{ "metadata": { "name": "", "signature": "sha256:4b08bbb242b14bb2e9d6b297d6c2efe9724a5525d0e315485c89f280e01ac4b8" }, "nbformat": 3, "nbformat_minor": 0, "worksheets": [ { "cells": [ { "cell_type": "heading", "level": 1, "metadata": {}, "source": [ "Chapter 16: Direct Broadcast Satellite Services" ] }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 16.1, Page 474" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math\n", "#Varaible Declaration\n", "\n", "EIRP=55 #EIRP for satellite(dBW)\n", "fD=12.5 #Downlink frequency(GHz)\n", "Pss=-101 #Receiving at ground station direction(degrees west)\n", "Rb=40*10**6 #Transmission Rate(Hz)\n", "D=18 #Diameter of antenna(inches)\n", "n=0.55 #Efficiency of antenna\n", "Tant=70 #Antenna noise(Kelvin)\n", "Teq=100 #Equivalent noise temperature at LNA(Kelvin)\n", "R=6371 #Radius of earth(Km)\n", "L=2 #Transmission losses(dB)\n", "aGSO=42164 #Circumference of earth(km)\n", "k=-228.6 #Boltzmann's constant (dB)\n", "PE=-90 #Longitude of Earth station(degrees west)\n", "LE=45 #Latitude of Earth station(degrees north)\n", "f=14 #Frequency(GHz)\n", "#Calculation\n", "B=PE-Pss\n", "b=math.acos(math.cos(B*3.142/180)*math.cos(LE*3.142/180))\n", "b=b*180/3.142\n", "A=math.asin(math.sin(abs(B)*3.142/180)/math.sin(b*3.142/180))\n", "A=A*180/3.142\n", "Az=180+A #Azimuth angle of antenna(degrees)\n", "d=(R**2+aGSO**2-2*R*aGSO*math.cos(b*3.142/180))**0.5 #Range of antenna(km)\n", "El=math.acos(aGSO*math.sin(b*3.142/180)/d) #Elevation angle of antenna(radians)\n", "El=El*180/3.142 #Elevation angle of antenna(degrees)\n", "Az=round(Az,1)\n", "El=round(El)\n", "d=round(d)\n", "FSL=32.4+20*math.log10(d)+20*math.log10(f*10**3) #Free space loss(dB)\n", "LOSSES=FSL+L #Total Transmission Losses\n", "Ts=Teq+Tant #Total system noise temperature(Kelvin)\n", "T=10*math.log10(Ts) #Total system noise temperature(dBK)\n", "G=n*(3.192*f*(D/float(12)))**2\n", "G=10*math.log10(G) #Antenna Gain(dB)\n", "GTR=G-T #G/T ratio(dB)\n", "CNR=EIRP+GTR-LOSSES-k #Carrier to noise ratio(dB)\n", "Rb=10*math.log10(Rb) #Transmission Rate(dBHz)\n", "EbN0R=CNR-Rb #Eb/N0 ratio at IRD(dB)\n", "EbN0R=round(EbN0R,1)\n", "#Results\n", "\n", "print \"The Azimuth angle of antenna is\",Az,\"degrees\"\n", "print \"The Elevaation Angle of Antenna is\",El,\"degrees\"\n", "print \"The Range of Antenna is\",d,\"km\"\n", "print \"The Eb/N0 ratio at IRD is\",EbN0R,\"dB\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "The Azimuth angle of antenna is 195.4 degrees\n", "The Elevaation Angle of Antenna is 37.0 degrees\n", "The Range of Antenna is 38020.0 km\n", "The Eb/N0 ratio at IRD is 10.3 dB\n" ] } ], "prompt_number": 1 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 16.2, Page 480" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math\n", "#Varaible Declaration\n", "\n", "R01=42 #Rainfall at earth station(mm/hr)\n", "p=0.01 #Percentage of time for which rain exceeds\n", "LE=45 #Latitue of earth station(degrees)\n", "hR=3.5 #Rain Height(km)\n", "h0=0 #Mean Sea level(km)\n", "Ta=272 #\n", "El=37 #Elevation angle of the antenna(degrees)\n", "Ts=170 #Total system noise temperature(Kelvin)\n", "NCR=2.3*10**-9 #Carrier to noise ratio\n", "fD=12.5 #Frequency of operation(GHz)\n", "f12=12 #Frequency 12GHz(GHz)\n", "f15=15 #Frequency 15GHz(GHz)\n", "#Coefficients for horizontal and vertical polarizations at 12GHz and 15GHz as given in Table 4.2\n", "\n", "ah12=0.0188\n", "av12=0.0168\n", "bh12=1.217\n", "bv12=1.2\n", " \n", "ah15=0.0367\n", "av15=0.0335\n", "bh15=1.154\n", "bv15=1.128\n", "\n", "#Calculation\n", "\n", "#Using Interpolation to find coefficients at 12.5 GHz\n", "\n", "ah=round(ah12+(ah15-ah12)*(fD-f12)/(f15-f12),3)\n", "bh=round(bh12+(bh15-bh12)*(fD-f12)/(f15-f12),3)\n", "av=round(av12+(av15-av12)*(fD-f12)/(f15-f12),3)\n", "bv=round(bv12+(bv15-bv12)*(fD-f12)/(f15-f12),3)\n", "\n", "#Coefficients for circular polarization\n", "\n", "ac=(ah+av)/2\n", "ac=round(ac,3)\n", "bc=(ah*bh+av*bv)/(2*ac)\n", "bc=round(bc,3)\n", "Ls1=(hR-h0)/math.sin(El*3.142/180) #Slant Path Length(km)\n", "Ls=round(Ls1,1) #Slant Path Length(km)\n", "LG=round(Ls*math.cos(El*3.142/180),1) #Horizontal projection of slant path length(km)\n", "r011=90/(90+4*LG) #Reduction Factor\n", "r01=round(r011,1) #Reduction Factor\n", "L=round(Ls1*r01,1) #Effective path length(km)\n", "alpha=round(ac*R01**bc,3) #Specific attenuation(dB/km)\n", "A=round(10**(alpha*L/float(10)),1) #Total Attenuation(dB)\n", "Trn=Ta*(1-1/A) #noise temperature with effect of rain\n", "Tscs=Ts\n", "NCrain=NCR*(A+(A-1)*Ta/Tscs) #Noise to carrier ratio due to rain\n", "CNrain=-10*math.log10(NCrain)#Noise to carrier ratio due to rain(dB)\n", "Rb=10*math.log10(40*10**6) #Transmission rate(dB)\n", "EbN0rain=round(CNrain-Rb,1) #Upper limit of Eb/N0 ratio in prescence of rain(dB)\n", "\n", "#Result\n", "\n", "print \"Hence the upper limit for Eb/N0 for given conditions is\",EbN0rain,\"dB\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Hence the upper limit for Eb/N0 for given conditions is -2.1 dB\n" ] } ], "prompt_number": 2 } ], "metadata": {} } ] }