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Article

Investigation into the Effect of Atmospheric Particulate Matter (PM2.5 and PM10) Concentrations on GPS Signals

1
Department of Civil Engineering, The University of Nottingham Ningbo China, 199 Taikang East Road, Ningbo 315100, China
2
Department of Chemical and Environmental Engineering, The University of Nottingham Ningbo China, 199 Taikang East Road, Ningbo 315100, China
*
Author to whom correspondence should be addressed.
Sensors 2017, 17(3), 508; https://doi.org/10.3390/s17030508
Submission received: 2 January 2017 / Revised: 1 March 2017 / Accepted: 2 March 2017 / Published: 3 March 2017
(This article belongs to the Section Remote Sensors)

Abstract

:
The Global Positioning System (GPS) has been widely used in navigation, surveying, geophysical and geodynamic studies, machine guidance, etc. High-precision GPS applications such as geodetic surveying need millimeter and centimeter level accuracy. Since GPS signals are affected by atmospheric effects, methods of correcting or eliminating ionospheric and tropospheric bias are needed in GPS data processing. Relative positioning can be used to mitigate the atmospheric effect, but its efficiency depends on the baseline lengths. Air pollution is a serious problem globally, especially in developing countries that causes health problems to humans and damage to the ecosystem. Respirable suspended particles are coarse particles with a diameter of 10 micrometers or less, also known as PM10. Moreover, fine particles with a diameter of 2.5 micrometers or less are known as PM2.5. GPS signals travel through the atmosphere before arriving at receivers on the Earth’s surface, and the research question posed in this paper is: are GPS signals affected by the increased concentration of the PM2.5/PM10 particles? There is no standard model of the effect of PM2.5/PM10 particles on GPS signals in GPS data processing, although an approximate generic model of non-gaseous atmospheric constituents (<1 mm) can be found in the literature. This paper investigates the effect of the concentration of PM2.5/PM10 particles on GPS signals and validates the aforementioned approximate model with a carrier-to-noise ratio (CNR)-based empirical method. Both the approximate model and the empirical results show that the atmospheric PM2.5/PM10 particles and their concentrations have a negligible effect on GPS signals and the effect is comparable with the noise level of GPS measurements.

1. Introduction

The Global Satellite Navigation System (GNSS) has been widely used in vehicle and personal navigation, engineering and geodetic surveying, geophysical and geodynamic studies, machine guidance, attitude determination [1], indoor positioning (with high-sensitivity receiver), etc. High-precision GNSS applications such as engineering and geodetic surveying need millimeter and centimeter level accuracy. GNSS includes the US Global Positioning System (GPS), the Russian GLObal NAvigation Satellite System (GLONASS), the European Galileo, and the Chinese Beidou (BDS); systems with global positioning coverage are considered as GNSS in this paper—BDS’s Geostationary Orbit (GEO) and Inclined Geosynchronous Orbit (IGSO) satellites are considered as Regional Navigation Satellite System (RNSS) in this paper because they only provide regional positioning capacity. GNSS signals transmit from Medium Earth Orbit (MEO) satellites passing through the space and atmosphere, and arrive at GNSS receivers on the Earth’s surface. Since GNSS signals are affected by atmospheric biases, method for correcting or eliminating any ionospheric and tropospheric bias are needed in GNSS data processing. The ionosphere is a dispersive medium, which causes different delays/advancements in measurements in different GNSS frequencies. The original GPS was designed to have two frequencies in the L1 and L2 bands, and the two frequencies can be linearly combined to eliminate