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Guidelines for the use of GNSS in surveying and mapping

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GPS (Global Position<strong>in</strong>g System)<br />

The United States <strong>GNSS</strong> system.<br />

GPS-ICD-200<br />

The GPS <strong>in</strong>terface control document is a US<br />

government document that conta<strong>in</strong>s <strong>the</strong> full<br />

technical description <strong>of</strong> <strong>the</strong> <strong>in</strong>terface between <strong>the</strong><br />

satellites <strong>and</strong> <strong>the</strong> <strong>use</strong>r. GPS receivers must comply<br />

with this specification if <strong>the</strong>y are to receive <strong>and</strong><br />

process GPS signals properly.<br />

GPS week<br />

GPS time started at Saturday/Sunday midnight on<br />

6 January 1980 <strong>and</strong> <strong>the</strong> weeks are numbered from<br />

that date, up to 1024 weeks. The first week<br />

‘rollover’, <strong>the</strong> start <strong>of</strong> <strong>the</strong> next renumber<strong>in</strong>g,<br />

occurred on 21 August 1999.<br />

Gravitational constant<br />

The proportionality constant <strong>in</strong> Newton’s Law <strong>of</strong><br />

Gravitation is G = 6.672 x 10 -11 m 3 kg -1 s -2 .<br />

Half-wave<br />

Measurements made us<strong>in</strong>g L2 squared<br />

measurements. The squar<strong>in</strong>g process results <strong>in</strong> only<br />

half <strong>of</strong> <strong>the</strong> orig<strong>in</strong>al L2 wavelength be<strong>in</strong>g available, a<br />

doubl<strong>in</strong>g <strong>of</strong> <strong>the</strong> orig<strong>in</strong>al L2 frequency.<br />

HDOP (Horizontal dilution <strong>of</strong> precision)<br />

See DOP <strong>and</strong> PDOP.<br />

Height – ellipsoidal<br />

The distance above or below <strong>the</strong> ellipsoid<br />

measured along <strong>the</strong> normal to <strong>the</strong> ellipsoid at that<br />

po<strong>in</strong>t. Not <strong>the</strong> same as elevation above sea level.<br />

<strong>GNSS</strong> receivers output position-fix height as <strong>the</strong><br />

height above <strong>the</strong> ITRS89 ellipsoid.<br />

HOW (H<strong>and</strong>over word)<br />

The word is <strong>the</strong> <strong>GNSS</strong> message that conta<strong>in</strong>s time<br />

synchronisation <strong>in</strong><strong>for</strong>mation <strong>for</strong> <strong>the</strong> transfer from <strong>the</strong><br />

C/A code to <strong>the</strong> P-code.<br />

IERS<br />

International Earth Rotation Service.<br />

Initialisation<br />

The moment when a rover <strong>GNSS</strong> receiver <strong>in</strong> a high<br />

precision real-time dynamic system (RTK) solves<br />

<strong>the</strong> <strong>in</strong>teger ambiguity <strong>and</strong> ga<strong>in</strong>s a real-time high<br />

precision fixed basel<strong>in</strong>e solution.<br />

Integer bias search<br />

The biases calculated <strong>in</strong> <strong>the</strong> float solution are fixed<br />

to <strong>in</strong>tegers. A search is <strong>the</strong>n undertaken to f<strong>in</strong>d<br />

closely related sets <strong>of</strong> <strong>in</strong>tegers. These sets are<br />

compared to <strong>the</strong> <strong>in</strong>itial set by divid<strong>in</strong>g <strong>the</strong> sum <strong>of</strong><br />

<strong>the</strong> squares <strong>of</strong> residuals <strong>of</strong> <strong>the</strong> trial set by that <strong>of</strong><br />

<strong>the</strong> orig<strong>in</strong>al set. A strong data set allows only one<br />

set <strong>of</strong> <strong>in</strong>tegers, <strong>and</strong> produces a ratio factor greater<br />

than 3.0. A weak data set may accept several<br />

different sets <strong>of</strong> <strong>in</strong>tegers with only small changes <strong>in</strong><br />

its sum <strong>of</strong> <strong>the</strong> squares fit, thus produc<strong>in</strong>g a small<br />

ratio factor.<br />

Integer bias terms<br />

The receiver counts <strong>the</strong> radio waves from <strong>the</strong><br />

satellite, as <strong>the</strong>y pass <strong>the</strong> antenna, to a high degree<br />

<strong>of</strong> accuracy. However, it has no <strong>in</strong><strong>for</strong>mation on <strong>the</strong><br />

number <strong>of</strong> waves to <strong>the</strong> satellite at <strong>the</strong> time it<br />

started count<strong>in</strong>g. This unknown number <strong>of</strong><br />

wavelengths between <strong>the</strong> satellite <strong>and</strong> <strong>the</strong> antenna<br />

is <strong>the</strong> <strong>in</strong>teger bias term.<br />

Integrated Doppler<br />

A measurement <strong>of</strong> Doppler shift frequency <strong>of</strong> phase<br />

over time.<br />

Ionospheric delay<br />

The ionosphere is a non homogeneous (both <strong>in</strong><br />

space <strong>and</strong> time) <strong>and</strong> dispersive medium. A wave<br />

propagat<strong>in</strong>g through <strong>the</strong> ionosphere experiences<br />

variable delay. Phase delay depends on electron<br />

content <strong>and</strong> affects carrier signals. Group delay<br />

depends on dispersion <strong>in</strong> <strong>the</strong> ionosphere as well,<br />

<strong>and</strong> affects signal modulation. The phase <strong>and</strong><br />

group delay are <strong>of</strong> <strong>the</strong> same magnitude but<br />

opposite sign.<br />

ITRF (International terrestrial reference frame)<br />

See Reference frame.<br />

JPO<br />

Jo<strong>in</strong>t Program Office <strong>for</strong> GPS located at <strong>the</strong> USAF<br />

Space Division at El Segundo, Cali<strong>for</strong>nia. The JPO<br />

consists <strong>of</strong> <strong>the</strong> USAF Program Manager <strong>and</strong><br />

Deputy Program Managers represent<strong>in</strong>g <strong>the</strong> Army,<br />

Navy, Mar<strong>in</strong>e Corps, Coastguard, National Imagery<br />

<strong>and</strong> Mapp<strong>in</strong>g Agency (NIMA) <strong>and</strong> NATO.<br />

Kalman filter<br />

A numerical method <strong>use</strong>d to track a time-vary<strong>in</strong>g<br />

signal <strong>in</strong> <strong>the</strong> presence <strong>of</strong> noise. If <strong>the</strong> signal can be<br />

characterised by some number <strong>of</strong> parameters that<br />

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

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