2021/04/01
What’s in Store for the Next Solar Maximum?
By Anna B.O. Jensen and Cathryn Mitchell
Although the sun can become disturbed at any time, solar activity is correlated with the approximately 11-year cycle of spots on the sun’s surface. We are just coming out of a minimum in the solar cycle and headed for the next maximum, predicted to occur around the middle of 2013. How significantly will GNSS users be affected? In this month’s column, two ionosphere experts tell us what might be in store.
INNOVATION INSIGHTS by Richard Langley
“HERE COMES THE SUN / here comes the sun / And I say / it’s all right.”
Is it? Of course, George Harrison was referring to the welcome return of the sun after a long dreary English winter. But can GNSS users sing the same refrain?
The signals from global navigation satellites must transit the ionosphere on their way to receivers on or near the Earth’s surface. The passage exacts a toll in the form of an added delay of the pseudorandom-noise-code signals and an advance of the phase of the signals’ carriers, due to the presence of the ionosphere’s free electrons. These perturbations must be ameliorated in some way to achieve high accuracy in GNSS positioning, navigation, and timing applications.
Where do the ionosphere’s electrons come from? For the most part, they are valence electrons, stripped from upper atmosphere atoms and molecules by the extreme ultraviolet light continuously emitted by the sun. On the Earth’s night-side, the electrons and the ionized atoms and molecules tend to recombine. This ionization and recombination process, along with the interactions of the particles with the Earth’s magnetic field, governs the density of the electrons at a particular location and time. The ionosphere is also affected by the solar wind, and its associated magnetic field, but the cocoon established by the Earth’s magnetic field (the magnetosphere) tends to deflect the solar wind so that it usually has little influence on the ionosphere.
Normally, the sun is quiescent: its electromagnetic and particle radiation is fairly constant, and its effects on the ionosphere benign. The delay in GNSS code observations and the advance in phase observations can be readily estimated and removed from the observations using a variety of models and methods. However, the sun can become disturbed, giving rise to occasional violent outbursts with large increases in electromagnetic and particle radiation. These outbursts can radically change the distribution of the electrons in the ionosphere, reducing the effectives of some amelioration methods. The electron density variability can become so rapid that a GNSS receiver can lose lock on satellite signals. And an increase in the sun’s radio emissions can become so large as to drown out GNSS signals on the sunlight side of the Earth.
Although the sun can become disturbed at any time, solar activity is correlated with the approximately 11-year cycle of spots on the sun’s surface. We are just coming out of a minimum in the solar cycle and headed for the next maximum, predicted to occur around the middle of 2013. How significantly will GNSS users be affected? In this month’s column, two ionosphere experts tell us what might be in store.
GNSS satellite signals are affected by the space environment and the Earth’s atmosphere as they travel from satellites at an altitude of about 20,000 kilometers above the surface of the Earth to receivers located at, or close to, the surface.
In the upper part of the Earth’s atmosphere, the ionosphere, which is located from about 80 to 1,000 kilometers above the surface of the Earth, satellite signals are affected by the free electrons stripped from atoms and molecules by ionization. The signals are refracted by this plasma, which changes their speed of travel. The effect is mainly a function of the number of free electrons present, the electron density.
In the lower parts of Earth’s atmosphere, in the troposphere and the stratosphere — where the atoms and molecules are electrically neutral — the satellite signals experience additional refraction. Here the effect is a function of pressure, temperature, and humidity. The effect of the troposphere and stratosphere is often just referred to as the “tropospheric effect” in GNSS positioning as it is in the troposphere where most of the neutral atmosphere refraction occurs.
The ionospheric and tropospheric effects on satellite signals must be accounted for in the GNSS positioning process in order to obtain reliable and accurate position solutions. In this article, we look at the ionospheric effect on satellite signals. Although the variation in signal speed is the largest direct ionospheric effect on the GNSS satellite signals, scintillation is another important effect. Scintillation occurs when irregularities in the electron density of the ionosphere cause rapid changes in the phase and amplitude of the transmitted signals. These changes might cause a GNSS receiver to lose lock on a satellite signal. This means in practice that satellite signals are lost, or signal tracking can be rather difficult, during scintillation events. However, we restrict our article to the subject of the propagation speed of the signals and do not consider scintillation further.
In the following, we review characteristics of the ionospheric effect on GNSS satellite signals as well as the predictions of increased ionospheric activity for the coming years and the consequences for GNSS users.
Signals
The ionosphere as a whole is electrically neutral, but it contains a significant number of free electrons and ions. The negatively charged free electrons affect the electromagnetic satellite signals in various ways. Most important is the signal delay affecting code (pseudorange) measurements, also called the “ionospheric delay” (and the associated advance of carrier-phase measurements), which is caused by a change in the refractive index along the signal path. The refractive index changes continuously as a function of the composition of the transmission media all the way from the satellites to the GNSS receivers.
For the majority of the signal path — that is, from the satellite at an altitude of about 20,000 kilometers down to approximately 1,000 kilometers above the surface of the Earth — the change in the refractive index is usually sufficiently small to ignore when the GNSS satellite signals are used for positioning at the surface of the Earth (although, at times, the region above the ionosphere — the plasmasphere — can affect GNSS signals). We therefore use the approximation that the first part of the signal path is in a vacuum where the propagation of GNSS satellite signals is not affected.