the first-order ionospheric effect. All GNSS, therefore, have two or more frequencies to tackle the ionospheric effect. Moreover, the ionospheric effect can be mitigated by applying correction models such as the Klobuchar model [2] and the NeQuick model [3]. Tropospheric refraction affects all GNSS frequencies the same, i.e., the delays in different frequencies are the same. Correction models such as the Hopfield model [4], and the Saastamoinen model [5] can be used to mitigate tropospheric bias. More details about GNSS ionospheric and tropospheric effects and their correction/mitigation can be found in [6].
Air pollution is a serious environmental problem globally, especially in developing countries. Major pollutants include sulfur oxides (SOx), nitrogen oxides (NOx), carbon monoxide (CO), volatile organic compounds (VOC), particulates, alternatively referred to as particulate matter (PM), chlorofluorocarbons (CFCs), ammonia (NH3), radioactive pollutants, etc. Particulates are tiny solid or liquid particles suspended in a gas. Respirable suspended particles (RSP) are relatively coarse particles with a diameter of 10 micrometers or less, also known as PM10. Fine particles with a diameter of 2.5 micrometers or less is known as PM2.5. High levels of PM2.5 in the air are linked to health hazards such as heart disease [7], reduced lung function and lung cancer. A global view of PM2.5 density observed by the Multi-angle Imaging SpectroRadiometer (MISR) and the Moderate Resolution Imaging Spectroradiometer (MODIS) remote sensing satellites in 2001–2006 presented by NASA is shown in Figure 1. It shows PM2.5 density is usually high in developing countries. Figure 2 shows the PM2.5 density observed by the MISR and MODIS remote sensing satellites over China in 2008–2010. Ningbo, for which the location in China is shown on the map (Figure 2), is the city where test data collection took place for this investigation.
GNSS can be used to estimate the zenith tropospheric delay [8] and to estimate precipitable water vapor content [9]. GNSS signals travel through the atmosphere, and so it may be asked whether GNSS signals are refracted by the atmospheric particulate matters or not. There is no standard model of the atmospheric PM2.5/PM10 particles on GNSS signals in GNSS data processing, and the authors could only find an approximate generic model of non-gaseous atmospheric constituents (<1 mm) [10] in the literature. This paper investigates the effect of the concentration of PM2.5/PM10 particles on GPS signals and validates the aforementioned approximate generic model with a carrier-to-noise ratio (CNR) based empirical method. Note that GPS is used in this investigation because it is the only GNSS providing global coverage with code division multiple access (CDMA) signals and that is in its full operational capacity (FOC) currently. The frequency division multiple access (FDMA) based GLONASS is not used in this investigation because physical interaction is usually frequency dependent. Moreover, the long constellation geometry repeatability (i.e., 8 days) of GLONASS would cause greater meteorological uncertainty in the proposed empirical method of this paper.
The objective of this paper is to investigate any effect of the concentration of atmospheric PM2.5 and PM10 on GPS signals based on single-station GPS dual-frequency data collected on the roof of the Science and Engineering Building (SEB) at the University of Nottingham Ningbo China (UNNC). This paper is divided into five sections: Section 1 presents the introduction and background of this research. Section 2 describes briefly the physics relevant to GNSS atmospheric refraction, and the approximate generic model of non-gaseous atmospheric constituents. The methodology of this investigation and the experimental data description are given in Section 3. Processing results and analysis are presented in Section 4. Finally, concluding remarks are given in Section 5.

