Global Positioning System Reference
In-Depth Information
four satellites form the optimum constellation. Under this condition the ele-
vation angle is 0 degree and three of the four satellites form an equilateral
triangle. The observer is at the center of the base of the tetrahedron. Under this
condition, the DOP values are: GDOP = 3 1 . 73, PDOP = 2 2 / 3 1 . 63,
HDOP = VDOP = 2 / 3 1 . 15, and TDOP = 1 / 3 0 . 58. These values can
be considered as the minimum values (or the limits) of the DOPs. In selecting
satellites, the DOP values should be as small as possible in order to generate the
best user position accuracy.
2.16 SUMMARY
This chapter discusses the basic concept of solving the GPS user position. First
use four or more satellites to solve the user position in terms of latitude, lon-
gitude, altitude, and the user clock bias as discussed in Section 2.5. However,
the solutions obtained through this approach are for a spherical earth. Since the
earth is not a perfect sphere, the latitude and altitude must be modified to reflect
the ellipsoidal shape of the earth. Equations (2.51) and (2.57) are used to derive
the desired values. These results are shown in Figure 2.9 as a quick reference.
Finally, the selection of satellites and the DOP are discussed.
REFERENCES
1. Spilker, J. J., “GPS signal structure and performance characteristics,” Navigation , Insti-
tute of Navigation, vol. 25, no. 2, pp. 121 - 146, Summer 1978.
2. Spilker, J. J. Jr., Parkinson, B. W., “Overview of GPS operation and design,” Chapter
2, and Spilker, J. J. Jr., “GPS navigation data,” Chapter 4 in Parkinson, B. W., Spilker,
J. J. Jr., Global Positioning System: Theory and Applications , vols. 1 and 2, American
Institute of Aeronautics and Astronautics, 370 L'Enfant Promenade, SW, Washington,
DC, 1996.
3. Kay, S. M., Fundamentals of Statistical Signal Processing Estimation Theory , Chapter
8, Prentice Hall, Englewood Cliffs, NJ 1993.
4. Bate, R. R., Mueller, D. D., and White, J. E., Fundamentals of Astrodynamics , Chapter
5, Dover Publications, New York, 1971.
5. Britting, K. R., Inertial Navigation Systems Analysis , Chapter 4, Wiley, 1971.
6. Riggins, R. “Navigation using the global positioning system,” Chapter 6, class notes,
Air Force Institute of Technology, 1996.
7. “Department of Defense world geodetic system, 1984 (WGS-84), its definition and rela-
tionships with local geodetic systems,” DMA-TR-8350.2, Defense Mapping Agency,
September 1987.
8. Spilker, J. J. Jr., “Satellite constellation and geometric dilution of precision,” Chapter
5, and Axelrad, P., Brown, R. G., “GPS navigation algorithms,” Chapter 9 in Parkinson,
B.W.,Spilker,J.J.Jr., Global Positioning System: Theory and Applications , vols. 1
and 2, American Institute of Aeronautics and Astronautics, 370 L'Enfant Promenade,
SW, Washington, DC, 1996.
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