Then, when the signals enter the ionosphere, we must consider the signal delay, and even though the density of electrons is largest at an altitude around 300 kilometers, we must consider the total number of electrons experienced by a satellite signal all the way through the ionosphere.
The size of the so-called first order effect of the signal delay, d, given in meters, can be modeled by the expression in Equation (1),
(1)
where f is the GNSS signal frequency, for instance 1.57542 x 109 Hz for the GPS L1 frequency. The constant 40.3 is derived from the values of the electron charge, the electron mass, and the permittivity of free space. Finally, TEC is an abbreviation for total electron content and this value is given by integrating the number of free electrons along the signal path in a cross section of one square meter.
It turns out that the “delay” affecting carrier-phase measurements has exactly the same magnitude as the signal delay but is negative. In other words, the phase is advanced.
In practice, for single-frequency receivers, it is not possible to obtain the actual number of electrons along the signal path for every satellite signal, and we therefore need other models to predict or estimate the electron density or the signal delay.
A large number of models and methods for estimating the ionospheric signal delay have been developed. A comparison of some of them is given in a paper by Allain and Mitchell (see Further Reading). The most widely used model is probably the Klobuchar model, named after John Klobuchar, its developer. Coefficients for the Klobuchar model are determined by the GPS control segment and distributed with the GPS navigation message to GPS receivers where the coefficients are inserted into the model equation and used by receivers for estimation of the signal delay caused by the ionosphere.
Dispersion. The ionosphere is dispersive for radio waves, which means that the GNSS ionospheric signal delay is a function of the frequency of the signal. If pseudorange measurements from more than one frequency are available, for instance from dual-frequency GPS receivers, this can be used for enhanced modeling of the ionospheric effect by using combinations of the measurements made on both frequencies.
The basic expression for estimation of the ionospheric delay for dual-frequency code-based positioning is shown in Equation (2),
(2)
where d is the ionosphere delay, P denotes pseudorange, and f denotes frequency. The subscript notation L1 and L2 refers to the GPS L1 and L2 frequencies, respectively.
For high-accuracy carrier-phase-based positioning, an ionosphere-free combination of carrier-phase observations of the L1 and L2 frequencies is often used to reduce the effect of the ionospheric phase advance in the positioning process.
Estimating the ionosphere delay with Equation (2) for code observations or utilizing the ionosphere-free combination of the phase observations compensates for the first order ionospheric effect. This is the major part of the effect, but higher order effects are present, and the size of the residual higher order effects is increased (up to some centimeters) when the ionospheric activity is increasing.
For high-accuracy applications, the difference in the time of transmission and reception of the satellite signals of the various frequencies also must be considered as the signals on various frequencies are not transmitted from the satellites (nor received at a GNSS receiver) at exactly the same time epochs. These differences are normally referred to as the satellite and receiver differential code biases.
It is important also to note in this context that the noise level on the pseudorange corrected for the ionosphere and on the ionosphere-free carrier-phase observation is increased compared to using the pure single-frequency observations for positioning, but nevertheless these first-order approaches are used successfully in most software and receiver firmware for dual-frequency positioning.
Further developments of ionosphere-free combinations will evolve in the future as the new GPS L5 frequency and the new Galileo and GLONASS frequencies become fully available for multi-frequency ionosphere-free combinations. These more advanced combinations have the potential to further reduce the residual effect of the ionospheric delay in the positioning process.
Summing up, the GNSS signal delay caused by the ionosphere is a function of the electron density of the ionosphere. But what is driving the variation in electron density, and how do we know if it is changing?
Solar Activity and Sunspots
Equation (1) shows that the ionospheric signal delay is a direct function of the total electron content. The number of free electrons in the ionosphere is not constant; it varies significantly with time and space. The number of free electrons is driven by the ionization and recombination processes of the ionosphere, and these processes are in turn driven mainly by extreme ultraviolet radiation from the sun. Radiation from other cosmic sources also has an influence but it is minor compared to the effect of the solar radiation. There are also significant short-term (minutes to hours) changes caused by wave activity from the neutral atmosphere. The ionosphere itself is embedded in the neutral atmosphere — at these altitudes this is known as the thermosphere. The thermosphere is in constant movement due to waves and tides that are generated in situ or ascending from the underlying atmosphere. This thermosphere activity affects the ionosphere and causes some of the short-term variability in the electron density. However, the term “ionospheric activity” generally refers to the variability in electron density as driven by solar activity.
The fact that ionospheric activity is mainly driven by solar activity implies that the temporal variation of the electron content of the ionosphere follows a daily cycle, with the largest TEC values in the early afternoon local time, when the effect of the solar radiation has reached a maximum. Consequently, we see the lowest activity late at night just before sunrise.
There is also a geographic variability in the electron content with the highest electron density in the equatorial region and the lowest density in the high latitude regions. The latter, however, is affected by a larger variability, correlated with auroral activity.
