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Link Budget and Satcoms Training
Introduction
The aim of this presentation is to provide an overview of the considerations necessary when calculating a satellite link budget.
INVSAT as a VSAT provider must implement solutions ensuring link budget integrity, whilst maintaining simple and inexpensive solutions where possible.
The link budget, no matter what part of the world the system is operating in, is driven by hardware performance, as well as atmospheric effects. The four main contributions from hardware to the overall performance are:
Satellite performance
Antenna performance
MODEM performance
HPA performance
The satellite performance is out of our hands, so it up to us to identify satellites with a suitable footprint for a required link and choose the appropriate provider based on cost and performance. Once a satellite has been identified a link budget calculation can be performed.
Introduction
There are often constraints on the size of antennas that can be deployed at a given site. For VSAT applications cost, mobility, type approval, location and appearance often feature in antenna choice.
In order for a satellite link to be maintained the MODEMS must ‘keep lock’. MODEM manufacturers specify signal strength, required to ‘keep lock’, in terms of power received as a carrier or error to noise ratio.
VSAT HPAs are sized in order to achieve a given performance (Eb/No). For VSAT applications solid state parametric amplifiers, SSPAs, are used to provide efficient , reliable, low cost amplification.
When performing a link budget calculation it is often necessary to trade performance, with antenna size or HPA size. The aim being to provide a reliable, compliant low cost solution.
UNITS
Link budget calculations express power in dBW
1W = 0dBW
2W = 3 dBW
10W = 10dBW
100W = 20dBW
1000W = 30dBW
x W = 10*log(x/1) dBW
x dBW = 10x/10 W
Noise calculations use both noise temperatures and noise figure
Noise Temperature = 290(10NF/10 - 1)
Antennas
Invsat 2400SE - C Band
Invsat 1200SE - Ku Band
Antenna Gain
The gain of an antenna is the ratio of power radiated (or received) by an antenna per unit solid angle in a given direction to the power radiated (or received) by an isotropic antenna (radiates evenly an all directions) fed with the same power
The gain is maximum in the direction of peak radiation (antenna boresight) and has a value expressed as:
Gmax = (4πD / λ2)Aeff
Aeff is the equivalent electromagnetic surface area of the antenna. For circular aperture antennas of diameter, D, A= πD2/4
Aeff= ηA, where η is efficiency of the antenna.
Gmax = η(πD / λ)2 = η(π D f / c)2
c is the speed of light
Question:
The 1200SE has a gain of 43.4dB at 14GHz, what is it’s efficiency?
Polarisation
Vertical
Horizontal Horizontal
Vertical
a ac
b bc
bx
ax
At TransmittingAntenna
At ReceivingAntenna
Cross Polar IsolationXPI = ac / bx or bc / ax
or in dBXPI(dB) = 20log(ac / bx ) or 20log(bc / ax )
Cross Polar DiscriminationXPD = 20log ( ac / ax )
A typical value for XPD is 30dBc
Equivalent Isotropic Radiated Power
The power radiated per solid angle by an isotropic antenna fed from a an RF source of power PT is given by, PT / 4π
In a direction where the transmit gain is GT , any antenna radiates a power per unit solid angle equal to, PT GT / 4π
PTPT
GT = 1
ISOTROPIC ANTENNA
GT
Area ASolid Angle = A / R2
REAL ANTENNA
R
Power Flux Density
A satellite antenna of effective area A, at a distance R from the earth station subtends a solid angle A / R2, at the earth station antenna. The satellite antenna receives a power equal to
PR = (PT GT / 4π)(A / R2) = φ A
φ = PT GT / 4π R2 is called the power flux density (W / m2)
Typical values of φ are -90dBW/m2 to -80dBW/m2
PTPT
GT = 1
ISOTROPIC ANTENNA
GT
Area ASolid Angle = A / R2
REAL ANTENNA
R
Received Signal Power
For a receive antenna of effective area, AReff, from the transmit antenna, the received power is:
PR= φAReff = (PT GT / 4πR)AReff
The equivalent area of the antenna is a function of the gain, GR, and can be expressed as:
AReff = GR/(4π/λ2)
Therefore received power:
PR= (PT GT / 4π R2) (λ2 /4π) GR
= (PT GT )(λ2 /4πR)2 GR
= (PT GT )(1/LFS) GR
LFS is free space loss and represents the ratio of the received and transmitted powers in a link between two isotropic antennas and is of the order of 200dB.
