165
1 INTRODUCTION
New shipping routes are emerging as a result of
icebergs melting in polar regions, allowing for more
efficient transport of people and goods. The opening
of the Northwest Passage, the maritime route
connecting the Pacific Ocean with the Atlantic Ocean
through the Arctic region, is considered such a
development [8]. The Northwest Passage location in
polar region renders satellite navigation, as a
navigation-supporting technology, vulnerable to
space weather effects [1]. Space weather is defined as
a set of conditions and events of variable energy
transfer originated in the Sun and spread through the
Modelling GPS Positioning Performance in Northwest
Passage during Extreme Space Weather Conditions
D. Špoljar
1,2
, O. Jukić
3
, N. Sikirica
2
, K. Lenac
1
& R. Filjar
1,2,3
1
University of Rijeka, Rijeka, Croatia
2
Krapina University of Applied Sciences, Krapina, Croatia
3
Virovitica University of Applied Sciences, Virovitica, Croatia
ABSTRACT: New shipping routes are emerging as a result of iceberg melting in polar regions, allowing for
more efficient transport of people and goods. Opening of the Northwest Passage, the maritime route connecting
Pacific Ocean with Atlantic Ocean through Arctic region, is considered such a development. The increasing
transport exploitation of the Northwest Passage requires the quality assessment of maritime navigation aids for
compliance with the established requirements. Here we contribute to the subject with addressing the polar
commercial-grade GPS positioning performance in the Northwest Passage in the extreme positioning
environment conditions during the massive 2003 space weather storm, a space weather event similar to the
Carrington Storm of 1859, the largest space weather event recorded. The GPS positioning environment in the
Northwest Passage during the Carrington-like storm in 2003 was reconstructed through the GNSS SDR
receiver-post processing of the experimental GPS observations. The raw GPS dual-frequency pseudoranges and
navigation messages were collected at the International GNSS Service (IGS) reference station at Ulukhaktok,
Victoria Island, Canada. Pseudorange processing and GPS position estimation were performed in three
scenarios of pre-mitigation of the ionospheric effects, known as the single major contributor GPS positioning
error: (i) no corrections applied, (ii) Klobuchar-based corrected GPS positioning, and (iii) dual-frequency
corrected GPS positioning. Resulting GPS positioning error vectors were derived as positioning error residuals
from the known reference station position. Statistical properties of the northing, easting, and vertical
components of the GPS positioning error vector were analyzed with a software developed in the R environment
for statistical computing to select suitable methods for the GPS positioning error prediction model
development. The analysis also identified the most suitable theoretical fit for experimental statistical
distributions to assist the model development. Finally, two competitive GPS positioning error prediction
models were developed, based on the exponential smoothing (reference) and the generalized regression neural
networks (GRNN) (alternative) methods. Their properties were assessed to recommend their use as mitigation
methods for adverse massive space weather effects in polar regions.
http://www.transnav.eu
the International Journal
on Marine Navigation
and Safety of Sea Transportation
Volume 15
Number 1
March 2021
DOI: 10.12716/1001.15.01.16
166
Earth’s surroundings that can affect space-borne and
ground-based technological systems. Geomagnetic
storms represent extreme forms of space weather that
can affect radio wave propagation across the
spectrum, degrading the positioning performance of
the Global Navigation Satellite System (GNSS) and
reducing the quality of the GNSS-based applications
[1, 7]. Here we address the effects of the 2003
geomagnetic storm on the polar commercial-grade
GPS positioning performance in the Northwest
Passage. The 2003 extreme space weather event, also
known as the ‘Halloween Storm’, is often compared to
the Carrington Storm of 1859, by far the largest solar
storm recorded [1, 2]. Considering the expected
increase in maritime traffic in the Northwest Passage
with the extensive utilization of satellite navigation
on-board the vessels, this study aimed at assessment
of the GPS positioning performance using the
common on-board equipment and compliance with
the requested and required GPS positioning
performance [4]. The study results with the
recommendation proposal to mitigate GNSS
positioning degrading ionospheric delay effects of
massive space weather developments on satellite
navigation performance in the polar region
2 METHOD AND MATERIAL
The GPS positioning environment in the Northwest
Passage during the Carrington-like storm in 2003 was
reconstructed throuvenrgh the GNSS SDR receiver-
post processing of the experimental GPS observations
taken in the region during the space weather event [3,
5, 7]. The research aims at addressing the excess GNSS
ionospheric delay caused by considerable space
weather event, and its contribution to the over-all
GNSS positioning error. As the result, a prognostic
model is to be developed to forecast the GPS
positioning error during a massive space weather
deterioration in the region of Northwest Passage. It
should be noted that we consider the other sources of
GPS positioning errors (multipath, GPS tropospheric
delay etc.) of the unchanged (unaffected) nature.