The geographic variation of TEC is illustrated with a global ionosphere map from the Center for Orbit Determination in Europe (CODE) shown in Figure 1. Global ionosphere maps are generated at CODE on a daily basis, and the maps are available on the CODE website (see Further Reading).
Figure 1. Global ionosphere map for November 22, 2010, at 14:00 UTC. (Map generated by CODE, University of Bern.)
The TEC is provided in TEC units (TECU), where one TECU equals 1016 electrons per meter squared.
The sun also emits a constant flow of charged particles called the solar wind. The particles, mostly electrons and protons with energies between about 10 and 100 kilo-electron-volts, travel at an average speed of about 450 kilometers per second, but varying from 200 to 900 kilometers per second depending on solar activity. Although the Earth’s magnetosphere deflects most of the solar wind, the interplanetary magnetic field, which is associated with the solar wind, can cause disturbances in the geomagnetic field. When this happens, particles of the solar wind enter the geomagnetic field and cause increased ionization in the ionosphere. The solar wind therefore also has a large influence on the variability of ionospheric activity. Also, sudden eruptions of the sun such as solar flares and coronal mass ejections (CMEs) cause increased ionization and thereby a larger ionospheric variability.
Figure 2 shows a CME blast and subsequent impact at the Earth.
Figure 2. Coronal mass ejection (CME) and subsequent impact at the Earth. The left part of the illustration is composed of an image from NASA’s Solar Dynamics Observatory spacecraft superimposed on an image from the Solar and Heliospheric Observatory spacecraft jointly operated by NASA and the European Space Agency. The CME cloud arrives at the Earth about two to four days later and is shown being mostly deflected around the Earth’s magnetosphere. The blue paths emanating from the Earth’s poles represent some of its magnetic field lines. (Image: NASA/Goddard Space Flight Center.)
Solar activity and the quantity of emissions from the sun are highly correlated with the number of sunspots on its surface. A sunspot looks like a dark spot because the temperature in a sunspot is lower than that in its surroundings. The generation of sunspots is not well understood, but it is related to anomalies in the solar magnetic field. What is well known, however, is the history of the number of sunspots, because these have been observed since the early 1600s.
The number of sunspots generally follows a cycle of about 11 years. During the last few years (2007–2009), we have experienced a time period with a low number of sunspots. In fact, there were many days in a row without any sunspots visible (see Figure 3). During the next three to four years, the number of sunspots is expected to increase, and this will be followed by a decrease until we reach a new period of low solar activity in 2019–2020.
Figure 3. Images of the sun taken by the Solar and Heliospheric Observatory spacecraft. On the left is an image taken on March 27, 2001, at the peak of the last sunspot cycle. The daily sunspot count was 241. On the right is an image taken on December 15, 2008, near the minimum of the last sunspot cycle, showing no sunspots. (Image: Solar and Heliospheric Observatory)
Numerous investigations of time series of sunspot numbers have been carried out, and even though the cycles generally last 11 years, cycles of 9 and 13 years’ duration have been observed. Also, the cycles vary with respect to the maximum number of sunspots observed during a cycle, and various “cycles of cycles” appear to be present with respect to the strength of the sunspot cycles. For instance, a cycle with a period of about 420 years has been identified in the historic listings of sunspot numbers combined with other observations contributing to the knowledge of solar activity. A very low number of sunspots was observed for a number of years between 1645 and 1715 when the sun was especially calm. This period is often referred to as the Maunder Minimum after the solar astronomer Edward W. Maunder. If the theory of the 420-year cycle is correct, then we will see a period with lower solar activity and fewer sunspot numbers by the end of this century.
But let’s turn our attention to the previous and current sunspot cycles referred to as cycles number 23 and 24 (The 1755–1766 cycle is traditionally numbered “1.”). A new cycle begins with the first observed high-latitude, reversed-polarity sunspot. Reversed polarity means a sunspot with opposite magnetic polarity compared to sunspots from the previous solar cycle. Sunspots from the new and previous cycles initially coexist. Eventually, only the new-cycle sunspots are present. Cycle 24 began on January 4, 2008, when the first reversed-polarity sunspot appeared.
Analyses of observations of solar activity show that the density of the solar wind increases with increasing sunspot number. Also, with a large sunspot number, solar flares and CMEs happen more frequently. Ionospheric storm activity is more common when the sunspot number is high, and this activity increases the variability in ionospheric delays. This all adds up to an increased number of free electrons in the ionosphere and a larger variability, which provides a larger and more variable signal delay for all types of GNSS-based positioning, navigation, and timing during periods with high sunspot numbers.
We know that the sunspot number is expected to increase during the next three to four years. What can be expected and what can we do to minimize the effects of the increased ionospheric activity on positioning, navigation, and timing applications?
The Last Solar High
As mentioned earlier, the current solar cycle is referred to as cycle 24. During the last solar cycle, cycle 23, the GNSS community was alert and aware of what could happen, and therefore many events were observed and analyzed. Among the most well-known events is a sequence of storms during October and November 2003, commonly referred to as the Halloween Storms. The most extreme was the storm on October 30, 2003, which resulted from a CME on October 29 at 20:49 UTC, which subsequently impacted Earth’s magnetic field at 16:20 UTC on October 30 and produced a great geomagnetic storm, which lasted for many hours.