2. Physics of Atmospheric Refraction in GNSS

According to the laws of reflection and refraction, when a plane wave falls on to a boundary between two homogeneous media of different optical properties, it is split into two waves—a transmitted wave proceeding into the second medium, and a reflected wave propagated back into the first medium [11]. In GNSS, it is well known that refraction occurs when GNSS signals propagate in the ionosphere and troposphere, and reflection occurs when there is multipath [12,13].
The ionospheric effects on the phase (δp) and code (δg) signal transmission path (s) can be represented as [6]:
δ p = ( n p 1 ) d s = ( a 1 f 2 + a 2 f 3 ) d s
where np denotes the refractive index of ionosphere on phase, coefficients a1 and a2 depend on the electronic density Ne, and f is the frequency:
δ g = ( n g 1 ) d s = ( a 1 f 2 a 2 f 3 ) d s
where ng denotes the refractive index of ionosphere on group. Omitting the second term on the right-hand side of Equations (1) and (2), we get:
δ p = δ g = ( a 1 f 2 ) d s
The ionospheric effects on the phase and code measurements have the opposite signs and have approximately the same magnitude. The coefficient a1 is −40.3Ne, where Ne is the electronic density. The total electronic content (TEC) in the zenith direction can be defined as:
T E C = N e d s
which can be computed from special models; see [6] for the details. Particulate matters are trapped in the planetary boundary layer that is usually below 2 km measured from sea level [14] while the ionosphere is in the region of 50–1500 km measured from sea level [15]. Therefore, no physical interaction between particulate matters in the lower atmosphere with ions/electrons in the ionosphere is possible.
Tropospheric effect depends on the temperature, pressure, humidity and altitude of the antenna location, it causes the same delays in different GNSS frequencies and measurement types (i.e., pseudorange and carrier phase). Similar to the ionospheric path delay, the tropospheric path delay can be written as [6]:
δ = ( n 1 ) d s
where n is the refractive index of the troposphere, the integration is taken along the signal path. Scaling of the refractive index anomaly (n − 1) is usually made by:
N = 10 6 ( n 1 )
where N is called tropospheric refractivity. N can be divided into the wet (about 10%) and dry (about 90%) components:
N = N w + N d
where indices w and d denote the wet and dry components, which are caused by the water vapour and dry atmosphere, respectively. Equation (5) becomes:
δ = δ w + δ d = 10 6 N d s
where the wet component of the tropospheric path delay (δw):
δ w = 10 6 N w d s
and, the dry component of the tropospheric path delay (δd):
δ d = 10 6 N d d s
Particulate matter (PM2.5 and PM10) may float in the air/gas or dissolve in water and become an aerosol [16], suspended in the troposphere [17]. The presence of particulate matter may change the refractivity of the troposphere. When an electromagnetic wave propagates through the “layer” of particulate matter, the possible physical interactions are reflection, refraction, absorption and scattering. GNSS frequency range (about 1.2–1.6 GHz) can be considered as very short radio waves or very long microwaves in the electromagnetic spectrum. We know that we can still receive GNSS signals when there is PM2.5/PM10 particulate matter in the atmosphere, therefore, the most likely and important physical interaction is refraction. However, it could be that the PM2.5/PM10 particulate matter has no physical effect on GNSS signals. If the refractive index of the particle is only slightly different than that of the surrounding medium [18]:
| n 1 | 1
The unity inside the absolute value symbol in Equation (11) is the refractive index of the medium relative to itself, because n is the refractive index of the particle relative to that of the medium. If the condition expressed by Equation (11) is fulfilled, then the particle interacts very weakly with the incident light [18]; this may not be applicable to other electromagnetic frequencies. Nephelometry is used to measure the aerosol scattering coefficient, and it is suggested that PM2.5 has the real part of refractive index in the range of 1.3–1.8 and the imaginary part of refractive index in the range of 0.000–0.200 in the visible light spectrum [19]; the wavelength in the visible light spectrum is shorter than the diameter of particulate matter and it is much shorter than the GNSS signal wavelengths. We know that a large variety of chemical compounds are involved in the formation of aerosols, and at the same time it is extremely difficult to determine the chemical composition of an atmospheric aerosol. A lack of accurate knowledge of this chemical composition makes it difficult to infer the property that strongly depends upon it, namely, the refractive index (both real and imaginary) [20]; in the literature a value of 1.55 has often been assigned for atmospheric aerosols [21]. The imaginary refractive index of atmospheric particulate matter in the 0.3–1.7 µm spectral region shows seasonal and geographic variations [22]; note that this spectrum is much shorter than the GNSS spectrum and the imaginary refraction (absorption) is not a concern in this paper. In practice, most refractivity measurement methods such as a specular reflection technique of normal incidence at the surface of disks made out of aerosol and Abbe’s refractometer could cause chemical and/or physical changes and thus result in an error in the estimation of the in situ refractive index [21].
There is no physical model of the effect of particulate matter PM2.5/PM10 on GNSS signals in the literature. An approximate generic model of non-gaseous atmospheric constituents (<1 mm), based on the Clausius-Mossotti equation for refractivity, is given in [10] as:
( n 1 ) × 10 6 = N = 1.5 × 10 6 M ρ [ ε 1 ε + 2 ]
where M denotes the mass content of the particles per unit of air volume, ρ denotes the density of the particles, ɛ denotes the permittivity of the particles, and M / ρ is the mass fraction of the suspended particles.
As stated above, due to the complex composition of particulate matter and the difficulties of measuring the refractive index of the particulate matter in the atmosphere, it is difficult to assess the impact of particulate matter (PM2.5/PM10) and its concentration on the tropospheric refractive index and on the GNSS signal propagation. This paper uses GPS raw carrier-to-noise ratio (CNR) data in consecutive sidereal days to analyze the impact of particulate matter on GNSS signal propagation, and validate the approximate generic model Equation (12).