Free Space Loss
Geostationary satellites are placed at a range, R0, 35786km above the equator.
LFS= (4πR/λ)2 = (4πR0/λ)2 (R/R0)= LFS(R0) (R/R0) 2
The range from an earth station to a satellite can be calculated from:
(R/R0)2 = (1+0.42(1 - cosLcosl))
l is the earth station latitude
L is the earth station to satellite relative longitude
(R/R0)2 is between 1 and 1.356 (0 to 1.3dB) depending on the earth station location.
Example Uplink
The 1200SE has a maximum antenna gain 43.4dB at 14GHz
It is fed by a 25W Kstar transceiver operating at 1dB output back off (OBO).
The RF loss between the Kstar output and the antenna interface is 1.5dB.
Calculate the uplink EIRP.
EIRP = PTGTmax/L
=((10*log(25))-1)+ 43.4 -1.5
= ? dBW
Calculate the power flux density , assuming the uplink is from Aberdeen to Telstar 12.
φ = (PTGTmax/L) / (4πR2)
= EIRP / (10*log(4*3.14*39100))
= ? dB(W/m2)
Example Downlink
BP operate a VSAT link to Aberdeen from the Jack Bates platform located West of Shetland. The range from the platform to the satellite is 39477km.
Calculate the power flux density at the earth station. Assume the link is via Telstar 12. The EIRP over the Shetland area is 49dBW.
φ = (PTGTmax/L) / (4πR2)
= 49 - (10*log(4*3.14*(39477000)2)
= -114 dB(W/m2)
If the downlink is to a 1200SE at 11.4GHz, calculate the free space loss, the gain of the 1200SE at the receive frequency and the power received by the 1200SE at Westhill.
LFS= 10*Log((4*3.14*39100000*11.4*10^9)/(3*10^8)) = 205.4dB
Grmax=10*log(0.67((3.14*1.2*11.4*10^9)/(3*10^8)^2) = 41.4
PR= EIRP - LFS + Grmax = 49 - 205.4 + 41.4= -115dBW = = 3.16pW
Sources of RF Loss
As well as free space loss and thermal losses in the output run from a VSAT HPA, there are additional losses arising from varied sources including:
atmospheric attenuation, rain, scattering, etc.
thermal losses in the equipment
mis-alignment of Tx and/or Rx antenna boresight
polarisation mismatch losses
Sources of RF Loss
Attenuation Of RF signal in the Atmosphere
Attenuation by rain and free space loss gives a total path loss that can be expressed as L = LFSLA
Transmit Losses, LFTX, between the HPA and the antenna
To provide an antenna with a power, PT, it is necessary to provide a power, PTX, at the HPA output so that PTX = PTLFTX
EIRP is, therefore, expressed as, EIRP = PTGT = (PTXGT)/ LFTX
Receive path losses, LFRX ,between the antenna and the receiver (LNB)
The signal power at the input to the receiver is PRX = PR LFTX / LFRX
Losses due to antenna misalignment
If the Tx and Rx antenna boresights are not aligned perfectly, there is a resultant loss in antenna gain. The losses are a function of the misalignment angles. Their value in dB is given by:
LT = 12(αT / θ3dB)2 and LR = 12(αR / θ3dB)2
Sources of RF Loss
Losses due to polarisation mismatch, LPOL
These occur when the receiving antenna is not oriented with the polarisation of the received wave.
At C Band we commonly use circular polarisation. The transmitted wave is only circularly polarised on the boresight axis of the antenna. Off axis the polarisation becomes elliptical. Propagation through the atmosphere can also change circular into elliptical polarisation.
At Ku Band we commonly use linear polarisation, as the wave propagates through the atmosphere the the of polarisation can rotate.
If the receive antenna is not properly aligned to the received waves plane of polarisation, and the angle of offset is γ, then LPOL = 20logcos γ
Typically, when installing a VSAT antenna feeds are adjusted to align the receive antenna boresight to the polarisation of the received wave.