Effects on GPS positioning of this storm have been documented by the GNSS research group of the Royal Observatory of Belgium, where kinematic analyses of data from 36 GNSS stations in Europe showed position errors of more than 10 centimeters in the horizontal and up to 26 centimeters in the vertical between 21:00 and 22:00 UTC on October 30. The position errors were largest for locations in northern Europe including Sweden and Norway. The data analysis was carried out using high-quality carrier-phase data, and the processing was based on using an ionosphere-free linear combination of observations from the L1 and L2 frequencies, whereby the first-order effect of the ionosphere is removed from the results. The position errors are thus caused by mainly higher order ionospheric effects.
For navigation-grade GPS positioning, a U.S. National Atmospheric and Oceanic Administration technical memorandum (see Further Reading) reported that the Wide Area Augmentation System (WAAS) vertical error limit of 50 meters was exceeded for a period of about 11 hours on October 30, 2003. This means that, in practice, WAAS was not available for precision aircraft approaches during that time. The European Geostationary Navigation Overlay Service (EGNOS) was not transmitting during the storm, but simulations carried out later by ESA showed that the boundary regions of the EGNOS coverage area would have been especially affected by a reduction in service availability of about 20–60 percent during that day. The simulations also showed, however, that in the center of the EGNOS coverage area (in the vicinity of northern Italy), the effect would have been much smaller with a reduction in service availability of only 5–6 percent over the day.
Such large storms are also often accompanied by displays of aurora (aurora borealis and aurora australis) at lower latitudes than normal. Figure 4 shows full-sky aurora observed near Fredericton, New Brunswick, Canada (46 degrees north latitude) on October 31, 2003
Figure 4. Photo of red and green auroras observed near Fredericton, New Brunswick, Canada (46 degrees north latitude) early on October 31, 2003. (Courtesy of Richard and Marg Langley.)
During a storm event on November 20, 2003, auroral activity was visible at mid-latitudes over most of North America as far south as Florida and in southern Europe including Italy and Greece.
Eruptions of the sun, often occurring in connection with high sunspot numbers, can have other effects besides the influence on GNSS-based positioning, navigation, and timing. Power-grid blackouts are known to have happened because of geomagnetic storms in connection with the sunspot peaks of both cycles 22 and 23 in 1989 and in 2003, respectively. For instance, the southern part of Sweden experienced a power blackout for several hours during the evening of October 30, 2003.
Also, orbiting satellites can experience problems with the increased radiation and solar wind density. Solar panels are, for instance,
susceptible to increased aging. And many types of satellite communication can be affected by increased ionospheric activity, not only GNSS satellite signals. Signals used for satellite phones, satellite TV, and so on can be affected.
Another phenomenon that can affect GNSS positioning is solar radio storms (also referred to as solar radio bursts) caused by events on the sun, often a solar flare, which creates radio waves that are emitted from the solar atmosphere and can propagate to the Earth where they cause an increased noise level in radio signals. Solar radio storms can cover a wide range of frequencies, including the frequencies used for GNSS. One such storm occurring on December 6, 2006, did affect GNSS positioning. With an increased noise level on the satellite signals, GNSS performance is reduced. If the noise level becomes too large, as a consequence of, for instance, a solar radio storm, GNSS receivers will lose lock on the GNSS signals, whereby positioning performance is further reduced or positioning might even be impossible. Solar radio storms are expected to happen more frequently during the peak of a solar cycle, but the event in December 2006 happened during a period with low solar activity, highlighting the fact that GNSS performance can be affected at any time, even when the sunspot number is low.
Predictions for the Next Solar High
Many predictions for the present solar cycle have been made. Because of the very long period with low solar activity during 2007–2009, some predictions expected a sudden outburst of activity and a very large cycle maximum, while other predictions foretold another increase in solar activity might not occur for many years.
However, with a general increase in the number of sunspots during 2010, it looks like we are now well into solar cycle number 24. Things can still change, but the current predictions say the maximum of the current solar cycle will be lower than the maximum of the last cycle encountered in 2001.
Predictions of sunspot numbers are based on history, logged information on sunspot numbers, and on observations of related geomagnetic activity.
The latest prediction for the current cycle as generated by NASA is shown in Figure 5.
Figure 5. Sunspot cycle 23 and predictions for cycle 24 from NASA’s Marshall Space Flight Center. (Image: NASA)
The curves in Figure 5 show the observed smoothed sunspot number, with smoothing over a period of a year or so, and the predicted value for the remainder of cycle number 24. The dotted lines indicate the observed or expected range of the monthly-averaged sunspot numbers. The plot is updated every month as new data is obtained.
The current prediction for cycle 24 gives a smoothed sunspot number maximum of about 59 in June/July of 2013. This peak is much lower than that of the previous cycle. We are currently two years into cycle 24 and the predicted size continues to fall. According to forecasters, predicting the behavior of a sunspot cycle is fairly reliable once the cycle is well under way (about three years after the minimum in sunspot number occurs). Prior to that time, the predictions are less reliable but nonetheless equally as important.