3. Methodology of Investigation and Experimental Data Description

Since the receiver clock offset of a GNSS receiver is not a constant, we cannot compare GNSS pseudorange and carrier-phase measurements collected in high and low PM periods directly. Moreover, relative positioning techniques cannot be used to detect the impact of particulate matter on GNSS signal propagation because the assumption of different residuals due to particulate matter in different atmospheric paths cannot be justified. An empirical method is used to investigate any impact of particulate matter on GNSS signal propagation, and the detail is described as follows.
The empirical method is to compare the CNR data in the unit of dBHz in two consecutive sidereal days with similar and very different PM indices; it is called the CNR method, see below. Owing to the unique condition of repeatable satellite geometry in about one sidereal day at continuous static antennas, the same multipath errors repeat at the same sidereal time of the next day [13] and so as the CNR if there are no abnormal ionospheric and tropospheric activities such as ionospheric scintillation. The method of calculating sidereal days used in this paper can be found in [23]. Six GPS data sets collected at a GNSS reference station (with a Leica GR25 receiver and AT20 antenna) on the roof of the Science and Engineering Building (SEB) at the University of Nottingham Ningbo China (UNNC) are used in this investigation, and PM10, PM2.5 and Air Quality Index (AQI) data was collected at a national air quality monitoring station located at the Ningbo Wanli University, which is about 1.5 km from UNNC and the altitudes of the two stations are similar (about 20 m). Details of PM10, PM2.5, AQI indices and their conversion to concentration of pollutant in µg/m3 can be found in [24]; for example, PM2.5 AQI 50 = 12 µg/m3, PM2.5 AQI 200 = 150.4 µg/m3, PM2.5 AQI 300 = 250.4 µg/m3, PM10 AQI 50 = 54 µg/m3, PM10 AQI 200 = 354 µg/m3, PM10 AQI 300 = 424 µg/m3. The UNNC GNSS reference stations on the roof are shown in Figure 3. Two selected data sets were collected in November 2014 and four data sets were collected in December 2015, the values of PM10, PM2.5 and AQI indices of the six data sets are shown in Table 1, Table 2, Table 3 and Table 4. Periods of high (>200) and low (<50) PM indices are selected for this investigation, ratios of PM10, PM2.5 and AQI indices between the same time periods of the first day and second day are also shown in the tables. Data set 1 has great differences in PM10, PM2.5 and AQI indices between the two sidereal days (6–8 November 2014), and the ratios of the indices are in the range of about 3 to 12 as shown in the last three columns of Table 1. On the other hand, the differences in PM10, PM2.5 and AQI indices between the two sidereal days (7–9 November 2014) in Data set 2 are small, the ratios of the indices are in the range of about 0.6 to 1.8 (mainly around 1) as shown in the last three columns of Table 2. Data sets 3–5 are the data sets with large differences in PM10, PM2.5 and AQI indices in two sidereal days (15–17, 23–25, 23–24 in December 2015), the ratios are about 4 as shown in Table 3, Table 4 and Table 5. Data set 6 has small differences in PM10, PM2.5 and AQI indices in the two sidereal days in 27–29 December 2015, and the ratios are close to 1 as shown in Table 6. If there is an impact of particulate matter and its concentration on GNSS signal propagation such as refraction, the CNR should be different when the ratios of PM10, PM2.5 and AQI indices in two sidereal days are large. Data sets (i.e., Data sets 2 and 6) with low ratios (~1) of PM10, PM2.5 and AQI indices in two sidereal days are used to show the nominal differences in CNR. If there is no noticeable change in CNR (<the nominal CNR difference) when the PM10, PM2.5 and AQI ratios between sidereal days are large, then particulate matter and its concentration may have no or very insignificant impact on GNSS signal propagation. The maximum AQI index in the scale is 500 [24], the maximum AQI index in the data sets is 314 while the minimum AQI index is 20. The quality of the GPS data sets was checked using the Translate/Edit/Quality Check (TEQC) software [25], and no abnormal data is found in the data sets. Moreover, the temperatures, pressures and relative humidity values between the sidereal days in the data sets are similar, the effect of the small differences of them translated to tropospheric delay is analyzed in the next section.

4. Results, Analysis and Discussion

4.1. Description of Results

The L1 and L2 CNR and their differences on two consecutive sidereal days of the selected satellites in the six data sets are shown in Figure 4, Figure 5, Figure 6, Figure 7, Figure 8 and Figure 9; only two satellites per data set are shown due to the page limit. Moreover, the statistical results (mean and standard deviation (S.D.) in 95% confidence level) of the L1 and L2 CNR differences (i.e., Day 1 CNR–Day 2 CNR) in two consecutive sidereal days with the satellite elevation angle greater than 30° are presented in Table 7 and Table 8. The 30° satellite elevation mask is used in order to reduce the effect of the high noise level at low elevation angles on the statistical results.

