based upon GNSS, is almost infinite. The
requirements of these systems with respect to the
positioning information provided by the positioning
terminal can vary from decimetres to hundreds of
metres, depending on the application. Some of these
systems are critical in terms of the need for safety,
liability or security, and they depend on accurate and
reliable positioning information to function
effectively. For ITSs and LBSs, a standard in 2015
is a single-frequency GPS L1 receiver, with
increasing SBAS and dual-constellation (with
GLONASS) capabilities. LBS receivers
(smartphones) are also often assisted (A-GNSS) by
and even hybridized with positioning based on
communication networks. The ability to use multiple
GNSSs improves the accuracy, integrity and
availability of positioning, especially in urban areas.
There is a very large offer of different types of
GNSS receivers today, with highly variable
performances and costs. The performance of a
GNSS may be improved by data fusion, namely by
integrating sensor measurements, other positioning
means or a priori data such as digital data bases.
This data fusion brings enhancement at three levels:
(1) standard position, velocity and time (PVT) are
improved in terms of availability, accuracy, and
integrity; (2) additional information, such as attitude
angles, may be provided, and (3) the output rate is
increased by one or two orders of magnitude. One of
the most influential trends in GNSS is the use of
multiple systems to achieve better error mitigation
(e.g. multipath), resistance to interference and
positioning accuracy. Ground and satellite based
augmentation systems will also be used more in the
future to improved position accuracy and integrity.
Furthermore, in this project we will consider cyber
and information security in an augmented GNSS,
which may influence PVT.
The GNSS positioning principle relies on
trilateration by which an unknown point location
(receiver) is estimated using distance measurements
observed from known point locations
(satellites)(Groves, 2013). The basic observable of
the system is the travel time required for a signal to
propagate from the satellite to the receiver
multiplied by the speed of light to compute distance.
The receiver could then be located anywhere on the
surface of a sphere centered on the satellite with a
radius that equals this distance. The quality of raw
GNSS observables is affected by several factors
originating from satellites, signal propagation, and
receivers. The signal transmitted by a satellite
propagates through the atmosphere, where it is
subject to delays caused by the ionosphere and
troposphere. The effects of these delays are only
partially compensated for by global models in single
frequency receivers.
At the ground level, multipath, namely the
reception of signals reflected from objects like
buildings surrounding the receiver, can occur,
inducing one of the largest errors that is difficult to
model, as it is strongly depends on the receiver
environment. The worst situations are experienced
when only reflected signals are received (non-line-
of-sight signals, or (NLOS) signals, resulting in
pseudo-range errors of several tens of metres or
greater in extreme cases.
Finally, random errors are encountered at the
receiver level due to receiver thermal noise. The
receiver clock offset (much larger than that of the
satellite) does not create any error, since it is
considered as an unknown and is calculated together
with the position. The position error that results from
the measurement errors above, which is referred to
as dilution of precision (DOP) depends also on the
relative geometry between the receiver and the
satellites. Accuracy is maximized when the
directions to tracked satellites are more uniformly
spread around the receiver.
The main task of a GNSS is to provide
localization and time synchronization services.
There are multiple GNSS systems available. The
most well-known one is the global positioning
system (GPS). GPS data is transmitted via
coarse/acquisition (C/A) code, which consists of
unencrypted navigation data. The encrypted
(military) signal is called the precision-code, which
is also broadcast by every satellite. It has it is own
PRN codes, but it is in the order of 1012 bits long.
When locked onto the signal, the receiver receives
the Y code, which is an encrypted signal with an
unspecified W code (Loukas et al., 2013;
Humphreys, 2013). Only authorized users can
decipher this. In later GPS satellites, extra features
were added (Radoslav et al., 2014; Uma and
Padmavathi, 2013). There are several methods of
augmenting GNSS data to get better estimates of
location. Three of these are satellite-based
augmentation systems (SBASs), assisted-GPS, and
differential-GPS. SBASs were the first type to be
developed; these systems are commonly used in
airplanes, for critical phases such as the landing
phase. They consist of a few satellites and many
ground stations. A SBAS covers a certain GNSS for
a specific area, and for every GNSS, accuracy
depends heavily on, and is influenced by external
factors (Grove, 2013). These factors affect not only
GNSS applications, but also every other wireless
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