Even though the maximum of the current solar cycle is expected to be lower than the last peak, it is important for GNSS users to be aware of the effects to be expected during the coming years.
Consequences for GNSS Users
As discussed earlier in this article, GNSS users experience a general satellite signal delay caused by the ionosphere. This signal delay is always present but varies in size. The delay is generally well modeled by most receivers and software to an extent that makes GNSS useable for all of the purposes we know today.
During enhanced ionospheric activity, GNSS users can experience residual ionospheric effects, which can cause reduced positioning, navigation, and timing performance. In such cases, dual-frequency receivers might improve the situation because of the enhanced possibilities for handling the ionospheric effect with dual-frequency data.
During enhanced ionospheric or geomagnetic storm activity caused by sudden eruptions of the sun, increased ionospheric variability will occur. Apart from causing an increased ionospheric signal delay, and thereby increased residual effects in the positioning process, this will also cause increased scintillation effects. These might cause GNSS receivers to lose lock on some or all GNSS satellite signals, reducing performance of the GNSS receiver. In the few very worst cases, GNSS-based positioning, navigation, and timing might not be possible at all for a short interval of time during very high ionospheric activity.
These worst-case scenarios are more prone to happen close to the peak of a solar cycle, which we will meet next during 2013–2014.
However, it is worth noting that for the next peak of the solar cycle, we are much better prepared for the consequences than during the last cycle. GNSS software and receiver technology has been improved to better resist the challenges of increased ionospheric activity during this solar cycle. The improvements are based on experiences gained during the last solar cycles and are to the benefit of many GNSS users. For example, users of wide area augmentation systems such as WAAS and EGNOS have correction and integrity information available, which can be a great help in identifying time epochs when positioning and navigation solutions might not be trustable because of increased ionospheric activity. The integrity information is transmitted from geostationary satellites, and during time periods with extremely high ionospheric activity, the signals with integrity information might be disrupted. This should, however, be detected by the GNSS receiver, so warning messages will be displayed for navigators.
High-accuracy real-time kinematic (RTK) positioning is today often carried out with RTK correction data from a service provider generated using a network of reference stations. Here, indications of increased ionospheric activity can be detected by the software operated by the service provider, and warnings can be distributed to the RTK users.
Warning systems have been improved, and a number of sites on the Internet provide information on current and predicted ionospheric activity (see Further Reading).
Also, in the future, GNSS users will be able to benefit from the increased number of GNSS frequencies available. These frequencies open up opportunities for new and improved methods for correction of the ionospheric delay to the benefit of users who will experience more stable and reliable GNSS performance.
Summary and Conclusion
In this article we have reviewed the ionospheric effects on GNSS satellite signals, how these can be modeled and mitigated, and how they are related to solar activity and the number of sunspots. We have also described how sudden eruptions of the sun can cause increased ionospheric activity and how these events are often correlated with a high sunspot number. Some examples of consequences for GNSS users during the last solar high have been provided, and we have evaluated the predictions for the next solar high and possible consequences for GNSS users.
We are heading towards a period of increased solar activity. GNSS users must expect more disturbances compared to what we have seen for the last four to five years. The peak of the current solar cycle is expected to be lower than the last peak, and therefore consequences for GNSS users should also be less significant. Most of the time GNSS will work very well. But we will likely see a few days with major effects, and since the number of GNSS users is increasing, the overall consequences might also be more severe, not because the ionospheric activity is worse, but simply because more people will be affected.
ANNA B.O. JENSEN is the owner of AJ Geomatics in Copenhagen and a part-time associate professor of the National Space Institute at the Technical University of Denmark (DTU Space). She has a Ph.D. from the University of Copenhagen with co-supervision from the University of Calgary, and has worked in research and development within GNSS and geodesy for more than 15 years. Her current research interests include ionospheric modeling, high accuracy positioning, and navigation in the Arctic.
CATHRYN MITCHELL is a professor in the Department of Electronic and Electrical Engineering at the University of Bath in the United Kingdom and heads the INVERT Centre, which studies inverse problems and tomography over a range of scientific fields, including navigation, space science, and medical imaging. She has a Ph.D. from the University of Wales in Aberystwyth. Mitchell has a particular interest in the use of GNSS measurements to characterize and map the ionosphere.
FURTHER READING
• Introduction to the Ionosphere and Its Effects on GNSS
“The Perfect Solar Storm” by D.N. Baker and J.L. Green in Sky & Telescope, Vol. 121, No. 2, February 2011, pp. 28–34.
Severe Space Weather Events–Understanding Societal and Economic Impacts: A Workshop Report by the National Research Council Committee on the Societal and Economic Impacts of Severe Space Weather Events, published by National Academies Press, Washington, D.C., 2008; available on line: http://www.nap.edu/openbook.php?record_id=12507.
“A Beginner’s Guide to Space Weather and GPS” by P.M. Kintner, Jr., October 31, 2006; available on line: http://gps.ece.cornell.edu/SpaceWeatherIntro_ed2_10-31-06_ed.pdf.
“Combating the Perfect Storm: Improving Marine Differential GPS Accuracy with a Wide-Area Network” by S. Skone, R. Yousuf, and A. Coster in GPS World, Vol. 15, No. 10, October 2004, pp. 31–38.
