<?xml version="1.0" encoding="UTF-8"?><?xml-stylesheet type="text/xsl" href="static/CINECAstyle.xsl"?><OAI-PMH xmlns="http://www.openarchives.org/OAI/2.0/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/ http://www.openarchives.org/OAI/2.0/OAI-PMH.xsd"><responseDate>2026-09-22T18:03:50Z</responseDate><request verb="GetRecord" identifier="oai:iris.polito.it:11583/2513765" metadataPrefix="oai_dc">https://iris.polito.it/oai/request</request><GetRecord><record><header><identifier>oai:iris.polito.it:11583/2513765</identifier><datestamp>2023-05-17T00:57:06Z</datestamp><setSpec>com_11583_2614433</setSpec><setSpec>com_11583_2614425</setSpec><setSpec>col_11583_2614423</setSpec></header><metadata><oai_dc:dc xmlns:oai_dc="http://www.openarchives.org/OAI/2.0/oai_dc/" xmlns:doc="http://www.lyncode.com/xoai" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:dc="http://purl.org/dc/elements/1.1/" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/oai_dc/ http://www.openarchives.org/OAI/2.0/oai_dc.xsd">
<dc:title>High-performance velocity, frequency and time estimation using GNSS</dc:title>
<dc:creator>UGAZIO, SABRINA</dc:creator>
<dc:contributor>Ugazio, Sabrina</dc:contributor>
<dc:subject>GNSS</dc:subject>
<dc:subject> Frequency</dc:subject>
<dc:subject> Velocity</dc:subject>
<dc:subject> Time</dc:subject>
<dc:subject> Software Receiver</dc:subject>
<dc:subject> Adaptive Phase Lock Loop</dc:subject>
<dc:subject> Rubidium</dc:subject>
<dc:subject> Ionosphere</dc:subject>
<dc:subject> TEC</dc:subject>
<dc:subject>Settore ING-INF/03 - Telecomunicazioni</dc:subject>
<dc:description>GNSS (Global Navigation Satellite System) receivers provide PVT solution,
where PVT stands for Position, Velocity and Time. In general, the main interest
of the common GNSS user is on the position solution and as a consequence the
main focus of the research is the improvement of the position solution accuracy.
However, many applications exist in which the measurement of both velocity
and/or time is crucial and this is the reason why the focus of this thesis is on
the Velocity and Time solution.
The PVT solution is computed through trilateration techniques, based on a TOA
(Time Of Arrival) ranging technique, therefore the PVT solution is correlated
to the measurement of time. In particular, the position solution is related to a
time measurement while the velocity solution is correlated to a frequency measurement.
Different factors that affect the velocity estimate on one side and the time estimate
on the other side are taken into account in this thesis, that in classic PVT
solution are usually neglected.
In the velocity/frequency estimate, the significant measurement is the change in
the user-satellite distance, i.e. a relative measurement, thus the measurements
errors that remain constant during the time interval over which the velocity is estimated
cancel out. Carrier-phase difference solution enables velocity accuracy in
the order of 1 mm/s, a high-level accuracy which is crucial for many applications,
including Inertial Measurement Unit (IMU) calibration, motion compensation for
Synthetic Aperture Radar (SAR) and flight reference systems. Thanks to the
cancellation of the common errors, that in the position solution represents the
very larger error sources, in the velocity solution other minor effects become the
limiting error sources. The first goal investigated in this thesis is to look for the
accuracy limit that can be achieved in the velocity/frequency solution.
The second objective is to investigate the problem of high- accuracy time solution.
As well as the position, the time is an absolute measurement, affected
by large error sources. Furthermore, the clock error is in common to all the
satellite measurements, and due to this, the common errors among the satellites
are not told apart and are in general attributed to the clock measurement. As a
result, lots of error sources that are not involved in the position solution become
dominant in the time solution. A main limiting factor in the timing accuracy is
represented by the errors in ionospheric delay estimate, where many error sources
are involved, in particular the unknown bias due to the receiver hardware.
