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4. Iridium LCC (1997). Iridium System Facts.http:==www.apspg.com=whatsnew=iridium=facts.html5. Teledisic (1998). Technical overview of the Teledesic network.http:==www.teledisic.com=tech=details.html6. Porcelli, G. (1986). Effects of atmospheric refraction on sun interference, INTEL-SAT Technical Memorandum, IOD-E-86-05.7. Kitsuregawa, T. (1990). Advanced Technology in Satellite CommunicationAntenna: Electrical and Mechanical Design. Artech House.8. Mayhan, J.T. (1983). Adaptive antenna design considerations for satellite communicationantennas, Proc. IEEE, 130, parts F & H.9. Pritchard, W.L., Suyderhoud, H.G., and Nelson, R.A. (1993). Satellite CommunicationSystems Engineering. Prentice-Hall.10. Hwang, Y. (1992). Satellite antennas, Proc. IEEE, 80, 183–193.11. Dalgleish, D.I. (1989). An Introduction to Satellite Communications. PeterPeregrinus.12. Maral, G. and Bousquet, M. (1993). Satellite Communications System: Systems,Techniques and Technology. John Wiley.13. Schekunoff, S.A. (1943). Electromagnetic Waves. D van Nostrand.14. Stratton, J.A. (1941). Electromagnetic Theory. McGraw-Hill.15. Aviation Week & Space Technology, Dec. 1977, 51.16. Aviation Week & Space Technology, Jan. 1999, 65.PROBLEMS1. A satellite system consists of 1000 units in series configuration. The failurerate of each unit is 0.48% per 1000 hours and is known to be constant. Ifthe mission time of the system is 1000 hours, calculate the systemreliability. If the desired reliability of the system for a mission time of1000 hours is 0.98, determine what failure rate would be required of thecomponents.2. An earth station is located at 79:34 W longitude and 37:09 N latitude.Calculate its look angle and range to a geosynchronous satellite whosesubsatellite point is located at 102 W longitude.3. Your colleague has been told to design an earth station, which is to belocated in your town. As an independent observer, you are encouraged toprovide a solution to check your colleague’s calculation. The subsatellitepoint should be within 22:25 of the town’s longitude. Write a computerprogram to compute the various look angles and ranges to a satellite locatedin geosynchronous orbit.4. A customer required 165.85 W continuous power for a communicationsatellite. Design a power source that meets this requirement. What addi-Copyright © 2002 by Marcel Dekker, Inc. All Rights Reserved.
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SatelliteCommunicationEngineeringMi
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This book is dedicated to my famili
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Because of the immense importance o
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means of a combination of applicati
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about my promise to my students, an
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2.3 Coverage Area and Satellite Net
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1Basic Principles of SatelliteCommu
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and voice (telephone) communication
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FIGURE 1.2Communication between two
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interpreting or uncovering the deci
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cryptographic keys K ti (where i ¼
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FIGURE 1.6Block ciphering technique
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FIGURE 1.7Part of block ciphering w
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Based on the ordering sequence of (
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TABLE 1.1 (continued )S612 1 10 15
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For an uncoded message x and the fe
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2. Your task is to develop a commun
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FIGURE 2.1Geometry of a satellite.
