Mission Design for the CubeSat OUFTI-1
Mission Design for the CubeSat OUFTI-1
Mission Design for the CubeSat OUFTI-1
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CHAPTER10COMMUNICATION SYSTEMThe communication system is <strong>the</strong> interface between <strong>the</strong> satellite and <strong>the</strong> earth.If in <strong>the</strong> case of OUTI-1 it also represents <strong>the</strong> payload, <strong>for</strong> <strong>the</strong> next missions ofLEODIUM Project it will be just a mean to be in contact with <strong>the</strong> spacecraft.The D-STAR system is used as main communication tool to send command,both <strong>for</strong> <strong>the</strong> satellite and <strong>for</strong> <strong>the</strong> future payloads, and to receive telemetry andpayload’s results. Given that D-STAR is an amateur-radio protocol, we planto make our <strong>CubeSat</strong> available to <strong>the</strong> ham-radio community when <strong>the</strong> radiolink is not used <strong>for</strong> command and telemetry. Fur<strong>the</strong>rmore, we plan to getspontaneous help from <strong>the</strong> worldwide amateur-radio community to keep an eyeon our satellite when it is not within sight of our ground station.Aware of <strong>the</strong> fact that a D-STAR has never flown into space, we cannot take<strong>for</strong> granted that everything will go fine, especially considering <strong>the</strong> fight loadsat launch and <strong>the</strong> radiation environment in orbit. Fur<strong>the</strong>rmore, if somethingfails just after launch, we strongly desire to be able to assess what happenedwith <strong>the</strong> satellite. There<strong>for</strong>e, we will place a backup command and telemetrysystem based on a CW beacon. Probably always switch on, it will be able tosend minimum housekeeping and to receive some commands.97