After a part to introduce GNSS and its basic principles, with the focus on the
aspects that are more relevant for the dissertation and that allow one to outline
the motivations of the work, the thesis is divided in three main parts, two regarding
in particular the velocity/frequency solution and the last one focused on
the high-accuracy time solution.
The first step to improve the velocity solution was to notice how the performance
is much worse on the vertical solution than on the horizontal and how highly correlated
the vertical solution is to the local frequency estimate. This is due to the
geometry of GNSS, that implies that users on the Earth or close to the Earth
(as aircrafts) can see satellites all around them on the horizontal direction, but
they cannot see satellites under them, which is rejected in a poorer geometry on
the vertical direction. Due to this characteristic, an error on the pseudorange, as
the clock error is, reflects on the vertical solution more heavily than on the other
dimensions. As a result, the vertical solution can be about three times worse
than the horizontal and from the covariance matrix of the solution it can be
seen how the correlation is high in particular between the vertical and the clock
solution. This fact is true both for the position and for the velocity solution,
which means that the vertical velocity accuracy is highly correlated to the local
oscillator frequency. As a result, a way to improve the vertical velocity accuracy
is to obtain a better estimate of the local frequency. In this thesis, models for
the local oscillators and ways to integrate the frequency estimate in the GNSS
solution are investigated.
Another important aspect to improve the performance of the velocity measurement
is to improve the accuracy of the GNSS measurement. Since the measurement
used to obtain precise velocity is the carrier phase, which enables accuracy
in the order of 1 mm/s, the goal to improve the accuracy on the carrier-phase
measurement is crucial. With this objective, novel Digital Phase Lock Loops (DPLLs) has been designed, both of second and third order, with an adaptive
bandwidth algorithm. The objective was to tune the loop bandwidth according
to the input signal dynamics and noise, and use a bandwidth small enough to
reduce the noise effects as much as possible, but wide enough to properly track
the input dynamics. Since the PLL is designed for precise velocity measurement,
the performance in terms of dynamics tracking ability is crucial.
The last part of the analysis concerns the time solution. In most of cases in
GNSS, high importance is given to the position accuracy, while the residual
common biases are included in the receiver clock error. This approach makes
the time solution not very accurate. Since the main bias which affects the time
solution is the ionosphere delay, in this thesis the accuracy of the Total Electron
Content (TEC) estimate is investigated, with the focus on the measurement bias.
All the measurements which this thesis refers to are made using GPS (Global
Positioning System) only, nevertheless sometimes in the thesis it is talked about
GNSS in general. This is because the approaches considered in this thesis are
tested here using GPS, but they can be applied to all the GNSSs.</dc:description>
<dc:date>2013</dc:date>
<dc:type>info:eu-repo/semantics/doctoralThesis</dc:type>
<dc:identifier>http://hdl.handle.net/11583/2513765</dc:identifier>
<dc:identifier>10.6092/polito/porto/2513765</dc:identifier>
<dc:language>eng</dc:language>
<dc:relation>numberofpages:259</dc:relation>
<dc:rights>info:eu-repo/semantics/openAccess</dc:rights>
<dc:format>STAMPA</dc:format>
<dc:publisher>Politecnico di Torino</dc:publisher>
<dc:publisher>country:Italy</dc:publisher>
<dc:rights>license:Creative commons</dc:rights>
<dc:rights>license:Creative commons</dc:rights>
<dc:rights>license:Creative commons</dc:rights>
<dc:rights>license:Creative commons</dc:rights>
<dc:rights>license uri:http://creativecommons.org/licenses/by/3.0/it/</dc:rights>
<dc:rights>license uri:http://creativecommons.org/licenses/by/3.0/it/</dc:rights>
<dc:rights>license uri:http://creativecommons.org/licenses/by/3.0/it/</dc:rights>
<dc:rights>license uri:http://creativecommons.org/licenses/by/3.0/it/</dc:rights>
</oai_dc:dc></metadata></record></GetRecord></OAI-PMH>