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Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 3 potx

Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 3 potx

Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 3 potx

... maximum Fundamentals of Global Positioning System Receivers: A Software Approach James Bao-Yen TsuiCopyright 2000 John Wiley & Sons, Inc.Print ISBN 0-4 7 1 -3 815 4 -3 Electronic ISBN 0-4 7 1-2 005 4-9 32 CHAPTER ... E, and the true n anomalies. Mean anomalyM and eccentricity esare given from the navigation data of the satellite. Eccen-tric anomaly E can be obtained from Equation ( 3. 30). True anomaly ... antenna and the accuracy of thesolid angle of the antenna because the power cannot be cut off sharply at a desired angle.If the receiving antenna has a unit gain, the effective area is(16) A effl24p( 3. 44)where...
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Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 4 potx

Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 4 potx

... 1996. Fundamentals of Global Positioning System Receivers: A Software Approach James Bao-Yen TsuiCopyright 2000 John Wiley & Sons, Inc.Print ISBN 0-4 7 1 -3 815 4 -3 Electronic ISBN 0-4 7 1-2 005 4-9 54 CHAPTER ... CORRECTION OF GPS SYSTEM TIME AT TIME OF TRANSMISSION 67nm a 3 s+ Dn (4 .33 )where m 3. 986005 × 1014meters 3 /sec2is the earth’s universal gravitationalparameter and is a constant, a sand Dn are ... time.q: argument of perigee.idot: rate of inclination angle.4.12 SUMMARYThis chapter takes the satellite position calculated in Chapter 3 and transformsit into an earth-centered, earth-fixed...
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Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 9 potx

Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 9 potx

... q is the argument of perigee (subframe 3, bits 197–204 and 211– 234 )obtained from navigation data. Fundamentals of Global Positioning System Receivers: A Software Approach James Bao-Yen TsuiCopyright ... in subframe 3 intoephermeris dataclear angmat navd rymkmatload d:/gps/big data/srvy 831 0;angmatang;ptnumattranspt;rymkmatfintime;[st navd]navdat(angmat);∗find naviga data (20ms) ... d:/gps/big data/srvy8210;angmatang;ptnumattranspt;rymkmatfintime;[st navd]navdat(angmat);∗find naviga data (20ms) & first angle9. 13 ADJUSTMENT OF COORDINATE SYSTEM OF SATELLITES 2 13 r1(x1xu)2+(y1yu)2+(z1zu)2+...
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Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 1 docx

Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 1 docx

... History of GPS Development 11 .3 A Basic GPS Receiver 21.4 Approaches of Presentation 3 1.5 Software Approach 3 1.6 Potential Advantages of the Software Approach 41.7 Organization of the ... tracking are per-formed by hardware. From the navigation data phase transition the subframesand navigation data can be obtained. Ephemeris data and pseudoranges can beFIGURE 1.1 A fundamental ... Generation of C/ A Code 785.7 Correlation Properties of C/ A Code 83 Fundamentals of Global Positioning System Receivers: A Software Approach James Bao-Yen TsuiCopyright 2000 John Wiley &...
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Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 2 ppsx

Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 2 ppsx

... isdr1dr2dr 3 dr4...drn a 11 a 12 a 13 1 a 21 a 22 a 23 1 a 31 a 32 a 33 1 a 41 a 42 a 43 1... a n1 a n2 a n31dxudyudzudbu(2. 13) where a i1xixuribu a i2yiyuribu a i3zizuribu(2.9)Equation ... [dxudyudzudbu]T a  a 11 a 12 a 13 1 a 21 a 22 a 23 1 a 31 a 32 a 33 1 a 41 a 42 a 43 1... a n1 a n2 a n31(2.15)12 BASIC GPS CONCEPTuser clock error cannot be corrected ... asdr1dr2dr 3 dr4 a 11 a 12 a 13 1 a 21 a 22 a 23 1 a 31 a 32 a 33 1 a 41 a 42 a 43 1dxudyudzudbu(2.8)where a i1xixuribu a i2yiyuribu a i3zizuribu(2.9)The...
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Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 5 pps

Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 5 pps

... navigation data rate carried by the P code through phasemodulation is at a 50 Hz rate.5.5 C/ A CODE AND DATA FORMAT(1,2,5)The C/ A code is a bi-phase modulated signal with a chip rate of ... health indication of the transmitting satellite. The MSB (bit77) indicates a summary of thehealth of the navigation data, where bit77 equals:0 All navigation data are OK.1 Some or all navigation ... Global Positioning System: Theory and Applications, vols.1 and 2, Ameri-can Institute of Aeronautics and Astronautics, 37 0 L’Enfant Promenade, SW, Wash-ington, DC,1996.8. Raquet, J., “Navigation...
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Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 6 pps

Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 6 pps

... Spilker(11)indicated that a 1-bit ADCdegrades the signal-to-noise ratio by1.96 dB and a 2-bit ADC degrades thesignal-to-noise by0.55 dB. Many commercial GPS receivers use only 1- or2-bit ADCs.Chang(12)claims ... theoretical performance,” Chapter 3 inParkinson, B. W., Spilker, J. J. Jr., Global Positioning System: Theory and Appli-cations, vols.1 and 2, American Institute of Aeronautics and Astronautics, 37 0L’Enfant ... Receivers: A Software Approach James Bao-Yen TsuiCopyright 2000 John Wiley & Sons, Inc.Print ISBN 0-4 7 1 -3 815 4 -3 Electronic ISBN 0-4 7 1-2 005 4-9 109 CHAPTER SIXReceiver HardwareConsiderations6.1...
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Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 7 pdf

Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 7 pdf

... input data do not arrive in a continuousmanner. This operation is suitable for a block of data. The input data are sam-pled with a 5 MHz ADC and stored in memory. Only 1 ms of the input data areused ... CODE SIGNALSFIGURE 7.6 Effect of phase transition on the delay and multiplication method.search for 1 ms of data to acquire a satellite. Longer data are needed for acquir-ing a certain satellite.One ... CONVOLUTION AND CIRCULAR CORRELATION(1)This section provides the basic mathematics to understand a simpler way to per-form correlation. If an input signal passes through a linear and time-invariant system, ...
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Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 8 pps

Fundamentals of Global Positioning System Receivers A Software Approach - Chapter 8 pps

... 0x(n)ej2pnk/N(8.40) Fundamentals of Global Positioning System Receivers: A Software Approach James Bao-Yen TsuiCopyright 2000 John Wiley & Sons, Inc.Print ISBN 0-4 7 1 -3 815 4 -3 Electronic ISBN 0-4 7 1-2 005 4-9 165 CHAPTER ... complicated and calculation intensive.In order to track20 ms of data without a navigation data phase transition,one must find a phase transition in the data. This requirement puts an additionalrestraint ... Jr., Global Positioning System: Theory and Applications, vols.1 and 2, AmericanInstitute of Aeronautics and Astronautics, 37 0 L’Enfant Promenade, SW, Washing-ton, DC,1996.7. Stockmaster,...
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fundamentals of global positioning system receivers a software approach

fundamentals of global positioning system receivers a software approach

... formats. Some content that appears inprint, however, may not be available in electronic format.Library of Congress Cataloging-in-Publication DataTsui, James Bao-yen. Fundamentals of global positioning ... includingthe high-dynamics user, such as in high-speed aircraft with flexiblemaneuverability. Fundamentals of Global Positioning System Receivers: A Software Approach, Second Edition,by James Bao-Yen TsuiISBN ... From the navigation data phase transition the subframesand navigation data can be obtained. Ephemeris data and pseudoranges can beobtained from the navigation data. The ephemeris data are used...
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