SEDSAT-2 Communications Design Notes 20080220

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Subsystem Notes as of SEDSIC '07

(Assumption: Satellite will be in Low Earth Orbit)

  • Frequency range (we’re using 420 MHz)
    • UHF (300 MHz – 3 GHz)
    • Availability of equipment (transmitter/receiver)
    • Smaller antenna structure
  • Modulation
    • Phase Shift-Keying
      • DPSK, a variation that is simpler to implement, but produces erroneous demodulations
      • QPSK
      • BPSK
        • Transmission bit rate is higher
        • Lower bandwidth
    • Frequency Shift-Keying
      • High power, high spectral efficiency (?)
      • High bandwidth
      • Extensively used by most CubeSats
      • Availability of equipment
      • Slower in transmission.
      • Reception setup is simpler
      • FSK is more power efficient
    • Amplitude Shift-Keying
      • linear and sensitive to atmospheric noise, distortions, propagation conditions on different route
      • requires excessive band-width, waste of power
      • modulation and demodulation is relatively inexpensive
      • used for digital data transfer over optical fiber
        • look into redundancy systems
        • Doppler effect
  • Antenna
    • Dipole
    • Bi-directional
      • Lower gain than the other two (1.64)
      • Smaller volume – one element
      • Simple to design
      • Seems to be best option
    • Log-Periodic Antenna
      • Lower in gain
      • Broad bandwidth
      • More space
      • More mass
  • Transceiver – Transmitter / Receiver
    • Weight
    • Link budget
    • Power budget, frequency, Antenna gain
  • Terminal Node Controller (TNC)
    • Which component to use.
    • What are the parameters? Weight, power, volume
  • Amplifier
    • Which component to use.
    • What are the parameters? Weight, power, volume
    • Necessity
      • Not very necessary
      • Power drain
      • Batteries will need to be bigger/heavier
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