中山大学纳米卫星星载通信子系统

B. Sheela Rani, E. Logashanmugam, S. Rajarajan, M. Sugadev, G. Jegan, N. Jagadhish Kumar, N. Jeevan Kumar
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引用次数: 5

摘要

任何卫星的通信子系统的主要目标是在卫星和地面站之间建立通信链路,以中继有效载荷和管理数据本文讨论了Sathyabama纳米卫星通信子系统硬件和软件设计的各个方面。本设计选用的硬件设备包括Microhard MHX-425超低功耗FHSS无线电收发器、Beacon发射机、Microchip dsPIC板载处理器和单极天线。为dsPIC处理器编写的软件负责将遥测和有效载荷信息编码为标准AX.25格式数据包以及解码从地面站传输的命令。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
On board communication subsystem for Sathyabama University nano-satellite
The primary goal of the communication subsystem of any satellite is to establish a communication link between the satellite and the ground station to relay payload and housekeeping data.[1] In this paper, various hardware and software design aspects of the Sathyabama nanosatellite communication subsystem is discussed. Hardware devices chosen for our design includes Microhard MHX-425 ultra low power FHSS radio transceiver, Beacon transmitter, Microchip dsPIC on board processor and monopole antennas. The software written for the dsPIC processor is responsible for encoding telemetry and payload information into standard AX.25 format data packets as well as decoding commands transmitted from the ground station.
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