4.2. Analysis of Results

The CNR differences of some satellites are positive and some are negative with positive being the majority in Data set 1 (see Table 7), we cannot see that the high PM10, PM2.5 and AQI indices in Day 1 (see Table 1) always lead to a reduction of CNR. Day 1 CNR minus Day 2 CNR would be always negative if the particulate matter had an impact on the GNSS signal propagation, which would lead to a reduction in signal strength and an increase in the noise level. In no physical and chemical circumstances would the additional particulate matter in the atmosphere increase the GNSS CNR. The overall mean values of L1 and L2 CNR differences of Data set 1 are less than those of Data set 2 (see Table 7, absolute values are considered). Since Data set 1 has great differences in PM10, PM2.5 and AQI indices between sidereal days (see Table 1) while Data set 2 has similar PM10, PM2.5 and AQI indices between sidereal days (see Table 2), we cannot find any significant impact of particulate matter on GNSS signal propagation based on the results of the data sets collected in November 2014.
Data sets 3–5 have great differences in PM10, PM2.5 and AQI indices between consecutive sidereal days (see Table 3, Table 4 and Table 5) while Data set 6 has similar PM10, PM2.5 and AQI indices between consecutive sidereal days (see Table 4). Similar to the data sets collected in November 2014, the CNR differences of some satellites are positive and some are negative with positive as the majority in Data sets 3–5 collected in December 2015 (see Table 8). The CNR differences in Data set 6 are less than the CNR differences in Data sets 3–5; however, the standard deviations are similar (see Table 8). Nevertheless, all the mean values of CNR differences in Data sets 1, 3–5 are much less than 1 dBHz, which is much less significant as the multipath effect [26].
The effect of the different temperatures, pressures and relative humidity values on tropospheric delays between sidereal days in the data sets is estimated. The hourly meteorological data collected at the national air quality monitoring station at Wanli University was put in the Saastamoinen tropospheric model [5,6], and the computed ZTDs in Days 1 and 2 and their differences of the six data sets are shown in Table 9. It shows that the effect of the different temperatures, pressures and relative humidity values on tropospheric delays between sidereal days is very small, therefore, the effect of the different meteorological conditions on CNR is negligible.
When we put a very high mass fraction of PM2.5/PM10 particles as 0.3 [27] and the relative permittivity of PM2.5 as 30 and PM10 as 3.8 [28] in (12), the path delays of PM2.5 and PM10 particles are about 0.2 and 0.4 mm, respectively, if 1 km is assumed as the PM2.5/PM10 layer height. When a simple mapping function of 1 / cos ( z e n i t h   a n g l e   o f   s a t e l l i t e ) is applied, the path delays of PM2.5 and PM10 particles become about 1.3 and 2.4 mm, respectively, when the zenith angle of a satellite is 80° (i.e., the elevation angle is 10°). Therefore, based on (12), the path delays induced by PM2.5/PM10 particles are in the similar range of GPS carrier-phase measurement noise or slightly larger when compared with the GNSS carrier-phase measurement noise levels described in [29].

5. Conclusions

The Global Satellite Navigation System (GNSS) has been widely used in vehicle and personal navigation, engineering and geodetic surveying, geophysical and geodynamic studies, machine guidance, attitude determination, indoor positioning (with high-sensitivity receiver), etc. High-precision GNSS applications such as engineering and geodetic surveying need millimeter and centimeter level accuracy. Air pollution is a serious environmental problem globally, especially in developing countries. Major pollutants include sulfur oxides, nitrogen oxides, carbon monoxide, volatile organic compounds, particulate matter (PM), chlorofluorocarbons, ammonia, radioactive pollutants, etc. GPS signals travel through the atmosphere before arriving at receivers on the Earth’s surface, but are GPS signals affected by the increased concentration of the PM2.5/PM10 particles? There is no standard model of the effect of PM2.5/PM10 particles on GNSS signals in GPS data processing, although an approximate generic model of non-gaseous atmospheric constituents (<1 mm) can be found in the literature. Through knowing the unique condition of repeatable satellite geometry of GPS in about one sidereal day at continuous static antennas, this paper presented an empirical method to investigate the impact of PM2.5/PM10 particles and their concentrations on GPS signal propagation. The method was used to compare the carrier-to-noise ratios (CNRs) in two consecutive sidereal days with similar and very different PM indices. Six data sets were collected on the campus of the University of Nottingham Ningbo China in November 2014 and December 2015 for this investigation. Since the receiver clock offset of a GNSS receiver is not a constant, we cannot compare GNSS pseudorange and carrier-phase measurements collected in high and low PM periods directly. Moreover, relative positioning techniques cannot be used to detect the impact of particulate matter on GNSS signal propagation because the assumption of differenced residuals due to particulate matter in different atmospheric paths cannot be justified. CNR is not affected by the different receiver clock offsets at different measurement epochs and it is not affected by multipath effect when the same sidereal time is used in the comparison. Therefore, CNR is used in this investigation.
In the CNR test, the results are mixed, but with more negative results than positive results (i.e., reduced CNR due to the presence of PM2.5/PM10 particles). All the CNR differences are much less than 1 dBHz, which is much less significant than the multipath effect. The CNR differences between consecutive sidereal days are likely due to the GPS carrier-phase measurement noise. Therefore, we cannot find any significant impact of high PM2.5/PM10 concentration on GPS signal propagation with the presented empirical method and the six data sets collected. This result agrees with the computed delays from the approximate generic model.

