay satellite meets the mission requirements and can provide references for the design of TT&C systems for future deep space exploration and lunar exploration missions.

     

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