γ
Summary of RF Loss
Considering all sources of loss, the signal power at the receiver becomes:
PRX = (PTX Gtmax / LTLFTX)(1/LFSLA)(Grmax/ LRLFRXLPOL)
The first bracket characterises the transmitting equipment EIRP
– This expression accounts for losses between the HPA and the antenna and the reduction in gain due to misalignment of the transmitting antenna.
The second bracket (1/L) characterises the transmitting medium
– The path loss takes account of attenuation of free space and the attenuation of the atmosphere due to rain etc.
The third bracket characterises the gain of the receiving equipment
– This expression accounts for losses between the receive antenna and the receiver (LNB), the loss of antenna gain due to misalignment and the losses due to polarisation mismatch.
Noise at the Receiver Input
Noise is unwanted signal without information content which is added to the useful signal. Noise reduces the ability of a receiver to reproduce the information content of the wanted signal correctly.
Noise originates from:
natural sources of radiation located within the antenna reception area
electronic components in the equipment
Only noise which lies in the signal bandwidth degrades receiver performance. Noise is commonly modelled assuming the power spectral density, N0 (W/Hz), is constant across the bandwidth. This is white noise. The equivalent noise power N (W) measured in a bandwidth BN (Hz) has a value: N = N0 BN (W)
B
N0(f)
N0
(W/Hz)
Frequency (Hz)
Spectral White Noise Density
Noise at the Receiver Input
The noise temperature of a noise source with noise power N is
T = N / kB = N0 / k
k is Boltzman’s constant = 1.379*10-23
T represents the thermodynamic temperature of a resistance which delivers the same available noise power as the source under consideration e.g. an LNB
If we consider the receive path of a VSAT terminal, we have several elements in series, each of these element has a gain, G j (j-1, 2, ….N) and an associated noise Tej. The overall noise of the receive path receives a contribution from each of the elements in the path.
The noise temperature of the device is
Te = Te1 + Te2/G1 + Te3/G1 G2 + …..+ TiN/G1 G2….GN-1
The noise figure of the device is
F = F1 + (F2 -1)G1 + (F3 -1)G1 G2 + …..+ (FN -1)G1 G2 ….GN-1
Application to noise temperature of Receiving Equipment
The receiving equipment above shows an antenna connected to an LNB.
There connection is lossy and is at a thermodynamic temperature, TF (which will be close to 290K). The connection has a loss value, LFRX, which corresponds to the equipment gain, GFRX= 1/ LFRX and is less than 1. The noise temperature of the system is determined at:
– the antenna output, before connection losses, temperature T1
– the LNB input, after connection losses, temperature T2
TA , Antenna
LFRX Feeder
T1
T2
TR , LNB
TF
Application to noise temperature of Receiving Equipment
At the antenna output, T1, the noise temperature, is the sum of the antenna noise temperature, and the receive subsystem consisting of the connection and the LNB in series. The noise temperature of the receive subsystem is (LFRX - 1) TF+ TR / GFRX. Adding the contribution of the antenna, which should be considered as a noise source, this becomes
T1 = TA + (LFRX - 1)TF + TR/GFRX
Now consider the LNB input, this noise must be attenuated by a factor LFRX. Replacing GFRX with 1/ LFRX , the noise temperature, T2, is:
T2 = T1 / LFRX = TA / LFRX + TF(1 - 1/LFRX ) + TR
TA , Antenna
LFRX Feeder
T1
T2
TR , LNB
TF
Consider a system with and without connection loss, LFRX.
Antenna noise temperature: TA = 100K
Thermodynamic temperature of the connection: TF = 290K
LNB noise temperature: TR = 90K
If LFRX, is zero
T2 = T1 / LFRX = TA / LFRX + TF(1 - 1/LFRX ) + TR
= 100 + 90 = 190K
If LFRX, is 1dB
= 100/101/10 + 290(1 - 1/101/10) + 90 = 79.43 + 59.6 + 90 = 229K
The connection losses reduce the antenna noise contribution but cause an overall increase in system noise temperature. Every 0.1dB of loss in the connection causes a 6.6K increase in system noise temperature
Note that the antenna noise temperature is a function of the direction in which it is pointing, its environment and its radiation pattern.