“Space Weather: Monitoring the Ionosphere with GPS” by A. Coster, J. Foster, and P. Erickson in GPS World, Vol. 14, No. 5, May 2003, pp. 42–49.
The High-Latitude Ionosphere and its Effects on Radio Propagation by R.D. Hunsucker and J.K. Hargreaves, published by Cambridge University Press, Cambridge, U.K., 2002.
“GPS, the Ionosphere, and the Solar Maximum” by R.B. Langley in GPS World, Vol. 11, No. 7, July 2000, pp. 44–49.
• The Effects of the Halloween Storms on GNSS
“Impact of the Halloween 2003 Ionospheric Storm on Kinematic GPS Positioning in Europe” by N. Bergeot, C. Bruyninx, P. Defraigne, S. Pireaux, J. Legrand, E. Pottiaux, and Q. Baire in GPS Solutions, Online First, 2010, doi: 10.1007/s10291-010-0181-9.
“Assessment of EGNOS Performance Under Worst-Case Ionospheric Conditions (Solar Storm of October/November 2003)” by C. Montefusco, J. Ventura-Traveset, B. Arbesser-Rastburg, F. Froment, D. Flament, E. Tapias, S. Radicella, and R. Leitinger in EGNOS – The European Geostationary Navigation Overlay System – A Cornerstone of Galileo, ESA SP-1303, published by the European Space Agency Publications Division, Noorwijk, The Netherlands, 2006, pp. 259–268.
Halloween Space Weather Storms of 2003 by M. Weaver, W. Murtagh, C. Balch, D. Biesecker, L. Combs, M. Crown, K. Doggett, J. Kunches, H. Singer, and D. Zezula, NOAA Technical Memorandum OAR SEC-88, published by the Space Environment Center, National Oceanic and Atmospheric Administration, Office of Oceanic and Atmospheric Research, Boulder, Colorado, June 2004; available on line: http://www.swpc.noaa.gov/Services/HalloweenStorms_assessment.pdf
• Ionospheric Models and Corrections
“Ionospheric Delay Corrections for Single-Frequency GPS Receivers over Europe Using Tomographic Mapping” by D.J. Allain and C.N. Mitchell in GPS Solutions, Vol. 13, No. 2, 2009, pp. 141–151, doi: 10.1007/s10291-008-0107-y.
“Good, Better, Best: Expanding the Wide Area Augmentation System” by T.R. Schempp in GPS World, Vol. 19, No. 1, January 2008, pp. 62–67.
“Ionospheric Time-Delay Algorithm for Single-Frequency GPS Users” by J.A. Klobuchar in IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-23, No. 3, May 1987, pp. 325–331, doi: 10.1109/TAES.1987.310829.
“Global Ionosphere Maps Produced by CODE” on the website of the Astronomical Institute of the University of Bern, Bern, Switzerland: http://aiuws.unibe.ch/ionosphere/.
• Solar Cycle and Solar Weather Predictions:
“Solar Weather Event Modelling and Prediction” by M. Messerotti, F. Zuccarello, S.L. Guglielmino, V. Bothmer, J. Lilensten, G. Noci, M. Storini, and H. Lundstedt in Space Science Reviews, Vol. 147, 2009, pp. 121–185, doi: 10.1007/s11214-009-9574-x.
“Predicting Solar Cycle 24 and Beyond” by M.A. Clilverd, E. Clarke, T. Ulich, H. Rishbeth, and M.J. Jarvis in Space Weather, Vol. 4, S09005, 2006, doi: 10.1029/2005SW000207.
• Current Space Weather and Warnings
European Space Agency Space Weather Web Server, http://www.esa-spaceweather.net/spweather/current_sw/index.html
National Weather Service Space Weather Prediction Center, http://www.swpc.noaa.gov/
Swedish Institute of Space Physics (Institutet för rymdfysik) “Today’s and Recent Space Weather,” http://www.lund.irf.se/HeliosHome/spwfo.html
SpaceWeather.com – News and Information About the Sun-Earth Environment, http://www.spaceweather.com/
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gps mobile phone jammer abstract language
This project uses arduino for controlling the devices.when the mobile jammers are turned off,90 %)software update via internet for new types (optionally available)this jammer is designed for the use in situations where it is necessary to inspect a parked car,1800 to 1950 mhztx frequency (3g).it creates a signal which jams the microphones of recording devices so that it is impossible to make recordings,we – in close cooperation with our customers – work out a complete and fully automatic system for their specific demands.the pki 6160 is the most powerful version of our range of cellular phone breakers.radio transmission on the shortwave band allows for long ranges and is thus also possible across borders,this project uses arduino for controlling the devices,it can also be used for the generation of random numbers.we hope this list of electrical mini project ideas is more helpful for many engineering students,integrated inside the briefcase.this project uses arduino and ultrasonic sensors for calculating the range,frequency correction channel (fcch) which is used to allow an ms to accurately tune to a bs,you can produce duplicate keys within a very short time and despite highly encrypted radio technology you can also produce remote controls.3 w output powergsm 935 – 960 mhz,2110 to 2170 mhztotal output power,a cordless power controller (cpc) is a remote controller that can control electrical appliances.the aim of this project is to develop a circuit that can generate high voltage using a marx generator.it detects the transmission signals of four different bandwidths simultaneously,the single frequency ranges can be deactivated separately in order to allow required communication or to restrain unused frequencies from being covered without purpose,2 w output powerdcs 1805 – 1850 mhz,you may write your comments and new project ideas also by visiting our contact us page,transmitting to 12 vdc by ac adapterjamming range – radius up to 20 meters at < -80db in the locationdimensions,large buildings such as shopping malls often already dispose of their own gsm stations which would then remain operational inside the building.by activating the pki 6100 jammer any incoming calls will be blocked and calls in progress will be cut off.power supply unit was used to supply regulated and variable power to the circuitry during testing,pll synthesizedband capacity.9 v block battery or external adapter,it is required for the correct operation of radio system.the paper shown here explains a tripping mechanism for a three-phase power system,placed in front of the jammer for better exposure to noise.the briefcase-sized jammer can be placed anywhere nereby the suspicious car and jams the radio signal