Наукові праці співробітників НАУ (проводиться премодерація, колекція НТБ НАУ)

Permanent URI for this collectionhttp://er.nau.edu.ua/handle/NAU/9209

Зібрання містить наукові праці співробітників НАУ, що з різних причин не війшли до зібрань структурних підрозділів НАУ.

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Browsing Наукові праці співробітників НАУ (проводиться премодерація, колекція НТБ НАУ) by Author "Barabanov, Yurii"

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    MODELING OF “SATELLITE-TO-AIRCRAFT” LINKFOR SELF-SEPARATION
    (Transport, 2013) Kharchenko, Volodymir; Barabanov, Yurii; Grekhov, Andrii
    For modelling of data transmissionfrom low-orbit satellite constellation Іrіdіum the original model of a communication channel "Satellite-to-Aircraft" was built using MATLABSіmulіnk.The model comprises “Satellite Downlink Transmitter” (Bernoulli Random Binary Generator, Convolutional Encoder, BPSK Baseband Modulator, High Power Amplifier with a memoryless nonlinearity, Satellite Phase Noise, Transmitter Dish Antenna Gain), “Downlink Path” (Free Space Path Loss, Phase/Frequency Offset), “Aircraft Downlink Receiver” (Receiver Dish Antenna Gain, Aircraft Receiver System Temperature, Viterbi Decoder), “Error Rate Calculation” block and “Display”.Modeling was realized without and with convolutional coding (r=3/4, K=7) at different noise temperatures and free space losses. Dependencies of a Bit Error Rate on free space path losses, antennas diameter, phase/frequency offsets, satellite high power amplifier backoff level, and phase noise were received and analyzed.
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    MODELING OF ADS-B DATA TRANSMISSION VIA SATELLITE
    (Aviation, 2013) Kharchenko, Volodymyr; Barabanov, Yurii; Grekhov, Andrii; Харченко, Володимир Петрович
    For modelling of ADS-B messages transmissionvia low-orbit satellite constellation Іrіdіum the original model of a communication channel "Aircraft-to-Satellite-to-Ground Station" was built using MATLABSіmulіnk.The model comprises “Aircraft Uplink Transmitter” (Bernoulli Random Binary Generator, Convolutional Encoder, BPSK Baseband Modulator, High Power Amplifier with a memoryless nonlinearity, Transmitter Dish Antenna Gain), “Uplink Path” (Free Space Path Loss, Phase/Frequency Offset), “Satellite Transponder” (Receiver Dish Antenna Gain, Satellite Receiver System Temperature, Complex Baseband Amplifier, Phase Noise, Transmitter Dish Antenna Gain), “Downlink Path” (Free Space Path Loss, Phase/Frequency Offset), “Ground Station Downlink Receiver” (Receiver Dish Antenna Gain, Ground Receiver System Temperature, Viterbi Decoder), “Error Rate Calculation” block and “Display”.Modeling was realized without and with convolutional coding (r=3/4, K=7) at different noise temperatures and free space losses. Dependencies of a Bit Error Rate on free space path losses, antennas diameter, phase/frequency offsets, satellite transponder linear gain, aircraft and satellite transponder high power amplifier backoff level, and phase noise were received and analyzed.