Acknowledgments

The authors would like to thank the reviewers for their in depth reviews and helpful suggestions that have greatly contributed to improving this paper. Part of the Article Processing Charge (APC) is funded by the Zhejiang Natural Science Foundation (ZJNSF) General Programme grant LY17D040001.

Author Contributions

Lawrence Lau conceived and designed the experiments, performed the experiments, analyzed the data, and wrote the paper; Jun He contributed PM, AQI and meteorological data.

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. Global view of PM2.5 in 2001–2006 based on data from the Multi-angle Imaging SpectroRadiometer (MISR) and the Moderate Resolution Imaging Spectroradiometer (MODIS) onTerra and on the GEOS-Chem model. (Source: http://visibleearth.nasa.gov/view.php?id=46823; Credit: NASA map by Robert Simmon, based on data from the Multi-angle Imaging SpectroRadiometer (MISR) and the Moderate Resolution Imaging Spectroradiometer (MODIS) on Terra and on the GEOS-Chem model. Caption by Holli Riebeek and Adam Voiland).
Figure 1. Global view of PM2.5 in 2001–2006 based on data from the Multi-angle Imaging SpectroRadiometer (MISR) and the Moderate Resolution Imaging Spectroradiometer (MODIS) onTerra and on the GEOS-Chem model. (Source: http://visibleearth.nasa.gov/view.php?id=46823; Credit: NASA map by Robert Simmon, based on data from the Multi-angle Imaging SpectroRadiometer (MISR) and the Moderate Resolution Imaging Spectroradiometer (MODIS) on Terra and on the GEOS-Chem model. Caption by Holli Riebeek and Adam Voiland).
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Figure 2. Satellite map of PM2.5 over China in 2008–2010 based on data from the MISR instrument on the Terra satellite, the MODIS instrument on the Terra and Aqua satellites, and a chemical transport model called GEOS-Chem. (Source: http://earthobservatory.nasa.gov/IOTD/view.php?id=77495; Credit: NASA Earth Observatory image by Jesse Allen, using data provided by Erica Zell, Battelle and Angel Hsu, Yale Center for Environmental Law & Policy. Caption by Adam Voiland.).
Figure 2. Satellite map of PM2.5 over China in 2008–2010 based on data from the MISR instrument on the Terra satellite, the MODIS instrument on the Terra and Aqua satellites, and a chemical transport model called GEOS-Chem. (Source: http://earthobservatory.nasa.gov/IOTD/view.php?id=77495; Credit: NASA Earth Observatory image by Jesse Allen, using data provided by Erica Zell, Battelle and Angel Hsu, Yale Center for Environmental Law & Policy. Caption by Adam Voiland.).
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Figure 3. GNSS reference stations in UNNC.
Figure 3. GNSS reference stations in UNNC.
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Figure 4. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN14 and PRN16 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 1; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR.
Figure 4. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN14 and PRN16 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 1; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR.
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Figure 5. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN14 and PRN15 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 2; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR; data gaps in the plots are due to a receiver data logging error.
Figure 5. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN14 and PRN15 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 2; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR; data gaps in the plots are due to a receiver data logging error.
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Figure 6. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN08 and PRN16 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 3; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR.
Figure 6. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN08 and PRN16 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 3; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR.
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Figure 7. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN14 and PRN16 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 4; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR.
Figure 7. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN14 and PRN16 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 4; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR.