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Future trends in satellite antennas
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In the United States, the three sat
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TABLE 2.3Typical Links Frequency Ba
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FIGURE 2.4Satellite period and orbi
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FIGURE 2.6An illustration of covera
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FIGURE 2.7constellation.A sketch of
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width of 1:73 with reduced coverag
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y ¼ elevation angle of satellite f
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We can conclude that the antenna mu
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FIGURE 2.9Design flowchart of a sat
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Risk control and monitoring measure
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TABLE 2.4Antenna Selection Criteria
Page 122: Then the system availability can be
Page 126: In fact, MTBF is the reciprocal of
Page 130: 2.7 ANTENNASBased on function, sate
Page 134: Two kinds of horns in common use ar
Page 138: FIGURE 2.13Geometry of a parabolic
Page 142: FIGURE 2.14 Axisymmetric reflector
Page 146: A transceiver antenna is a single a
Page 150: The gain, in the axial mode, of a h
Page 154: angles, spacecraft may shadow the s
Page 158: 3. The probability of both parallel
Page 162: the baseband signal (more details a
Page 166: matrix in the communications subsys
Page 170: FIGURE 2.24Typical transfer charact
Page 176: tional protection is required to en
Page 180: 3.1 BASIC PRINCIPLE OF EARTH STATIO
Page 184: 3.1.1 Technical and Operational Req
Page 188: excellent protection against noise
Page 192: FIGURE 3.3QPSK modulator.FIGURE 3.4
Page 196: TABLE 3.28-PSK Truth TableInput bit
Page 200: FIGURE 3.8An M-ary PSK demodulator
Page 204: where B is the allocated channel ba
Page 208: A frequently used function is the Q
Page 212: In view of (3.11), Eq. (3.18) can b
Page 216: Encoder and DecoderAn encoder is an
Page 220: Modulator and DemodulatorA modulato
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Zero Forcing Technique. Suppose the
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The adjoint of matrix A is obtained
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FIGURE 3.14The three-tap equalizer
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First, in the case of digital signa
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than 1=A. Whichever law is used, th
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FIGURE 3.16Block diagram for estima
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3.4.2 Antenna TrackingAn earth stat
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controlling antenna pointing. The m
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FIGURE 3.19A generalized model of a
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FIGURE 3.20Entropy of a binary sour
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whereHðYÞ¼output entropy, the av
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To have a feel for this expression,
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2. The system’s overall condition
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transmitted down the fiber as digit
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10. Kantor, L. Y. (ed). (1987). Han
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142. Simulate the probability of bi
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FIGURE 4.1A simplex link.baseband c
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Chapter 2, Sec. 2.7, discusses that
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From (4.6), the received power P r
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FIGURE 4.3A model of the combined-l
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4.1.2 Rain AttenuationRain attenuat
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FIGURE 4.5rates.Average rainstorm p
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FIGURE 4.6Adjacent satellite interf
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FIGURE 4.8Satellite separation dist
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inability of satellite A to accurat
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FIGURE 4.10 Cross-link E b =N 0 vs.
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Then using (4.41), the overall C=N
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(iv)(v)(vi)(vii)Calculate the recei
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5Communication Networks andSystemsC
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discriminate among carriers by temp
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FIGURE 5.2 Principle of FDMA system
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FIGURE 5.3 Operational concept of T
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FIGURE 5.5TDMA: bit rate r b for 1
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Copyright © 2002 by Marcel Dekker,
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5.2 CAPACITY COMPARISON OFMULTIPLE-
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Rearranging (5.11) in terms of ener
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The transmission bit rate isR r ¼
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6Error Detection and CorrectionCodi
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the channel and reconstruct the sou
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message sequence X . Thus, a system
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If we consider a message X ¼ð1010
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can be seen in Table 6.1 that the m
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FIGURE 6.1A (7, 4) cyclic code gene
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FIGURE 6.2Convolutional codes encod
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Alternative methods of describing a
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FIGURE 6.5 Code tree diagram of Fig
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FIGURE 6.8 Code tree diagram of rat
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consistent with the constraint leng
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trellis depth is approximated to 5L
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FIGURE P.1A convolutional coder.the
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7Regulatory Agencies andProceduresT
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of the radiofrequency spectrum, and
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The CCIR works through the medium o
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7.1.3 IFRBThe International Frequen
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The national or regional spectrum m
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3. The need to expand or enhance th
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The DSP will be responsible for res
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2. Provide a convenient framework w
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FIGURE 8.3Types of user-to-network
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H1-channels are designed to carry v
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information. The transfer cell prov
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The OSI layers are divided into two
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plane is denoted by U, the control
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interfacing, maintenance, and conne
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adjoining base station to scan the
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FIGURE 8.9Geometry of a polygon.The
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FIGURE 8.11Splitting cells into sma
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causes signal fading. Of course, th
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FIGURE 8.14TCP=IP suite and its rel
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access to an Internet point of pres
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message security via satellite is d
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REFERENCES1. Wu, W.W. (1989). Eleme
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Appendix ANotationsThe symbols have
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N sPP rP sP TRRðtÞR cR eR rR vSS
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g Central anglez Channel gainZ Ante
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AttenuationBandwidthBearer serviceB
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Frequency divisionmultiple accessFr
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MultiplexingNetworkOmnidirectionala
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UplinkUser-to-networkinterfaceThe e
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