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ECE 5233 Satellite Communications
Prepared by: Dr. Ivica Kostanic Lecture 17: Multiple Access Schemes (2) (Section 6.2 and 6.3 ) Spring 2014
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Outline IM in FDMA Calculation of C/N with IM TDMA
Important note: Slides present summary of the results. Detailed derivations are given in notes.
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IM products between wideband signals
Satellite signals are broadband IM distortion is wideband as well As the amplifier is driven into saturation distortion components grow faster (3dB for 1dB) When there are more than two signals, there are many IM components IM distortion raises the noise floor for the satellite signals Spectrum analyzer plot for showing IM distortion with 3 signals Note: IM distortion is mitigated by forcing the operation in the linear part of the PA (back off) IM distortion spectrum for 2 wideband signals
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C/N calculation with IM
Path through transponder – another link degrading C/N The overall C/N has three components (uplink, downlink and transponder) The overall performance is limited by the smallest of the three Optimum reached when all of them are the same Change of C/N at the output as a function of input power Note: In practice analysis of IM becomes complex and tools are used to determine optimum operation of the transponder
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Examples Intermodulation example (page 228) Example 6.2.1
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Illustration of TDMA principle
Signals from various earth stations are interlaced in time Each signal uses the entire transponder bandwidth – no IM Modulation must be digital to accommodate intermittent nature of transmission Signals are wideband – not well suited for large number of narrowband signals Transmission of the earth stations must be synchronized Each earth station transmits one burst per frame Duration of frame from 125us to few ms Earth station received all the transmissions and just de-multiplexes the desired one – issue of synchronization Illustration of TDMA principle
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Burst formation for an individual earth station
TDMA burst generation TDMA satellite access works well with landline TDMA systems Rate adjustment accomplished through buffering Burst of a satellite earth station consists of preamble (overhead) and user data Preamble – contains data necessary for system operation (synchronization and signaling) User data - payload Burst formation for an individual earth station Note: Data rate on the satellite link is much larger than data rate of incoming streams
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Example of frame structure for INTELSAT/EUTELSAT
TDMA frame structure Bursts are organized into frames Guard times are inserted between burst – ensures that there is no overlap between bursts One earth station - in charge of providing reference burst (no user data) Traffic burst – carries user data Longer frames – less overhead Example of frame structure for INTELSAT/EUTELSAT
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Example of the burst reception process
On the downlink each station receives all the bursts in the frame Beginning of the frame – reference burst Beginning of the burst – preamble Synchronization with the burst – unique word Each station extract the portion of the burst Data received discontinuously – to provide rate matching there is a buffer at the receiver Example of the burst reception process
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Example Example 6.3.1
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