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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CHAPTER 1010.1 Communication hardwareThe hardware <strong>for</strong> satellite D-STAR communication has never been built untilnow: it’s <strong>the</strong> main grey area of <strong>the</strong> project. In fact, a traditional D-STARground repeater is composed by a series of boxes with dimension and massdefinitely incompatible with a <strong>CubeSat</strong>: everything has to be reduced at mostand some functionalities will be cut out.We are not going to give detailed in<strong>for</strong>mation on <strong>the</strong> subject as it’s part of ano<strong>the</strong>r <strong>the</strong>sis on <strong>OUFTI</strong>-1 [RD5]. Anyway a brief introduction of <strong>the</strong> hardwareis almost compulsory.The system is shown in block diagram in figure 10.1Figure 10.1: Communication system block diagramThe signal at 145 MHz frequency is received, amplified and demodulated.Voice and data stream are <strong>the</strong>n separated. The low rate stream is <strong>the</strong>n searched<strong>for</strong> command packages and, if any, <strong>the</strong>y are analyzed, verified as originating from<strong>the</strong> Reference Control Station and <strong>the</strong>n processed if suitable. In this case, downlinkdata are fitted with requested telemetry in<strong>for</strong>mation. O<strong>the</strong>rwise, receivedlow rate user’s data are recombined without additional delay with <strong>the</strong> receivedvoice stream, modulated, amplified and sent back immediately via <strong>the</strong> downlinkpath at 435 MHz frequency.The mode of operation is a voice based system called DV mode: it runs at4800 bds, 0.5 GMSK modulated. It is made by 3600 bds AMBE encoded voicestream (2400 bds voice + 1200 bds FEC) and a low speed uncorrected dataGalli Stefania 98 University of Liège