Additionally, while the research focuses on the GPS
ionospheric delay, we do not consider effects of the
GPS ionospheric scintillation in this research.
Observations were collected of raw (uncorrected) GPS
dual-frequency pseudouranges and GPS navigation
messages broadcast at the International GNSS Service
(IGS) reference station at Ulukhaktok, formerly
Holman, Victoria Island, Canada (latitude:
70.7364000N, longitude: 117.7609000W, 39.5 m above
the mean sea level), and made available through the
IGS internet archives
(ftp://cddis.nasa.gov/gnss/data/daily). The IGS is set to
assist scientists and the other interested parties with
the provision of the GNSS pseudoranges uncorrected
for ionospheric effects to allow for research into the
ionospheric effects on GNSS performance and
operations. Nominally established to provide with
daily records of observed raw (uncorrected) GNSS
pseudoranges at 30 s sampling time, the reference
stations may occasionally provide reduced sets of
observations, and/or present observations in faulty
and inconsistent manner. External events may also
cause tempral suspension of pseudorange collection.
In an approach similar to the essence of differential
GNSS, we consider the GNSS ionospheric delay to be
approximately constant in the bounded region around
the observation site, thus allowing the generalisation
of the observed ionospheric delay effects on GNSS
performance at stationary site to be applicable on the
near-by dynamical environment of mobile maritime
objects (vessels).
We used the Ulukhaktok (Holman) GPS pseudorange
observations from the period DOY298 (25
th
October)
DOY315 (11
th
November) in 2003 to cover the most
intensive phase of the largest space weather event
observed in modern history. Pseudorange processing
and GPS position estimation were performed in three
scenarios of pre-mitigation of the ionospheric effects,
known as the single major contributor to GPS
pseudorange measurement error, and, consequently,
GPS positioning error: (i) GPS positioning exposed to
ionospheric effects, with no corrections applied, (ii)
Klobuchar-based corrected GPS positioning, as
defined with (1) using the GPS-broadcast correction
model parameters (αi,βi,i = 1,…,4) and (iii) dual-
frequency corrected GPS positioning procedure
utilizing pseudorange measurements ρ(f1) and ρ(f2) on
carrier frequencies f1 and f2, respectively, taken
instantaneously, to obtain TEC, and consequently the
GPS pseudorange observations freed from the first-
order ionospheric effects (2).
( ) ( )
( )
( )
( ) ( )
0
33
00
2
cos , day
,
iono
nn
n m n m
nn
tt
t t DC A
P
AP
==

= +



==

(1)
(2)
In the Klobuchar model (1), symbols may be
identified as follows: DC = 5e-9 s, A(φ) denotes
amplitude of the day-time cosine component of the
GPS ionospheric delay, determined with the GPS-
broadcast (αi, i = 1, …, 4) parameters and the user
position’s geomagnetic latitude, P(φ) denotes period
of the day-time cosine component of the GPS
ionospheric delay, determined with the GPS-
broadcast (αi, i = 1,…, 4) parameters and the user
position’s geomagnetic latitude, t denotes the time
instant for which the GPS ionospheric delay is
determined in [s], and t0 = 14 hours local time in [s],
and tiono(t) denotes the resulting GPS ionospheric time
delay in [s] at the time instant t.
