立方体结构卫星s波段收发器设计

Tung The-Lam Nguyen, N. K. Kiem, S. Ta, Van Cuong Nguyen, Anh Duc Tran, Thanh Nam Le, Chien Ngoc Dao
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引用次数: 0

摘要

由于功率和尺寸有限,以及收发器成本低,立方体卫星结构卫星的通信能力有限。因此,立方体卫星与地面站之间的通信面临着许多风险,例如削弱收发器性能和降低任务数据吞吐量。本文提出了一种用于卫星遥测、跟踪和控制的s波段收发器的设计方案。该收发器可提供96kbps的测量数据速率,最大输出功率为39.3 dBm (8.5 W),总体体积为87.4 93.4 20 mm3,包括铝外壳在内总质量为252克。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design of S-Band Transceiver for CubeSat Structure Satellites
CubeSat structure satellites have limited communication ability as a result of limited power and size, as well as low cost transceivers. The communication between CubeSat and the Earth station therefore faces a lot of risks such as impairing transceiver performance and degrading mission data throughput. In this paper, a design of S-band transceiver for telemetry, tracking and control (TT&C) is presented for use onboard CubeSat satellites. The transceiver can provide a measured 96 Kbps of data rate with maximum output power of 39.3 dBm (8.5 W) and an overall volume of 87.4 93.4 20 mm3 with total mass of 252 grams including aluminum housing.
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