Please use this identifier to cite or link to this item:
https://er.nau.edu.ua/handle/NAU/22447
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DC Field | Value | Language |
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dc.contributor.author | Kharchenko, Volodymir | - |
dc.contributor.author | Barabanov, Yurii | - |
dc.contributor.author | Grekhov, Andrii | - |
dc.date.accessioned | 2016-09-28T09:55:49Z | - |
dc.date.available | 2016-09-28T09:55:49Z | - |
dc.date.issued | 2013 | - |
dc.identifier.other | №4 | - |
dc.identifier.other | P. 361–367 | - |
dc.identifier.uri | http://er.nau.edu.ua/handle/NAU/22447 | - |
dc.description | MODELING OF “SATELLITE-TO-AIRCRAFT” LINKFOR SELF-SEPARATION / Volodymir Kharchenko, Yurii Barabanov, Andrii Grekhov // Transport. – 2013. – V.28. – №4. – P. 361–367. | uk_UA |
dc.description.abstract | 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. | uk_UA |
dc.language.iso | en | uk_UA |
dc.publisher | Transport | uk_UA |
dc.relation.ispartofseries | ;V.28 | - |
dc.relation.ispartofseries | ;№4 | - |
dc.subject | free-flight | uk_UA |
dc.subject | self-separation | uk_UA |
dc.subject | ADS-B | uk_UA |
dc.subject | BER | uk_UA |
dc.subject | communication channel | uk_UA |
dc.subject | aircraft | uk_UA |
dc.subject | satellite | uk_UA |
dc.subject | convolutional encoder | uk_UA |
dc.subject | BPSK | uk_UA |
dc.subject | free space loss | uk_UA |
dc.subject | phase/frequency offset | uk_UA |
dc.subject | memoryless nonlinearity | uk_UA |
dc.subject | phase noise | uk_UA |
dc.subject | Viterbi decoder | uk_UA |
dc.subject | amplifier backoff level | uk_UA |
dc.subject | noise temperature | uk_UA |
dc.subject | antenna diameter | uk_UA |
dc.title | MODELING OF “SATELLITE-TO-AIRCRAFT” LINKFOR SELF-SEPARATION | uk_UA |
dc.type | Article | uk_UA |
Appears in Collections: | Наукові праці співробітників НАУ (проводиться премодерація, колекція НТБ НАУ) |
Files in This Item:
File | Description | Size | Format | |
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TRANSPORT_Kharchenko_Barabanov_Grekhov.docx | стаття, подана у видавництво | 782 kB | Microsoft Word XML | View/Open |
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