Position estimates were obtained using the open
source GNSS Software-Defined Radio receiver
RTKLIB (developed by Dr T Takasu, available form:
http://www.rtklib.com). Resulting GPS positioning
error vectors were derived as positioning error
residuals from the known reference station position.
Statistical properties of the northing, easting, and
vertical components of the GPS positioning error
167
vector were analyzed with a tailored software
developed by these authors in the R environment for
statistical computing to improve the understanding of
the positioning error generation process, and to select
suitable methods for the GPS positioning error
prediction model development [3].
We deployed the Cullen and Fray method to
estimate the theoretical statistical distribution of
closest fit to the experimental one, derived from the
GPS position error estimates. Developed by Pearson,
and described later by Cullen and Fray, the method
extend the suggestion for the best fit. We conduct the
actual analysis using the bespoke software developed
in the R environment for statistical computing, and its
external package fitdistrplus [9].
The analysis identified the most suitable
theoretical fit for experimental statistical distributions
to assist the model development. Finally, two
competitive GPS positioning error prediction models
were developed, based on the exponential smoothing
(reference) and the Generalized Regression Neural
Networks (GRNN) [6] (alternative) methods. Model
development and properties assessment were
performed using a tailored software developed in the
R environment for statistical computing to
recommend the utilization for mitigation of
contribution to GPS positioning performance
deterioration of the excessive GPS ionospheric delay
caused by adverse massive space weather effects in
polar regions.
Performance analysis of the models developed was
based on the analysis of residuals, obtained as a
difference between the model-based position forecast
in the particular scenario (i) (iii) , and th etrue
position of the reference station.
3 RESEARCH RESULTS
The methodology described in the previous Section
was applied on the Ulukhaktok GPS raw pseudorange
data, taken during the Carrington-like space weather
storm of 2003. As a result, insight was gained into
statistical properties of the northing, easting, and
vertical components of the GPS positioning vectors, in
three scenarios of the ionospheric effects mitigation,
as depicted in Figures 1. (for all ionospheric
mitigation scenarios), and 2. (no-corrections
ionospheric mitigation scenario only).
The most suitable theoretical statistical distribution
to fit the experimental one was selected using the
Cullen & Fray diagram, as shown in Figure 3. for the
northing component of the GPS positioning vector in
the no-correction scenario.
A time series of horizontal GPS positioning errors
was constructed from time series of northing and
easting positioning errors. Using the horizontal GPS
positioning error time series, two candidate
prediction model development methods were selected
and tuned, i.e., the exponential smoothing and the
generalized regression neural networks (GRNN), to
develop candidate models of the horizontal GPS
positioning error. The original time series of 2872
single-point horizontal GPS positioning errors was
split into the first 2857 elements training set, and the
remaining 15 elements test set to assess the prediction
models performance.
Figure 1. Exploratory analysis results of the components of
the GPS positioning error vector in the ionospheric effects
mitigation scenarios of (i) no correction (no), (ii) broadcast
Klobuchar corrections (Kl), and (iii) dual-frequency
correction
Figure 2. Experimental statistical distribution density
functions for the northing, easting, and vertical components
of the GPS positioning error vector in the no-correction
ionospheric effects mitigation scenario
The most suitable theoretical statistical distribution
to fit the experimental one was selected using the
Cullen & Fray diagram, as shown in Figure 3. for the
northing component of the GPS positioning vector in
the no-correction scenario.
168
Table 1. The Exponential Smoothing (ES) and the Generalized Regression Neural Networks (GNNR) GPS positioning error
prediction models performance based on residual analysis.
