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  • Blaze Terra Extension Enables Access to WAMI

    Eternix Ltd., provider of software for GIS visualization and editing in 3D, has released its first WAMI extension, enabling Blaze Terra users to access WAMI data through cloud-based services. WAMI — Wide Area Motion Imagery — is an advanced sensor-based technology that has been gaining popularity since its adoption by the Open Geospatial Consortium (OCG).

    Blaze Terra’s advanced GIS environment allows real-time decision makers working with WAMI to yield optimal insights and results at comfort and speed. Instant overlay of WAMI data with digital elevation models (DEM) or any other geospatial data, such as 3D models, raster or shape files, ensures a comprehensive user experience. In addition, a set of WAMI specific features, such as playback control and feature tracking, use WAMI’s inherent video qualities.

    “We believe that Blaze Terra’s high-end capabilities open a whole set of new opportunities for GIS professionals working with WAMI,” said Daniel Zeitlin, CTO at Eternix Ltd. “Vital application of WAMI occurs in areas where real-time decision making is key. Blaze Terra’s fast processing speed and holistic approach make it the ideal choice for such real-time applications.”

     

  • Galileo Satellites Ready for Fueling as Launcher Takes Shape

    Galileo Satellites Ready for Fueling as Launcher Takes Shape

    Galileo satellite being prepared for fit check. This testing, to ensure the seventh and eight Galileo satellites fit onto their dual-launch dispenser took place in mid-February 2015. The dispenser sits atop the Fregat upper stage of their Soyuz ST-B launcher.
    Galileo satellite being prepared for fit check. This testing, to ensure the seventh and eight Galileo satellites fit onto their dual-launch dispenser took place in mid-February 2015. The dispenser sits atop the Fregat upper stage of their Soyuz ST-B launcher. Photo: European Space Agency

    By the European Space Agency

    All the elements for this month’s Galileo launch are coming together at Europe’s Spaceport in French Guiana. As the two satellites undergo final testing and preparations, the first part of their Soyuz launcher has also been integrated.

    Assembly of the Soyuz ST-B’s first two stages, plus its four first stage boosters, took place at the Spaceport’s Soyuz Launcher Integration Building last week. Assembly takes place on a horizontal basis, in the Russian manner.

    The next step will be the addition of the third stage, then the main part of the launcher will be complete, ready to be transported to the Soyuz launch pad and moved to the vertical position.

    The final fourth stage of the Soyuz is the reignitable Fregat, which will transport the two satellites to their final 23,222-km altitude medium Earth orbit. This will be attached to the Soyuz on the launch pad, once the satellites, their dispenser and launch fairing have been mounted on it.

    Since the seventh and eighth Galileo satellites arrived in French Guiana last month, they have undergone several tests – including one System Compatibility Test Campaign each, where they are linked up to the rest of the global Galileo ground segment as if they are already ‘live’ in orbit.

    Assembly of seventh and eighth Galileo satellites' Soyuz ST-B’s first two stages, plus its four first stage boosters, took place at the Spaceport’s Soyuz Launcher Integration Building in the first week of March 2015. Assembly takes place on a horizontal basis, in the Russian manner.
    Assembly of seventh and eighth Galileo satellites’ Soyuz ST-B’s first two stages, plus its four first stage boosters, took place at the Spaceport’s Soyuz Launcher Integration Building in the first week of March 2015. Assembly takes place on a horizontal basis, in the Russian manner. Photo: European Space Agency

    The all-important ‘fit check’ was passed in the middle of February. The two satellites were installed separately onto their dual-launch dispenser, to check they fitted correctly.

    This dispenser has the task of holding them in place atop the Fregat during the launch and flight to their final orbit, then releasing them. They will be installed together later this month, after the satellites have been fueled.

    Last week saw the finalization of their hardware and software, and the charging of their batteries — on which the satellites will be reliant from the short but crucial period from their launch to the unfurling of their solar arrays in orbit.

    The pair of satellites is now ready to be transferred to the Spaceport’s S5A fueling facility, where they will receive the fuel to keep them controllable during their 12-year working lives.

    After their fueling and final check, the pair of satellites will be in launch configuration. After a final review they will then become available for Arianespace teams to carry out the final preparation, known as Combined Operations, leading to the launch day.

    The launch of the seventh and eighth Galileo satellites will take place on Friday, March 27.