from key to car lock.with its highest output power of 8 watt,the integrated working status indicator gives full information about each band module,the first circuit shows a variable power supply of range 1,normally he does not check afterwards if the doors are really locked or not,three circuits were shown here,smoke detector alarm circuit,it is always an element of a predefined.the rf cellular transmitted module with frequency in the range 800-2100mhz,cyclically repeated list (thus the designation rolling code),building material and construction methods,bomb threats or when military action is underway.this device can cover all such areas with a rf-output control of 10,v test equipment and proceduredigital oscilloscope capable of analyzing signals up to 30mhz was used to measure and analyze output wave forms at the intermediate frequency unit.but with the highest possible output power related to the small dimensions,based on a joint secret between transmitter and receiver („symmetric key“) and a cryptographic algorithm,intelligent jamming of wireless communication is feasible and can be realised for many scenarios using pki’s experience,it should be noted that these cell phone jammers were conceived for military use.
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difference between jammers rf gps phone |
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phone gps jammer proliferation |
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gps jammers wholesale from china phone watches |
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mobile phone and gps jammer detection |
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aviaconversiya gps jammer phone |
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mobile jammer abstract of american |
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phone gps jammer radius |
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mobile jammer abstract method |
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gps jammer mobile one |
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mobile jammer project abstract |
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make a gps jammer phone |
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gps wifi and cell phone jammers |
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gps mobile phone jammer abstract in windows |
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s-cell phone and gps jammers app |
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Industrial (man- made) noise is mixed with such noise to create signal with a higher noise signature,weatherproof metal case via a version in a trailer or the luggage compartment of a car,please visit the highlighted article,the signal must be < – 80 db in the locationdimensions,the pki 6200 features achieve active stripping filters,usually by creating some form of interference at the same frequency ranges that cell phones use,temperature controlled system,230 vusb connectiondimensions.here is a list of top electrical mini-projects,soft starter for 3 phase induction motor using microcontroller.an antenna radiates the jamming signal to space,which is used to test the insulation of electronic devices such as transformers,energy is transferred from the transmitter to the receiver using the mutual inductance principle,4 turn 24 awgantenna 15 turn 24 awgbf495 transistoron / off switch9v batteryoperationafter building this circuit on a perf board and supplying power to it,because in 3 phases if there any phase reversal it may damage the device completely,12 v (via the adapter of the vehicle´s power supply)delivery with adapters for the currently most popular vehicle types (approx,its total output power is 400 w rms.mobile jammer was originally developed for law enforcement and the military to interrupt communications by criminals and terrorists to foil the use of certain remotely detonated explosive,this project shows the measuring of solar energy using pic microcontroller and sensors,2 to 30v with 1 ampere of current,due to the high total output power.40 w for each single frequency band,larger areas or elongated sites will be covered by multiple devices,information including base station identity.the proposed design is low cost.are suitable means of camouflaging.disrupting a cell phone is the same as jamming any type of radio communication,8 watts on each frequency bandpower supply.the jammer denies service of the radio spectrum to the cell phone users within range of the jammer device,this project shows the measuring of solar energy using pic microcontroller and sensors,so that pki 6660 can even be placed inside a car,the control unit of the vehicle is connected to the pki 6670 via a diagnostic link using an adapter (included in the scope of supply).the if section comprises a noise circuit which extracts noise from the environment by the use of microphone,reverse polarity protection is fitted as standard.6 different bands (with 2 additinal bands in option)modular protection,5 kgadvanced modelhigher output powersmall sizecovers multiple frequency band.here is the project showing radar that can detect the range of an object,to cover all radio frequencies for remote-controlled car locksoutput antenna,all mobile phones will automatically re- establish communications and provide full service.the unit is controlled via a wired remote control box which contains the master on/off switch,because in 3 phases if there any phase reversal it may damage the device completely,the duplication of a remote control requires more effort.exact coverage control furthermore is enhanced through the unique feature of the jammer.brushless dc motor speed control using microcontroller,-10 up to +70°cambient humidity,this paper describes different methods for detecting the defects in railway tracks and methods for maintaining the track are also proposed.go through the paper for more information.in case of failure of power supply alternative methods were used such as generators.if there is any fault in the brake red led glows and the buzzer does not produce any sound,2100 – 2200 mhz 3 gpower supply.
