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Guidelines for the use of GNSS in surveying and mapping

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or as <strong>the</strong> corrections that would be generated from<br />

a ‘virtual’ base station adjacent to <strong>the</strong> <strong>use</strong>r. Actual<br />

raw base station GPS data or virtual GPS<br />

observation data is also transmitted to <strong>the</strong> rover.<br />

Observ<strong>in</strong>g session<br />

The period <strong>of</strong> time over which <strong>GNSS</strong> data is<br />

collected simultaneously by two ore more receivers.<br />

PDOP (Position dilution <strong>of</strong> precision)<br />

PDOP is a unitless scalar value express<strong>in</strong>g <strong>the</strong><br />

relationship between <strong>the</strong> error <strong>in</strong> <strong>use</strong>r position <strong>and</strong><br />

<strong>the</strong> error <strong>in</strong> satellite position. Geometrically, <strong>for</strong> four<br />

satellites PDOP is proportional to <strong>the</strong> <strong>in</strong>verse <strong>of</strong> <strong>the</strong><br />

volume <strong>of</strong> <strong>the</strong> pyramid <strong>for</strong>med by unit vectors from<br />

<strong>the</strong> receiver to <strong>the</strong> four satellites observed. Values<br />

considered good <strong>for</strong> position are small, say 3.<br />

Values greater than 7 are considered poor. Thus,<br />

small PDOP is associated with widely separated<br />

satellites. PDOP is related to horizontal <strong>and</strong> vertical<br />

DOP by PDOP 2 = HDOP 2 + VDOP 2 . Small PDOP is<br />

important <strong>in</strong> dynamic surveys, which are sensitive<br />

to larger PDOP values, but much less so <strong>in</strong> static<br />

techniques.<br />

Phase lock<br />

The technique whereby <strong>the</strong> phase <strong>of</strong> an oscillator<br />

signal is made to follow exactly <strong>the</strong> phase <strong>of</strong> a<br />

reference signal. It does so by first compar<strong>in</strong>g <strong>the</strong><br />

phases <strong>of</strong> <strong>the</strong> two signals <strong>and</strong> <strong>the</strong>n us<strong>in</strong>g <strong>the</strong><br />

result<strong>in</strong>g phase difference signal to adjust <strong>the</strong><br />

reference oscillator frequency, so as to elim<strong>in</strong>ate<br />

phase difference when <strong>the</strong> two signals are next<br />

compared.<br />

Phase observable<br />

See Reconstructed carrier phase.<br />

Po<strong>in</strong>t position<strong>in</strong>g<br />

A geographic position produced from one receiver<br />

<strong>in</strong> a st<strong>and</strong>-alone mode. At best, position accuracy<br />

obta<strong>in</strong>ed from a st<strong>and</strong>-alone receiver is 20-30m,<br />

depend<strong>in</strong>g on <strong>the</strong> geometry <strong>of</strong> <strong>the</strong> satellites.<br />

Precise (P)-code<br />

The protected or precise code transmitted on both<br />

L1 <strong>and</strong> L2 GPS frequencies. This code is made<br />

available by <strong>the</strong> DoD only to authorised <strong>use</strong>rs. The<br />

P-code is a very long sequence (about 1014 bits) <strong>of</strong><br />

pseudo r<strong>and</strong>om b<strong>in</strong>ary bi-phase modulations <strong>of</strong> <strong>the</strong><br />

GPS carrier at a chipp<strong>in</strong>g rate <strong>of</strong> 10.23 MHz. It<br />

repeats every seven days but is a section <strong>of</strong> a full<br />

37 week code. Each satellite <strong>use</strong>s a one-week<br />

segment <strong>of</strong> this code which is unique to each GPS<br />

satellite, <strong>and</strong> is reset each week.<br />

Precise position<strong>in</strong>g service (PPS)<br />

The full accuracy, s<strong>in</strong>gle-receiver GPS position<strong>in</strong>g<br />

service provided to <strong>the</strong> United States military<br />

organisations <strong>and</strong> o<strong>the</strong>r selected agencies.<br />

Pseudo r<strong>and</strong>om noise (PRN)<br />

PRN is a sequence <strong>of</strong> b<strong>in</strong>ary digits that appear to<br />

be r<strong>and</strong>omly distributed. This is <strong>use</strong>d <strong>in</strong> <strong>the</strong> <strong>GNSS</strong><br />

C/A <strong>and</strong> P codes, with each <strong>GNSS</strong> satellite<br />

transmitt<strong>in</strong>g a unique PRN. <strong>GNSS</strong> receivers <strong>use</strong> this<br />

PRN to identify which satellites <strong>the</strong>y are track<strong>in</strong>g.<br />

The important property <strong>of</strong> PRN codes is that <strong>the</strong>y<br />

have a low auto correlation value <strong>for</strong> all delays or<br />

lags except when <strong>the</strong>y are exactly co<strong>in</strong>cident. Each<br />

NAVSTAR satellite has its own unique C/A <strong>and</strong> P<br />

pseudo r<strong>and</strong>om noise codes.<br />

Pseudo static<br />

A technique <strong>in</strong>volv<strong>in</strong>g <strong>the</strong> observation <strong>of</strong> two<br />

separate simultaneous data sets at two or more<br />

stations with a time gap between observations (60<br />

m<strong>in</strong>utes is recommended). Data sets can be<br />

computed with <strong>the</strong> k<strong>in</strong>ematic processor or as a<br />

static <strong>GNSS</strong> observation set with two files at each<br />

station. Basel<strong>in</strong>e vectors can be computed <strong>and</strong><br />

applied to <strong>the</strong> known station(s) with<strong>in</strong> a network. A<br />

good method when cont<strong>in</strong>uous lock is unlikely to<br />

be ma<strong>in</strong>ta<strong>in</strong>ed due to vegetation or o<strong>the</strong>r<br />

obstructions.<br />

Pseudolite<br />

A ground-based <strong>GNSS</strong> transmitter station which<br />

broadcasts a signal with a structure similar to that<br />

<strong>of</strong> an actual <strong>GNSS</strong> satellite.<br />

Pseudorange<br />

The apparent distance from a satellite to <strong>the</strong> phase<br />

centre <strong>of</strong> a <strong>GNSS</strong> receiver antenna. This is<br />

computed from <strong>the</strong> C/A or P code which gives a<br />

signal propagation time. This time can <strong>the</strong>n be<br />

multiplied by <strong>the</strong> speed <strong>of</strong> light to give an apparent<br />

distance, which is not <strong>the</strong> true distance.<br />

Pseudorange differs from <strong>the</strong> actual range by <strong>the</strong><br />

amount that <strong>the</strong> satellite <strong>and</strong> <strong>use</strong>r clocks are <strong>of</strong>fset,<br />

by propagation delays, <strong>and</strong> o<strong>the</strong>r errors. The<br />

apparent propagation time is determ<strong>in</strong>ed from <strong>the</strong><br />

time shift required to align (correlate) a replica <strong>of</strong><br />

<strong>the</strong> <strong>GNSS</strong> code generated <strong>in</strong> <strong>the</strong> receiver with <strong>the</strong><br />

70 | GUIDELINES FOR THE USE OF <strong>GNSS</strong> IN LAND SURVEYING AND MAPPING

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