    Cutaway view of the Soyuz rocket fairing carrying a pair of Galileo satellites. Photo: European Space Agency
    Cutaway view of the Soyuz rocket fairing carrying a pair of Galileo satellites. Photo: European Space Agency
  • Karel Introduces High-Performance GPS/INS System

    Karel Introduces High-Performance GPS/INS System

    The VIA-100G GPS/IMU by Karel Electronics.
    The VIA-100G GPS/IMU by Karel Electronics. Photo: Karel Electronics

    The VIA-100G, an integrated GPS and MEMS-IMU (inertial measurement system), has been added to the ViaNav inertial navigation system family produced by Karel Electronics Corporation.

    Featuring a high-accuracy fusion filter running on an embedded processor, the VIA-100G provides all the functions of a vertical reference unit (VRU), an attitude and heading reference system (AHRS) and integrated GPS/IMU system. The system contains GPS, 3D gyroscopes, 3D accelerometers, a magnetometer, a static pressure sensor and temperature sensors in a compact and rugged enclosure. The embedded processor provides driftless and real-time navigation information over a wide range of temperature in dynamic and static conditions, Karel said.

    The sensors are integrated with a highly accurate fusion filter. A Kalman filter running on an embedded processor fuses data from the IMU, GPS, magnetometer, altimeter and barometer in an optimal manner to output highly accurate navigation solutions. VIA-100G outputs high-frequency position, velocity and attitude information in addition to calibrated 3D acceleration, rotation, magnetometer and pressure data.

    The ViaNav product family includes other navigation products designed to be used in stability, guidance, control and navigation applications in industry. The VIA-100 line includes:

    • VIA-100I, is an inertial measurement unit with 3D accelerometers and 3D gyroscopes.
    • VIA-100A, is a 3 DOF AHRS that provides driftless real-time orientation information over the full 360 degrees of angular motion on all three axes. It includes 3D accelerometers, 3D gyroscopes and 3D magnetometers.
    • VIA-100A+, is a 3 DOF AHRS that provides driftless real-time orientation information. It includes a multi-IMU configuration and employs an optimum filter to lower IMU noise level. It provides 3D orientation with improved accuracy and reliability.
  • GEO Business 2015 Releases Conference Program

    GEO Business 2015, which takes place at the Business Design Centre in London from May 27-28, has released its conference program.

    More than 170 abstracts were received from authors representing 28 countries — an increase of 55 percent on the previous show.

     “With such incredible industry support, we are delighted to present a programme which reflects the vibrancy of technology in the geospatial sector,” Conference Chairman Graham Mills (Chairman of Technics Group and President of The Survey Association) said. “In fact, with so much innovation within the industry, the committee felt the need to introduce two new sessions this year, making a total of 16 sessions with a variety of presentations in each.” 

    An informative keynote address opens the show each day, including a presentation on the first day from Andrew McNaughton, technical director from HS2 (the UK’s proposed new high speed rail line). Day Two opens to a presentation about the “BIM Toolkit and Digital Plan of Work Project” by Dr Stephen Hamil, director of design and innovation at National Building Specification, UK.

    One of the new sessions is on “Emerging and Developing Technologies,” focusing on the future of geospatial technology. Topics include wearable GIS tools by Jaak Laineste, founder of Nutiteq; the future of maps by Gary Gale, founder of Malstow Geospatial; and the evolution of geospatial technology by Lee Braybrooke, marketing manager at Trimble. The other new session, “Is Your Asset Management Fit for the 21st Century?”, looks at how geospatial solutions can be used to support the management of assets in a variety of different situations.

    Other highlights of the program include a talk by Andrew Thompson, director of Savills (UK), about the role of geospatial professionals in the resolution of development neighbor disputes, following an increased parliamentary interest in the subject for new legislation.

    In a session on specifications and standards, Chris Preston, a senior engineer with Network Rail, will be discussing attitudes to risk and risk mitigation, including affordable solutions to control risk associated with geospatial data capture. In the same session, David Andrews, geospatial imaging officer at English Heritage, will be presenting English Heritage’s new edition of Metric Survey for Specifications, which is due to be released in May. The new version reflects changes in technology, including digital cameras, motion software and unmanned aerial platforms, as well as BIM. The session will be of interest to all those in the commercial sector who work on cultural heritage projects.

