89
The precise orbit and clock corrections used in the
XP system are determined in cooperation with Na-
tional Aeronautics and Space Administration
(NASA) Jet Propulsion Laboratory (JPL) based on
NASA’s worldwide network of reference stations.
The PPP method used in the XP system involves
using the satellite specific precise orbit and clock
corrections instead of virtual reference station range
corrections. These corrections represent the most ac-
curate estimate of the errors of the GNSS satellites
broadcast orbit and clocks. Unlike the corrections
used in the multiple reference station HP method,
which are reference station and satellite specific, the
orbit and clock corrections used in the PPP XP
method are satellite specific only and not location
dependent. The positioning accuracy is no longer
limited by the distance from the reference stations.
Therefore, application of these corrections leads to
virtually homogeneous high positioning accuracy
worldwide.
Typical 24 hour monitoring results from the XP
system operating in dynamic mode at Lafayette,
USA, on the Gulf of Mexico coast, as observed on
January 23, 2011 are shown in Figure 3. The posi-
tion accuracy given in terms of standard deviation is
4, 3, and 8 cm, for longitude, latitude and height, re-
spectively.
Figure 3. XP Position Results, Lafayette, January 23, 2011
XP solution was also extensively tested at various
locations and over an extended time. The results of
these tests showed that the XP solution provides 10
cm horizontal, 20 cm vertical accuracies in terms of
95% statistics. Unlike HP, the accuracy of XP is not
dependent on location and distance from the refer-
ence stations.
5 GLONASS AUGMENTED PRECISE POINT
POSITIONING G2
Fugro introduced in 2009 truly the next generation
multi constellation real-time PPP system, based on
the use of precise GPS and GLONASS orbit and
clock corrections, called G2 (Melgard et al, 2009).
The development has benefited from the close coop-
eration between Fugro and the European Space Op-
eration Centre (ESOC), an establishment of the Eu-
ropean Space Agency (ESA). ESOC has contributed
with their expertise on precise orbit and clock pro-
cessing techniques while Fugro built an operational
real time system.
G2 position solution uses the PPP method with fi-
ne tuned statistical models to process GPS and
GLONASS satellite observations and precise orbits
and clock corrections determined from the global G2
network. These corrections are satellite specific only
and not location dependent, similarly to XP. There-
fore, the application of these corrections in a G2 user
solution leads to virtually homogeneous high posi-
tioning accuracy worldwide
The G2 service utilizes Fugro’s network of dual
system GNSS reference stations to calculate precise
orbits and clocks on a satellite by satellite basis for
all 50 plus satellites of the two global navigation sat-
ellite systems. The system comprises about 40 dual-
frequency GPS and GLONASS reference stations,
operated independently of HP and JPL networks,
evenly distributed around the world.
Successful integration of GLONASS carrier
phase observations in G2 solution required account-
ing for incompatibilities between GPS and
GLONASS systems. GLONASS satellites, unlike
GPS, use different satellite specific frequencies. Al-
so, GLONASS observations refer to different time
system than GPS. However, after accounting for the-
se differences GLONASS satellites act like addi-
tional GPS satellites in G2 solution.
Including GLONASS together with GPS satel-
lites improves redundancy, geometry and availabil-
ity of a positioning solution. Because of the greater
number of satellites and improved geometry, inte-
grated GPS and GLONASS G2 solution offers faster
convergence than GPS only solution (Melgard et.al,
2009). Additional GLONASS satellites offer the po-
tential to enable a positioning solution that may not
be possible with GPS only, especially in challenging
tracking environments with line of sight obstructions
such as depicted in Figure 4.