satelliteCNR
The ratio of carrier to noise for the specified parameters of the satellite communication budget.
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Syntax
Function call
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cn,info = satelliteCNR(cfg)— calculates the ratio of the carrier frequency signal to noise (Carrier-to-Noise Ratio, CNR)cnfor the satellite communication budget parameters specified in the configurationcfg. The function also returns the intermediate results of the CNR calculation in the output argument.infobased on the parameters of the communication channel budget specified in the input argumentcfg.
Arguments
Input arguments
# cfg — CNR configuration object
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the Satellites CNRCONFIG object
Details
The CNR configuration object, set as an object EngeeSatellites.SatelliteCNRConfig.
Output arguments
# cn is the ratio of carrier to noise
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scalar
Details
The ratio of the carrier frequency signal to noise, returned as a scalar in dB. For more information, see Algorithms.
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# info — intermediate results of CNR calculation
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structure
Details
Intermediate results of the CNR calculation based on the parameters of the communication channel budget specified in the argument cfg, and returned as a structure with the following fields.
| Structure Field | Description |
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The effective isotropic radiated power of the transmitting antenna, returned as a scalar in dBW. |
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The loss in free space from the transmitting to the receiving antenna, returned as a scalar in dB. |
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The received isotropic power at the receiving antenna, returned as a scalar in dBW. |
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The ratio of the carrier power density to the noise power density, returned as a scalar in dB Hz. |
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The ratio of energy per bit to the noise power density, returned as a scalar in dB. |
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The ratio of energy per symbol to the noise power density, returned as a scalar in dB. |
All fields in the structure have a data type Float64. For more information, see Algorithms.
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Examples
Calculation of the carrier/noise ratio and energy reserve
Details
Let’s calculate the carrier/noise ratio and the energy reserve of the communication line for the specified parameters of the satellite communications budget.
Create a CNR configuration object with the default properties, and then change these properties.
import EngeeSatellites: SatelliteCNRConfig
cfg = SatelliteCNRConfig()
cfg.TransmitterPower = 17 # дБВт
cfg.TransmitterSystemLoss = 9 # дБ
cfg.TransmitterAntennaGain = 38 # дБи
cfg.Distance = 40215 # км
cfg.Frequency = 11 # ГГц
# В данном случае к прочим потерям относятся, соответственно, потеря
# поляризации, помехи и потери, связанные с неправильным направлением антенны.
polLoss = 3.0103
intLoss = 2
antLoss = 1
cfg.MiscellaneousLoss = polLoss + intLoss + antLoss # дБ
cfg.GainToNoiseTemperatureRatio = 25 # дБ/К
cfg.ReceiverSystemLoss = 2 # дБ
cfg.BitRate = 10 # Мбит/с
Let’s output the properties of the CNR configuration object.
show(cfg)
SatelliteCNRConfig:
TransmitterPower=17
TransmitterSystemLoss=9
TransmitterAntennaGain=38
Distance=40215
Frequency=11
MiscellaneousLoss=6.0103
GainToNoiseTemperatureRatio=25
ReceiverSystemLoss=2
BitRate=10
SymbolRate=10
Bandwidth=6
Calculate the carrier/noise ratio.
import EngeeSatellites.Functions: satelliteCNR
cn, info = satelliteCNR(cfg)
println("\ncn = ", cn, "\ninfo: ",
"\n\tTransmitterEIRP = ", info.TransmitterEIRP,
"\n\tFSPL = ", info.FSPL,
"\n\tReceivedIsotropicPower = ", info.ReceivedIsotropicPower,
"\n\tCarrierToNoiseDensityRatio = ", info.CarrierToNoiseDensityRatio,
"\n\tReceivedEbNo = ", info.ReceivedEbNo,
"\n\tReceivedEsNo = ", info.ReceivedEsNo)
cn = 18.44395628356213
info:
TransmitterEIRP = 46
FSPL = 205.3633983858191
ReceivedIsotropicPower = -165.3736983858191
CarrierToNoiseDensityRatio = 86.22546878739857
ReceivedEbNo = 16.22546878739857
ReceivedEsNo = 16.22546878739857
Calculate the supply of the communication line. Assume that the required ratio of energy per bit to noise power density (Eb/No) is 10 dB, and the loss during implementation in the receiver — 2 dB.
reqEbNo = 10
implLoss = 2
margin = info.ReceivedEbNo - reqEbNo - implLoss
println("margin = ", margin)
margin = 4.225468787398569
Algorithms
The carrier-to-noise ratio (CNR) in a satellite communication system measures the power of the carrier signal at a receiver relative to the noise power at the same receiver. The following diagram shows the various signal losses and amplifications that occur in satellite communications.
To calculate the carrier/noise ratio cn for the system, the function satelliteCNR performs various intermediate calculations using the properties of the configuration object EngeeSatellites.SatelliteCNRConfig, and outputs them to the structure info. The function uses these formulas for intermediate calculations.
Structure Field info |
Formula |
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The function then calculates the carrier-to-noise ratio using the formula
cn = CarrierToNoiseDensityRatio − 10 * log10(Bandwidth) − 60.