    With BIM sweeping through businesses, the programme includes two sessions on the subject. On Day One, Tim Wood, Global Business Architect at Arup, will be “joining the dots between GIS and BIM” as he talks about Arup’s role in regenerating Croydon, a city in the UK.  Similarly, Fred Mills, founding director of The B1M, will deliver a topical paper explaining the opportunities and benefits of mass BIM adoption on the second day of the conference.

    Another important talk on the subject of data comes from John Carpenter, director of Strategy and Planning at Ordnance Survey, who will provide insight into how geospatial data has been maintained at Ordnance Survey and how there is a need for new initiatives to extend the reach and impact for the next generation of stakeholders. On a similar subject, Adam Iwaniak, president of the Wroclaw Institute for Spatial Information and Artificial Intelligence, will present information about a recent project to develop the GeoMedia Semantic Toolkit, which is able to create and integrate linked data, making it possible to deliver geospatial knowledge in the Linked Data Web.

    For more information on the conference, visit www.GeoBusinessShow.com.

  • EuroGeographics, EuroSDR to Join on European Spatial Research

    EuroGeographics and EuroSDR have announced that they will work together to provide a framework for European spatial data research and development.

    The cooperation agreement will further the development of the EuroSDR Research Plan and the activities of the EuroGeographics Knowledge Exchange Networks. As a result, members of both not-for-profit organizations will benefit from greater opportunities for professional development. They will also be able to take part in joint projects and hand over tasks more appropriate to the other organisation’s expertise.

    “We have a common interest in carrying out and applying relevant research and developments in the field of geographic information and spatial data infrastructures,” said Ingrid Vanden Berghe, president of EuroGeographics, the membership association of the European National Mapping, Land Registry and Cadastral Authorities.

    “With rapid technological advances generated by a digital information society, the time from research via development to operation has never been faster. This agreement will ensure our members remain up to date with and understand the possibilities presented by new technologies and methodologies so they can react more quickly to user demands.”

    Martin Salzmann, president of EuroSDR, which links national mapping, land registry and cadastral authorities with research institutes and universities in Europe, added: “Achieving synergy in our activities benefits both our members and society by strengthening research and development, sharing results of common interest and making these operational. At the same time, we will foster and stimulate a vibrant research community with which to capitalise on future technologies and to be responsive to user demands. By working together we also avoid the risks of duplication of work between us and our member organisations.”

    EuroGeographics and EuroSDR are both committed to supporting wide range of initiatives that will benefit people across Europe, the companies said. These include the European Spatial Data Infrastructure, Copernicus, Galileo, Horizon2020, European Location Framework and the European Digital Single Market.

  • Antenna Array and Receiver Testing with a Multi-RF Output GNSS Simulator

    Antenna Array and Receiver Testing with a Multi-RF Output GNSS Simulator

    Luck_opener-W

    By Thorsten Lück, Günter Heinrichs, IFEN GmbH, and Achim Hornbostel, German Aerospace Center

    This article discusses the GALANT adaptively steered antenna array and receiver and demonstrates the test scenarios generated with the GNSS simulator. Exemplary results of different static and dynamic test scenarios are presented, demonstrating the attitude determination capabilities as well as the interference detection and mitigation capabilities.

    The vulnerability of GNSS to radio frequency interference and spoofing has become more and more of a concern for navigation applications requiring a high level of accuracy and reliability, for example, safety of life applications in aviation, railway, and maritime environments.In addition to pure power jamming with continuous wave (CW), noise or chirp signals, cases of intentional or unintentional spoofing with wrong GNSS signals have also been reported.

    Hardware simulations with GNSS constellation signal generators enable the investigation of the impact of radio interference and spoofing on GNSS receivers in a systematic, parameterized and repeatable way. The behavior of different receivers and receiver algorithms for detection and mitigation can be analyzed in dependence on interference power, distance of spoofers, and other parameters. This article gives examples of realistic and advanced simulation scenarios, set up for simulation of several user antennas simultaneously.

    The professional-grade high-end satellite navigation testing and R&D device used here is powerful, easy to use, and fully capable of multi-constellation / multi-frequency GNSS simulations for safety-of-life, spatial and professional applications. It provides all L-band frequencies for GPS, GLONASS, Galileo, BeiDou, QZSS, SBAS and beyond in one box simultaneously. It avoids the extra complexity and cost of using additional signal generators or intricate architectures involving several hardware boxes, and offers full control of scenario generation. A multi-RF capable version provides up to four independent RF outputs and a master RF output that combines the RF signal of each of the up to four individual RF outputs.