Noise Temperature Example
The Carrier to Noise Ratio, (Hz), of a link is calculated from
C/N0 = [(PTX Gtmax / LTLFTX)(1/LFSLA)(Grmax/ LRLFRXLPOL)]
/ [TA / LFRX + TF(1 - 1/LFRX ) + TR ](1/k)
C/N0 can also be interpreted as:
C/N0 = (transmitter EIRP)(1/path loss)(receiver gain/noise temperature)(1/k)
C/N0 can also be expressed in terms of power flux density
C/N0 = φ(λ2/4π)(receiver gain/noise temperature)(1/k)
Where, φ = (transmitter EIRP)(4πR2)
Carrier to Noise Ratio
The Carrier to Noise Ratio, (Hz), of a link is calculated from
C/N0 = [(PTX Gtmax / LTLFTX)(1/LFSLA)(Grmax/ LRLFRXLPOL)]
/ [TA / LFRX + TF(1 - 1/LFRX ) + TR ](1/k)
C/N0 can also be interpreted as:
C/N0 = (transmitter EIRP)(1/path loss)(receiver gain/noise temperature)(1/k)
C/N0 can also be expressed in terms of power flux density
C/N0 = φ(λ2/4π)(receiver gain/noise temperature)(1/k)
Where, φ = (transmitter EIRP)(4πR2)
The (receiver gain/noise temperature) expression in C/N0 the receive equipment G/T and is a figure of merit for the quality of performance of the receiving equipment.
Carrier to Noise Ratio
The noise temperature of a receiver (LNB) depends on the contributions from the components within it. Thus, there is a contribution from the front end LNA, a contribution from the downconverter stage and a contribution from any output IF amplifiers. This can be expressed as:
TR = TLNA + TMX/GLNA + TIF/GLNA GMX
Calculate the LNB system noise temperature for an LNB comprising:
TLNA = 110K, GLNA = 50dB
TMX = 850K, GMX = -10dB or LMX = 10dB
TIF = 400K, GIF = 30dB
TR = 110 + 850/105 + 400/ 105 10-1
=110K
It is the high gain of the LNA which limits the overall noise temperature of the LNB to that of the LNA.
Receiver Noise Temperature Example
Calculate the uplink C/N0 for the following system:
VSAT parameters:
– Frequency, 14.4GHz– Transmit power, 25W– Loss between HPA and
antenna, 1.5dB– Antenna diameter, 1.2m– Antenna efficiency, 0.67
– Maximum pointing error, 0.2°
– VSAT-Satellite distance, 39100km
– Atmospheric wave attenuation, 0.3dB
Example C/N0 Uplink
Satellite Parameters:
– Antenna efficiency, 0.65
– Receiving beam aperture, 2.5°
– Receiver noise figure, 2.5dB
– Input losses, 1dB– Polarisation mismatch
loss, 0dB
– Thermodynamic temperature of connection, 290K
– Antenna noise temperature, 290K
From the VSAT, EIRP = (PTX Gtmax / LTLFTX)
PTX = 25W = 10*log(25) = 14dBW
GTmax = η(πD / λ)2 = η(π D f / c)2 = 0.67[(π*1.2*14.4*109)/(3*108)]2 = 29139
GTmax = 10*log(29139) = 43.4dB
LT = 12(αT / θ3dB)2 =12 (αTDfu / 70c)2 = 0.3
EIRP = 43.4 + 14 - 0.3 - 1.5 = 55. 6dBW
Attenuation in the uplink is LU = LFS LA
LFS = (4πRfu / c)2 = 5.55*1020 = 10*log(5.55*1020 ) = 207.4dB
LU = 207.4 + 0.3 = 207.7dB
For the satellite,
G/T = (Grmax/ LRLFRXLPOL)] / [TA / LFRX + TF(1 - 1/LFRX ) + TR ]
GTmax = η(πD / λ)2 = η(π70/θ3dB)2 = 0.65(3.14*70/2.5)2 = 37dBi
Example C/N0 Uplink
G/T = 37 - 2.5 -1 - 10log(290/101/10 + 290(1 - 1/ 101/10) + 290) = 5.9dBK-1
For the uplink, (C/N0)U = (EIRP)VSAT(1/LU)(G/ T)SL(1/k)
(C/N0)U = 55.5dBW - 207.7dB + 5.9dBK-1 + 10*log(1.38*10-23) = 82.3dBHz
In order to calculate / achieve a given link availability it is necessary to include rain margin in the link budget. In a temperate climate (Northern Europe), attenuation due to rain, ARAIN, is typically 10dB. This figure, at a frequency of 14GHz, would typically be exceeded for 0.01% of the time for an average year.
