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CHAP TER 1 4. 1       Global positioning technology

               14.1.2.2.3 Almanac and support data                most users from taking full advantage of both GPS fre-
               subframes                                          quencies. Without a complete knowledge of the
                                                                  encrypted L 2 frequency, only mathematical exercises
               Subframes four and five of the navigation message data  enable high accuracy applications of GPS such as sur-
               frame contain comprehensive almanac data for the entire  veying to take advantage of any information provided by
               GPS constellation, along with delay parameters that the
                                                                  L 2 .
               receivers use for approximating phase delay of the
               transmitted signal through the ionosphere, and correc-
               tion factors to correlate GPS and Universal Time   14.1.3.1.1 Position calculation
               Coordinated (UTC).                                 The fundamental technique for determining position
                 The almanac data contains orbit and health in-   with the GPS is based on a basic range measurement
               formation on all of the satellites in the GPS constellation.  made between the user and each GPS satellite observed.
               GPS receivers use this information to speed up the  These ranges are actually measured as the GPS signal
               acquisition of SV signal transmissions. The almanac data  time of travel from the satellite to the observer’s posi-
               in subframe four contains health and status information  tion. These time measurements may be converted to
               on the operational satellites numbered 25 through 32,  ranges simply by multiplying each measurement by the
               along with ionospheric and UTC data. The almanac data  speed of light; however, since most GPS receiver internal
               in subframe five contains health and status information  clocks are incapable of keeping time with sufficient
               on the operational satellites in the GPS numbered  accuracy to allow accurate ranging, the mathematical
               1 through 24.                                      PVTsolution must solve for errors in the receiver clock at
                 For a more detailed description of the information
               contained in the Navigation Message, refer to the ICD-  the time each observation of a satellite is made. Satellite
                                                                  ranges are commonly called pseudoranges to include this
               GPS-200c specification, which is available from the US  receiver clock error and a variety of other errors inherent
               Coast Guard Navigation Center.
                                                                  in using GPS. These receiver clock errors are included as
                                                                  one component in a least squares calculation, which is
               14.1.3 Fundamentals of satellite-                  used to solve for position using a technique called
               based positioning                                  trilateration.
                                                                    To calculate the values for PVT, the concept of tri-
                                                                  angulation in two-dimensions as is commonly practised in
               To understand the true value and cost of the positioning  determining the location of an earthquake epicentre is
               capabilities of the GPS, it is important for the user to  extended into three-dimensions, with the ranges from
               have a basic understanding of the science behind posi-  the satellites prescribing the radius of a sphere (see
               tioning, and the types of components and techniques that  Fig. 14.1-2). This technique is known as trilateration,
               may be used to calculate accurate positions. This section  since it uses ranges to calculate position, whereas tri-
               divides this discussion into three main areas: the basic  angulation uses angular measurements. If a sphere
               science behind GPS; the different unassisted and   centred on the satellites’ position in space is hypotheti-
               assisted position calculation techniques that may be  cally created with the range from the user to each sat-
               used, depending upon the needs of the specific appli-  ellite as its radius, the intersection of three of these
               cation; and the hardware and software components   spheres may be used to determine a user’s two-
               necessary for calculating a position.
                                                                  dimensional position. While it may seem counterintui-
                                                                  tive that ranges to three satellites will allow for only
               14.1.3.1 The basic science of global               a two-dimensional position, in fact one observation is
               positioning                                        needed to solve for each of latitude, longitude and
                                                                  receiver clock error. Thus, to determine a user’s position
               The design of the GPS makes it an all-weather system  in three-dimensions a minimum of four satellites is
               whereby users are not limited by cloud cover or in-  required, in order to solve for altitude, as well as latitude,
               clement weather. Broadcasting on two frequencies, the  longitude and clock error.
               GPS provides sufficient information for users to de-  Once pseudoranges have been determined to three or
               termine their PVT with a high degree of accuracy and  more SVs, the user’s PVT can be calculated by solving
               reliability. As mentioned previously, frequency L 1 is  N simultaneous equations as a classic least squares
               generally regarded as the civilian frequency while fre-  problem, where N is the number of satellite pseudor-
               quency L 2 is primarily used for military applications.  anges measured. The relationship between the receiver
               Applications and positioning techniques in this chapter  and each satellite’s position can best be written by
               will focus on GPS receiver technology capable of tracking  extending the Pythagorean Theorem as illustrated in
               L 1 only, as cost and security issues typically preclude  equation 14.1.1, where i is the number of each satellite


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