    Each individual RF output is connected to one or more “Merlin” modules (the core signal generator module for one single carrier) allowing simulation of up to 12 satellites per module. Because of the flexible design of the Merlin module, each one can be configured to any of the supported L-band frequencies.

    As one chassis supports up to nine individual Merlin modules, different Multi-RF combinations are feasible:

    • two RF outputs with up to four modules each
    • three RF outputs with up to three modules each
    • four RF outputs with up to two modules each.

    With these configurations, the user can simulate different static or dynamic receivers or even one receiver with multiple antennas, covering such challenging scenarios as ground networks, formation flying or use of beam-forming antennas.

    As the user is free to assign each individual module to a dedicated simulated antenna, the user could also employ up to nine modules to simulate nine different carrier signals for one single antenna using the master RF output, thus simulating the complete frequency spectrum for all current available GNSS systems in one single simulation.

    All modules are calibrated to garantee a carrier phase coherency of better than ±0.5°. Figure 1 shows the output at the RF master of two modules assigned to the same carrier but with a phase offset of 180°.

    Figure 1. Carrier-phase alignment of the high-end simulator with six modules compared to the first module.
    Figure 1. Carrier-phase alignment of the high-end simulator with six modules compared to the first module.

    Theoretically, the resulting signal should be zero because of the destructive interference. In practice, a small residual signal remains because of component tolerance, small amplitude differences and other influences. Nevertheless the best cancellation can be seen at this point. The phase accuracy can now simply be estimated from the measured power level of the residual signal:

    Luck-Eq1  (1)

    Luck-Eq2 (2)

    with

    Luck-Eq2b

    This means that the sum of two sine waves with the same frequency gives another sine wave. It has again the same frequency, but a phase offset and its amplitude is changed by the factor A. The factor A does affect the power level. If φ is 180° then A is 0, which means complete cancellation.

    So A shows the power of the resulting signal relative to the single sine wave. It can also be transformed to dB:

    Luck-Eq3 (3)

    Figure 2 shows the carrier suppression as a function of carrier phase offset with a pole at 180ϒ.

    Figure 2. Carrier suppresion as a function of phase delay.
    Figure 2. Carrier suppresion as a function of phase delay.

    The factory calibration aligns the modules to a maximum of 0.5ϒ misalignment. The measured suppresion therefore shall be better than 41.18 dBc. In practice, the residual signal is also caused by other influences, so that the actual phase alignment can be expected to be much better.

    With four RF outputs, the received signal of a four element antenna can be configured very easily. Figure 3 shows the dialog to configure a four-element antenna with the geometry shown in Figure 4. Note that the antenna elements are configured in the body-fixed system with the x-axis to front and the y-axis to the right (inline with a north-east-down, NED, system when facing to north), while the geometry shown in Figure 4 follows an east-north-up (ENU) convention.

    Figure 3. Configuration of individual antennas per receiver.
    Figure 3. Configuration of individual antennas per receiver.
    Figure 4. Geometry of the GALANT four-element phased-array antenna (view from top).
    Figure 4. Geometry of the GALANT four-element phased-array antenna (view from top).

    The following sections give an overview of multi-antenna systems and discuss results from a measurement campaign of the German Aerospace Center (DLR) utilizing the simulator and the DLR GALileo ANTenna array (GALANT) four-element multi-antenna receiver.

    Multi-Antenna Receivers

    Multi-antenna receivers utilize an antenna array with a number of antenna elements. The signals of each antenna element are mixed down and converted from analog to digital for baseband processing. In the baseband, the signals received by the different antenna elements are multiplied with complex weighting factors and summed. The weighting factors are chosen in such a way that the received signals from each antenna element cancel out into the direction of the interferers (nulling) and additionally, for advanced digital beamforming, such that the gain is increased into the direction of the satellites by forming of individual beams to each satellite. Because all these methods work with carrier phases, it is important that in the simulation setup, the signals contain the correct carrier phases at the RF-outputs of the simulator corresponding to the user satellite and user-interferer geometry, and the position and attitude of the simulated array antenna.

    Figure 5 presents the geometry of a rectangular antenna array with 2×2 elements and a signal s(t) impinging from direction (ϕ, θ).