__________________________________________________________________________________________________
Scenario (i): No corrections Scenario (ii): Klobuchar corrections Scenario (iii): Dual-frequency corrections
Mean Median Max Mean Median Max Mean Median Max
__________________________________________________________________________________________________
ES 0.2208 0.0527 2.5948 0.1208 0.0515 2.6363 -0.1390 0.3251 2.4469
GRNN 0.0527 -0.1154 2.4266 0.0292 -0.0401 2.5448 -0.1128 0.3212 2.4648
__________________________________________________________________________________________________
A time series of horizontal GPS positioning errors
was constructed from time series of northing and
easting positioning errors. Using the horizontal GPS
positioning error time series, two candidate
prediction model development methods were
selected and tuned, i.e., the exponential smoothing
and the generalized regression neural networks
(GRNN), to develop candidate models of the
horizontal GPS positioning error. The original time
series of 2872 single-point horizontal GPS positioning
errors was split into the first 2857 elements training
set, and the remaining 15 elements test set to assess
the prediction models performance. The reduction of
number of GPS pseudorange observations in
comparison with the nominal determination for
provision of 30 s-sampled data was not explained by
IGS.
The most suitable theoretical statistical
distribution to fit the experimental one was selected
using the Cullen & Fray diagram, as shown in Figure
3. for the northing component of the GPS positioning
vector in the no-correction scenario.
The model performance analysis was conducted
on the basis of residuals between the estimated
positions and the true position of the IGS reference
station. Two candidate models extend similarly in
their performance, as evident from the performance
assessment results outlined in Table 1.
Figure 3. Cullen & Fray diagram for the northing
component of the GPS positioning vector in the no-
correction scenario.
We suggest the preference should be given to the
GRNN model for its ability to accommodate a larger
variance in GPS positioning performance during the
extended period of observations, and for the
method’s ability to learn from new cases.
4 DISCUSSION
The commercial-grade GPS positioning performance
in the Northwest Passage was assessed in three
scenarios of the ionospheric effects mitigation. In
general, the GPS positioning performance observed
during a massive deterioration of space weather does
not meet the requirements for maritime navigation
and non-navigation applications. Notable biases and
variations were identified in three components of the
GPS positioning error vector in all three scenarios of
presumed GPS use in the Arctic region of the
Northwest Passage during a massive space weather
disturbance. Deterioration of the GPS positioning
error was understood to result from the inadequate
GPS receiver design, as well as from the unaccounted
space weather deterioration of the unknown
statistical properties, thus its effects were not being
accounted when using common correction models
and procedures. Those were exploited for the GPS
positioning error prediction model development
based on the observed northing, easting, and vertical
positioning errors, and on two competing model
development methods: the exponential smoothing,
and the Generalised Regression Neural Networks
(GRNN). Based on this study results, a set of
recommendations on the GNSS receiver design and
the standalone and assisted GNSS use in the newly
opened and emerging transport routes in polar
regions are proposed for improvement of safety,
accuracy, and sustainability of maritime navigation.
The recommendations are as follows:
GNSS receiver design that benefits from dual-
frequency GNSS ionospheric effects corrections is
recommended for use in the Northwest Passage.
Use of the Klobuchar correction model is not
recommended in the Northwest Passage during the
periods of intensive space weather disturbance,
and/or geomagnetic and ionospheric storm.
Use of the Generalised Regression Neural
Networks (GRNN) GPS positioning error prediction
model on either un-corrected, or dual frequency-
corrected GPS pseudoranges-based position estimates
is a recommended practice in the Northwest Passage
during a period of intensive space weather
disturbance and/or geomagnetic and ionospheric
storm.
Utilisation of recommended GRNN model may
lead to the transition from infrastructure-assisted
mitigation of the GNSS ionospheric effects towards
the adaptive GNSS positioning process, capable of the
GNSS positioning environment awareness, as
proposed in [10]. The adaptive GNSS positioning
process is particularly suitable for maritime vessels,
which may offer power stability and sufficiency, as
well as required computational capacity.
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