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Figure 8. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN10 and PRN14 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 5; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR.
Figure 8. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN10 and PRN14 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 5; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR.
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Figure 9. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN08 and PRN16 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 6; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR.
Figure 9. Plots of L1 (a,b) and L2 (c,d) CNR of satellites PRN08 and PRN16 in Day 1 vs. L1 and L2 CNR of the satellites in Day 2 of Data set 6; Blue: Day 1 CNR, Green: Day 2 CNR, Red: the differences in Day 1 and Day 2 CNR.
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Table 1. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 1.
Table 1. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 1.
DateTime (hh:mm)PM10PM2.5AQIPM10 RatioPM2.5 RatioAQI Ratio
6 November 201419:001442222224.09.76.2
6 November 201420:001302032033.99.26.2
6 November 201421:001302032034.210.26.5
6 November 201422:001422162164.39.86.5
6 November 201423:001482232234.911.77.4
7 November 201400:001472212214.711.17.1
7 November 201401:001412132134.19.36.3
7 November 201402:001362072073.06.94.6
7 November 201419:00362336---
7 November 201420:00332233---
7 November 201421:00312031---
7 November 201422:00332233---
7 November 201423:00301930---
8 November 201400:00312031---
8 November 201401:00342334---
8 November 201402:00453045
Table 2. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 2.
Table 2. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 2.
DateTime (hh:mm)PM10PM2.5AQIPM10 RatioPM2.5 RatioAQI Ratio
7 November 201416:003826380.90.70.9
7 November 201417:003222321.00.70.9
7 November 201418:003019300.90.60.9
7 November 201419:003623361.10.71.0
7 November 201420:003322331.00.71.0
7 November 201421:003120311.30.81.2
7 November 201422:003322331.81.11.7
7 November 201423:003019301.71.11.5
8 November 201400:003120311.30.91.3
8 November 201416:00423942---
8 November 201417:00323036---
8 November 201418:00333235---
8 November 201419:00343535---
8 November 201420:00333333---
8 November 201421:00232626---
8 November 201422:00182020---
8 November 201423:00181820---
9 November 201400:00242324---
Table 3. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 3.
Table 3. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 3.
DateTime (hh:mm)PM10PM2.5AQIPM10 RatioPM2.5 RatioAQI Ratio
15 December 201521:001812802804.29.36.5
15 December 201522:001912952954.08.96.1
15 December 201523:001942982983.77.85.6
16 December 201500:001922932933.67.05.4
16 December 201501:001892902903.46.35.2
16 December 201521:00433043
16 December 201522:00483348
16 December 201523:00533853
17 December 201500:00544254
17 December 201501:00564656
Table 4. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 4.
Table 4. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 4.
DateTime (hh:mm)PM10PM2.5AQIPM10 RatioPM2.5 RatioAQI Ratio
23 December 201519:002003143144.96.06.0
23 December 201520:001943053054.76.16.1
23 December 201521:001892952954.55.75.7
23 December 201522:001902932933.95.05.0
23 December 201523:001912942943.74.74.7
24 December 201500:001942942943.74.74.7
24 December 201519:00415252
24 December 201520:00415050
24 December 201521:00425252
24 December 201522:00495959
24 December 201523:00516262
25 December 201500:00526363
Table 5. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 5.
Table 5. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 5.
DateTime (hh:mm)PM10PM2.5AQIPM10 RatioPM2.5 RatioAQI Ratio
23 December 201515:001362212214.05.35.3
23 December 201516:001432292293.34.24.2
23 December 201517:001532402403.84.64.6
23 December 201518:001662582584.25.05.0
24 December 201515:00344242
24 December 201516:00445555
24 December 201517:00405252
24 December 201518:00405252
Table 6. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 6.
Table 6. PM10, PM2.5 and AQI indices and their ratios between the two sidereal days of Data set 6.
DateTime (hh:mm)PM10PM2.5AQIPM10 RatioPM2.5 RatioAQI Ratio
27 December 201520:005548550.70.60.7
27 December 201521:005549550.70.70.7
27 December 201522:005650560.70.60.7
27 December 201523:005753570.80.80.8
28 December 201500:005650560.80.70.7
28 December 201501:005448540.70.60.7
28 December 201520:00757475
28 December 201521:00757575
28 December 201522:00767878
28 December 201523:00686768
