THE conventional geomatics industry
including mapping and surveying
applications has been revolutionized with
the use of GPS, which is the best known,
and currently fully operational satellite
based navigation system operated by USA
(Parkinson, and Spilker Jr., 1995). In the
mean time, Russia also operates its own
satellite based navigation system called
GLONASS. The USA is modernizing
GPS in order to retain its superiority in
satellite based navigation technologies
(MacDonald, 2002,). In order to keep
up with USA’s progress in building next
generation system, Russia is taking
serious steps to modernize GLONASS
as well (Federal Space Agency for the
Russian Federation, 2005). The GPS
and GLONASS signals are free but its
availability is not guaranteed and currently
most users are prepared to accept this
risk (Parkinson, and Spilker Jr., 1995).
However, as satellite navigation becomes a
vital technology across a number of critical
industrial sectors, the prospect of, for
example, a nation’s transport infrastructure
becoming dependent on this technology
is a strategic risk that most industrial
countries are not willing to accept. This
argument initiated the Galileo program in
Europe. Therefore, those systems form the
mainframe of Global Navigation Satellite
Systems (GNSS) (MacDonald, 2002,).
Unlike GPS, Galileo will also offer a
guaranteed service to users who are willing
to pay for it (e.g. commercial service
– CS, and Public Regulated Service
PRS) in addition to a free signal similar
to that of GPS (Open Service - OS and
Safety of Life service - SoL). Galileo
will be available to the public in 2012
(European Commission, 2003). Despite
many technical differences between these
three GNSS systems, the commonality of
the carrier frequencies they use creates
the potential for the future development
of an interoperable GNSS receiver.
The vast majority of the world will be
users of these existing systems. The
fundamental questions then are: “Which
system or systems should a country use?”;
“How to choose a combination of the
systems?”; “What are the benefi ts and
respective merits of those systems?” There
is no simple answer to these questions, as
the best solution will undoubtedly depend
on the targeted application, which has its
own requirements in terms of accuracy,
reliability, robustness, cost and other
application-specifi c criteria. What can be
provided, however, is a means whereby
parameters that describe these performance
requirements can be computed.
Comparing those pricy hardware GNSS
simulators, high-accuracy software
simulations are a cost-effective and
precise tool to evaluate the performance
characteristics attainable from the future
GNSSs, and have been recognized as
an appropriate pre-development tool
for satellite navigation systems and
applications in Canada and European
countries. In addition, the entire hardware
simulators available on the market can only
emulate the signals from a single system at
the present time. On the other hand, a dual
systems simulator is easier to implement in
the software level. The technical benefits of this approach lie in the fact that the
software simulations are reproducible
and totally controlled, and parameters
can be changed individually if necessary
for an in-depth understanding of the
underlying effects. This paper introduces a
qualitative assessment of the performance
characteristics of the future GNSS
infrastructure around Taiwan area using a
multi-system software simulation toolkit
being developed; therefore, representative
results over Taiwan are demonstrated.
Evolving From GPS
to Future GNSS
GPS Modernization
Motivated by the United States Department
of Defense (DoD), the current GPS has
experienced three decades’ development.
Although the original motivation was
only for military purposes, GPS has
been widely used in civilian applications
during the past few decades. However,
the integrity, availability, and accuracy
still need further improvement for
various applications. For the surveying
industry, applications can be classifi ed
according to the achievable accuracy:
Single Point Positioning (SPP) is the
technique for which GPS was originally
designed and delivers the Standard
Positioning Service (SPS) performance
mentioned above. Differential GPS
(DGPS) can overcome some of
the limitations of GPS by applying
corrections to the basic pseudorange
measurements, based on a receiver
making measurements at a known point
(a reference station). The accuracy
achievable from DGPS can range from
a few meters down to few decimeters,
depending on the quality of the
receiver and the DGPS technique used
(Parkinson, and Spilker Jr., 1995).
GPS Surveying also works differentially
but can achieve centimeter accuracy
using a special measurement technique.
A typical receiver, for both SPP and
DGPS1, measure the ranges to the
satellites by timing how long the signal
takes to come from the satellite (the
pseudorange, referred to as such because
this measurement is contaminated by the receiver clock error) (Lachapelle, 2002).
However, receivers used in surveying
and geodesy measure the phase of the
underlying carrier wave signal (the
so-called carrier phase). For baselines
between points separated by more than
20km, it is important that such receivers
can also correct for the ionosphere
(Lachapelle, 2002). For shorter
baselines, dual-frequency receivers are
necessary for rapid initialization of cmlevel
positioning. Given that civilians
users only have access to the SPS,
surveying receivers employ sophisticated
signal processing techniques to measure
the phase of the L2 signal. This level
of sophistication is a major reason why
surveying receivers are more expensive
than receivers used for SPP and DGPS.
Therefore, a GPS modernization program
was initiated in the late 1990’s, in an
attempt to upgrade GPS performance for
both civilian and military applications.
The GPS modernization program started
with the cancellation of SA in 2000. It will
be followed by the addition of a new a
second civil code on L2 (L2C), then a third
civil frequency L5. Further modernization
consists of the assessment and design
of a new generation of satellites to meet
military and civil requirements through
2030. Table1 includes a summary of the
launch schedule of the modernized GPS
satellites according to MacDonald (2002).
GPS Block IIR-M is the second part of
Block IIR, with eight modernized satellites
being built by Lockheed Martin. The IIRM
satellites will have a new civil signal
on L2 at higher signal power than normal
IIR satellites. The Boeing Company has
the contract for GPS Block IIF, with nine
satellites in total that are intended to provide
improved anti-jam capability, increased
accuracy, higher integrity, and secured
operational M-codes. Additionally, a third
civil code at a new frequency L5 will also
be included. The purpose of the GPS III
program is to deliver major improvements
in accuracy, assured service, integrity,
and fl exibility for civil users. Currently
led by both Lockheed Martin and Boeing
both, the team of GPS III program has
proposed the use of the same signal
structure as Galileo for its open signals and decided the year 2012 as the target date
of the launch of fi rst GPS III satellite.