Deep Space Receiver for Cassini-Huygens Radio Link

G. Boscagli, M. Comparini
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引用次数: 5

Abstract

The CASSLNI-HUYGENS mission is a deep space mission for the exploration and the study of the atmosphere of Titan. The combined Orbiter-Probe spacecraft will reach the Saturn system about 8.5 years after the launch. At that time the Probe will be separated and its mission will start transmitting scientific and housekeeping data during the descent phase to the surface of Titan via S-band radio relay link. The Probe Data Relay Link is composed by the Probe Transmitter Terminal (PTT), on Huygens spacecraft, and the Orbiter Receiving Terminal (ORT), on Cassini spacecraft. The PTT includes two chains which tranrsmit the phase modulated carriers at two different frequencies with opposite circular polarizations. On the orbiter the two signals are discriminated and separately amplified by the LNAs. The receivers acquire and synchronize the carter and subcarrier and provide the data demodulation and decoding. Major requirements of the deep space receivers are fast signal acquisition and demodulation capability at very low C/No. The paper describes the Orbiter Receiver architecture underlying the advantages of a fully digital approach.
卡西尼-惠更斯无线电链路的深空接收器
casslni -惠更斯任务是一项深空任务,用于探索和研究土卫六的大气。轨道探测器联合航天器将在发射后大约8.5年到达土星系统。届时,探测器将被分离,其任务将开始在下降阶段通过s波段无线电中继链路向土卫六表面传输科学和家政数据。探测器数据中继链路由惠更斯号航天器上的探测器发射终端(PTT)和卡西尼号航天器上的轨道器接收终端(ORT)组成。PTT包括两条链,这两条链以两个不同的频率以相反的圆极化传输相位调制载波。在轨道飞行器上,这两个信号分别由lna进行区分和放大。接收机采集和同步载波和子载波,并提供数据解调和解码。深空接收机的主要要求是在极低的C/No下的快速信号采集和解调能力。本文描述了基于全数字化方法优势的轨道接收器架构。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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