29 December 201500:00747575
29 December 201501:00757979
Table 7. 95% confidence level statistical results of the L1 and L2 CNR differences of selected satellites in two consecutive sidereal days in the Datasets 1 and 2 collected in November 2014. Data with the satellite elevation angle greater than 30° is used.
Table 7. 95% confidence level statistical results of the L1 and L2 CNR differences of selected satellites in two consecutive sidereal days in the Datasets 1 and 2 collected in November 2014. Data with the satellite elevation angle greater than 30° is used.
Data Set 1 Great AQI DifferenceL1 (dBHz)L2 (dBHz)
PRNMeanS.D.MeanS.D.
140.0590.160−0.0560.560
160.1590.1450.0510.371
180.0160.1910.0110.809
21−0.0170.3170.3451.523
24−0.0090.2470.1001.074
Overall0.0420.090
Data set 2 Similar AQIL1 (dBHz)L2 (dBHz)
PRNMeanS.D.MeanS.D.
140.1240.1270.0790.221
150.1840.196−0.9751.085
180.0970.144−0.0430.386
240.1570.167−0.7020.744
290.1670.1910.0720.857
Overall0.146−0.314
Table 8. 95% confidence level statistical results of the L1 and L2 CNR differences of selected satellites in two consecutive sidereal days in the Datasets 3 to 6 collected in December 2015. Data with the satellite elevation angle greater than 30° is used.
Table 8. 95% confidence level statistical results of the L1 and L2 CNR differences of selected satellites in two consecutive sidereal days in the Datasets 3 to 6 collected in December 2015. Data with the satellite elevation angle greater than 30° is used.
Data Set 3 Great AQI DiffL1 (dBHz)L2 (dBHz)
PRNMeanS.D.MeanS.D.
080.0770.125−0.0120.257
16−0.0290.1556−0.0750.251
26−0.0470.166−0.0870.230
270.0030.1270.0150.156
Overall0.001−0.039
Data set 4 Great AQI diffL1 (dBHz)L2 (dBHz)
PRNMeanS.D.MeanS.D.
140.1850.1320.0940.314
160.0490.1730.0520.263
260.0840.1620.0790.215
27−0.0190.152−0.0500.176
Overall0.0750.044
Data set 5 Great AQI diffL1 (dBHz)L2 (dBHz)
MeanS.D.MeanS.D.
100.0920.0970.0720.171
120.1680.1470.1010.346
140.1930.1470.1080.414
180.0880.1090.0580.205
Overall0.1350.085
Data set 6 Similar AQIL1 (dBHz)L2 (dBHz)
MeanS.D.MeanS.D.
080.0770.1250.0130.220
160.0410.150−0.0410.286
26−0.0190.121−0.0410.209
270.0500.1240.0250.164
Overall0.037−0.011
Table 9. Saastamoinen modelled ZTD in Day 1 and Day 2 and their differences of the six data sets.
Table 9. Saastamoinen modelled ZTD in Day 1 and Day 2 and their differences of the six data sets.
Data Set 1Day 1 ZTD (m)Day 2 ZTD (m)ΔZTD (m)
19:002.4602.4590.0008
20:002.4662.4600.0063
21:002.4682.4620.0059
22:002.4702.4600.0103
23:002.4712.471−0.0007
00:002.4682.470−0.0027
01:002.4662.475−0.0090
02:002.4642.482−0.0179
mean−0.0009
Data set 2Day 1 ZTD (m)Day 2 ZTD (m)ΔZTD (m)
16:002.4552.492−0.0364
17:002.4572.493−0.0356
18:002.4592.492−0.0332
19:002.4592.493−0.0335
20:002.4602.492−0.0322
21:002.4622.491−0.0281
22:002.4602.489−0.0294
23:002.4712.484−0.0122
00:002.4702.482−0.0112
mean−0.0280
Data set 3Day 1 ZTD (m)Day 2 ZTD (m)ΔZTD (m)
21:002.4172.3880.0284
22:002.4192.3890.0296
23:002.4192.3860.0329
00:002.4182.3850.0324
01:002.4182.3890.0286
mean0.0304
Data set 4Day 1 ZTD (m)Day 2 ZTD (m)ΔZTD (m)
19:002.4402.448−0.0085
20:002.4392.446−0.0070
21:002.4422.448−0.0052
22:002.4442.448−0.0041
23:002.4432.445−0.0017
00:002.4442.4440.0002
mean−0.0044
Data set 5Day 1 ZTD (m)Day 2 ZTD (m)ΔZTD (m)
15:002.4372.451−0.0145
16:002.4412.452−0.0114
17:002.4432.450−0.0072
18:002.4422.451−0.0088
mean−0.0105
Data set 6Day 1 ZTD (m)Day 2 ZTD (m)ΔZTD (m)
20:002.4502.4240.0260
21:002.4462.4200.0265
22:002.4462.4220.0239
23:002.4422.4220.0203
00:002.4422.4160.0260
01:002.4422.4150.0270
mean0.0250

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Lau, L.; He, J. Investigation into the Effect of Atmospheric Particulate Matter (PM2.5 and PM10) Concentrations on GPS Signals. Sensors 2017, 17, 508. https://doi.org/10.3390/s17030508

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Lau L, He J. Investigation into the Effect of Atmospheric Particulate Matter (PM2.5 and PM10) Concentrations on GPS Signals. Sensors. 2017; 17(3):508. https://doi.org/10.3390/s17030508

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Lau, Lawrence, and Jun He. 2017. "Investigation into the Effect of Atmospheric Particulate Matter (PM2.5 and PM10) Concentrations on GPS Signals" Sensors 17, no. 3: 508. https://doi.org/10.3390/s17030508

APA Style

Lau, L., & He, J. (2017). Investigation into the Effect of Atmospheric Particulate Matter (PM2.5 and PM10) Concentrations on GPS Signals. Sensors, 17(3), 508. https://doi.org/10.3390/s17030508

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