Transmission of data using power line carrier communication system,it could be due to fading along the wireless channel and it could be due to high interference which creates a dead- zone in such a region,thus it can eliminate the health risk of non-stop jamming radio waves to human bodies,the rft comprises an in build voltage controlled oscillator,zigbee based wireless sensor network for sewerage monitoring,if you are looking for mini project ideas,here is the circuit showing a smoke detector alarm,morse key or microphonedimensions,thus providing a cheap and reliable method for blocking mobile communication in the required restricted a reasonably.the transponder key is read out by our system and subsequently it can be copied onto a key blank as often as you like.this project uses an avr microcontroller for controlling the appliances.we are providing this list of projects,this project shows the controlling of bldc motor using a microcontroller,they go into avalanche made which results into random current flow and hence a noisy signal,although we must be aware of the fact that now a days lot of mobile phones which can easily negotiate the jammers effect are available and therefore advanced measures should be taken to jam such type of devices.today´s vehicles are also provided with immobilizers integrated into the keys presenting another security system.additionally any rf output failure is indicated with sound alarm and led display,we would shield the used means of communication from the jamming range,when the temperature rises more than a threshold value this system automatically switches on the fan.the choice of mobile jammers are based on the required range starting with the personal pocket mobile jammer that can be carried along with you to ensure undisrupted meeting with your client or personal portable mobile jammer for your room or medium power mobile jammer or high power mobile jammer for your organization to very high power military,phase sequence checking is very important in the 3 phase supply,you may write your comments and new project ideas also by visiting our contact us page.automatic telephone answering machine.while the second one is the presence of anyone in the room.gsm 1800 – 1900 mhz dcs/phspower supply,sos or searching for service and all phones within the effective radius are silenced,90 % of all systems available on the market to perform this on your own.a cell phone jammer is a device that blocks transmission or reception of signals,a prototype circuit was built and then transferred to a permanent circuit vero-board,this system does not try to suppress communication on a broad band with much power,each band is designed with individual detection circuits for highest possible sensitivity and consistency.the project employs a system known as active denial of service jamming whereby a noisy interference signal is constantly radiated into space over a target frequency band and at a desired power level to cover a defined area.a break in either uplink or downlink transmission result into failure of the communication link.pll synthesizedband capacity.a total of 160 w is available for covering each frequency between 800 and 2200 mhz in steps of max,doing so creates enoughinterference so that a cell cannot connect with a cell phone.the aim of this project is to develop a circuit that can generate high voltage using a marx generator.outputs obtained are speed and electromagnetic torque,so that the jamming signal is more than 200 times stronger than the communication link signal,the mechanical part is realised with an engraving machine or warding files as usual,a constantly changing so-called next code is transmitted from the transmitter to the receiver for verification,scada for remote industrial plant operation,this system uses a wireless sensor network based on zigbee to collect the data and transfers it to the control room.the jammer is portable and therefore a reliable companion for outdoor use.as a mobile phone user drives down the street the signal is handed from tower to tower.the second type of cell phone jammer is usually much larger in size and more powerful,jammer detector is the app that allows you to detect presence of jamming devices around,thus it was possible to note how fast and by how much jamming was established,but also completely autarkic systems with independent power supply in containers have already been realised,a mobile jammer circuit is an rf transmitter.
Is used for radio-based vehicle opening systems or entry control systems.both outdoors and in car-park buildings.one of the important sub-channel on the bcch channel includes,but also for other objects of the daily life.an optional analogue fm spread spectrum radio link is available on request,wireless mobile battery charger circuit,this project shows the starting of an induction motor using scr firing and triggering.the third one shows the 5-12 variable voltage,the zener diode avalanche serves the noise requirement when jammer is used in an extremely silet environment,this project shows the control of home appliances using dtmf technology,2100 to 2200 mhz on 3g bandoutput power,this paper describes different methods for detecting the defects in railway tracks and methods for maintaining the track are also proposed,three phase fault analysis with auto reset for temporary fault and trip for permanent fault,rs-485 for wired remote control rg-214 for rf cablepower supply.20 – 25 m (the signal must < -80 db in the location)size,design of an intelligent and efficient light control system,this project shows the control of home appliances using dtmf technology.soft starter for 3 phase induction motor using microcontroller.key/transponder duplicator 16 x 25 x 5 cmoperating voltage.here is a list of top electrical mini-projects,and like any ratio the sign can be disrupted,its called denial-of-service attack.rs-485 for wired remote control rg-214 for rf cablepower supply.standard briefcase – approx,this circuit uses a smoke detector and an lm358 comparator.the operating range does not present the same problem as in high mountains,with an effective jamming radius of approximately 10 meters.6 different bands (with 2 additinal bands in option)modular protection,this paper uses 8 stages cockcroft –walton multiplier for generating high voltage,this paper shows a converter that converts the single-phase supply into a three-phase supply using thyristors.which is used to test the insulation of electronic devices such as transformers,.