This gives LU = 207.7 + 10 = 217.7dB
(C/N0)U = 55.5dBW - 217.7dB + 5.9dBK-1 + 10*log(1.38*10-23) = 72.3dBHz
The ratio (C/N0)U for the uplink would be greater than the 72.3dBHz for 99.99% of the time in an average year.
Example C/N0 Uplink
Calculate the downlink C/N0 for the following system:
Satellite parameters:
– Frequency, 11.6GHz– Transmit power, 125W– Satellite Output Losses,
2 dB– Satellite EIRP, 50dBW
VSAT Parameters:
– VSAT-Satellite distance, 39400km
– Atmospheric attenuation, 0.3dB
– Antenna diameter, 1.2m
Example C/N0 Downlink
VSAT Parameters (Contd.):
– Antenna efficiency, 0.67
– Receiving beam aperture, 2.5°
– Receiver noise figure, 1.4dB
– Input losses, 0.5 dB– Polarisation mismatch
loss, 0dB– Thermodynamic
temperature of connection, 290K
– Antenna noise temperature, 290K
From the Satellite, EIRP = (PTX Gtmax / LTLFTX) = 50dBW
Attenuation in the uplink is LD = LFS LA
LFS = (4πRfu / c)2 = 3.66*1020 = 10*log(5.55*1020 ) = 205.6dB
LU = 205.6 + 0.3 = 205.9dB
For the VSAT,
G/T = (GRmax/ LRLFRXLPOL)] / [TA / LFRX + TF(1 - 1/LFRX ) + TR ]
GRmax = η(πD / λ)2 = η(π D f / c)2 = 0.67[(π*1.2*11.6*109)/(3*108)]2 = 14236
GRmax = 10*log(14236) = 41.5dB
LT = 12(αT / θ3dB)2 =12 (αTDfu / 70c)2 = 0.2
LFRX = 0.5dB
Antenna noise temperature, TA = TSKY / ARAIN + Tm(1-1/ ARAIN) + TGROUND
– = 20/1010/10 + 275(1-1/1010/10) + 45 = 295K G/T = 41.5 - 0.2 - 0.6 -10*log(295/100.5/10 + 290(1-1/ 100.5/10)+110 =
14.8dBK-1
Example C/N0 Downlink
For the downlink, (C/N0)D = (EIRP)SL(1/LU)(G/ T)ES(1/k)
(C/N0)D = 50 - 216.2 + 14.8 +228.6 = 77.1 dBHz
The ratio C/ND for the downlink will be greater than 77.1dBHz for 99.99% of the time during an average year.
Example C/N0 Downlink
For the complete VSAT to VSAT link
(C/N0)-1T = (C/N0)-1
U + (C/N0)-1D + (C/N) )-1
SAT
This link has been calculated for a single carrier case.
For multicarriers, the HPA, of the VSAT uplink and the Satellite are backed off from saturation. This is done so that Intermodulation products resulting from interaction between the carriers are reduced. When the HPA is backed off sufficiently, it is said to be operating in the linear region.
Example C/N0 Total
Digital Transmission - Modulation
AnalogSource
DigitalSource
SourceEncoder
Encryptionand / orScrambling
Time DivisionMultiplexer
ChannelEncoding
DigitalModulation VSAT
Rb, Bit Rate
Rc, Bit Rate (bits/s)
R, Symbol Rate (baud)
Digital Transmission - Channel Encoding
N = 2n
information data symbolsN = 2n
Encoded data symbols
rredundancy bits
ChannelEncoder
Input rateRb
Output rateRc
Code Rate, ρ = n / (n + r)
Channel encoding inserts redundancy (r redundant bits for n information bits) for purposes of error control and error correction.
Rb = information bit rate
Rc = channel (encoded) bit rate
Rc = Rb / ρ
Rc is larger than Rb
Digital Transmission - Demodulation
Symbol error probability is a function E/N0
E = energy per bit (J)
N0 = noise power spectral density (W/Hz)
Eb/N0 = (C/N0) / Rb
VSAT DEMOD &DETECTION
SYMBOL DETECTION
BIT DETECTION
Symbol errorProbability
Bit errorProbability
R