    Figure 5. Parallel wavefront impinging on a rectangular array with 2x2 elements.
    Figure 5. Parallel wavefront impinging on a rectangular array with 2×2 elements.

    The spacings of the elements dx, dy are typically half a wavelength, but can also be less. The range difference for antenna element i relative to the reference element in the center of the coordinate system depends on the incident direction (ϕ, θ) and the position (m=0,1, n=0,1) of the element within the array:

    Luck-Eq4 (4)

    The corresponding carrier phase shift is:

    Luck-Eq5 (5)

    For CRPA and adaptive beam forming applications, the differential code delays may be neglected if they are small compared to the code chip length. However, it is essential that the carrier phase differences are precisely simulated, because they contain the information about the incident direction of the signal and are the basis for the array processing in the receiver. For instance, the receiver can estimate the directions of arrival of the incident signals from these carrier phase differences.

    Now we consider a 2×2 array antenna. It can be simulated with the simulator with four RF outputs, where each output corresponds to one antenna element. In the simulator control software, a user with four antennas is set up, where the position of each antenna element is defined as an antenna position offset relative to the user position. In this approach, both differential code and carrier delays due to the simulated array geometry are taken into account, because the code and carrier pseudoranges are computed by the simulator for the position of each antenna element. However, the RF hardware channels of the receiver front-end may have differential delays against each other, which may even vary with time. If the direction of the satellites and interferers shall be estimated correctly by the receiver algorithms, a calibration signal is required to measure and compensate these differential hardware delays.

    For the real antenna system, a binary phase-shift keying (BPSK) signal with zero delay for each antenna channel is generated by the array receiver and fed into the antenna calibration port. For the simulation, this calibration signal must also be generated by the constellation simulator.

    In a simple way, a satellite in the zenith of the user antenna can be simulated, which has the same distance and delay to all antenna elements. Unfortunately, this simple solution includes some limitations to the simulated position and attitude of the user, because the user position must be at the Equator (if a “real” satellite is simulated in form of a geostationary satellite) and the antenna must not be tilted.

    With a small customization of the simulator software, these limitations could be overcome. Figure 6 shows how to set up the generation of a reference signal. This reference signal can either be simulated as a transmitter directly above the user position, which follows the user position and thus allows also simulations offside the Equator, or simulated as a zero-range signal on all RF outputs, neglecting any geometry, which is the preferred method. The latter one is more or less identical to the reference/calibration signal generated by the receiver itself.

    Figure 6. Configuration of a modulated reference signal.
    Figure 6. Configuration of a modulated reference signal.

    The power level of this signal is held constant and is not affected by any propagation delay or attenuation simulated by the control center.

    Attitude Determination

    According to Figure 5, the phase difference measured between antenna elements is a function of the direction of arrival (DoA). Thus, the DoAs of the incident signals can be estimated from the phase differences. In the GALANT receiver, the DoAs are estimated by an EPSPRIT algorithm after correlation of the signals. Compared with the (known) positions of the GNSS satellites, this allows the estimation of the antenna array attitude. Figure 7 shows the sky-plot of simulated satellites as seen at receiver location (simulated on the right; reconstructed by the receiver from the decoded almanac in the middle and the DoA on the left). By comparison of the estimated DoAs of all satellites and the skyplot from the almanac, the attitude of the antenna is estimated (left). In addition, the attitude angles simulated by the simulator is given (right).

    Figure 7. Simulating and estimating attitude with a multi-element antenna.
    Figure 7. Simulating and estimating attitude with a multi-element antenna.

    Simulation of Interference

    It is possible to simulate some simple types of interference. Possible interference scenarios are:

    Wideband Noise. By increasing the power of a single satellite of the same or another GNSS constellation, a wideband pseudo-noise signal can be generated. Using a geostationary satellite also enables simulating an interference source at low elevations and constant position. Use of power-level files also allow generation of scenarios with intermittent interference (switching on and off the interference) with switching rates up to 5 Hz.

    CW or Multi-Carrier IF. By disabling the spreading code and navigation message, a CW signal can be generated. The simulator also allows configuration of subcarrier modulations. Without spreading code (or to be precise with a spreading code of constant zero) the generated signal will consist of two carriers symmetrically around the original signal carrier (for example, configuring a BOC(1,1) signal will create two CW signals at 1.57542 GHz ± 1.023 MHz, thus producing “ideal” interferer for the Galileo E1 OS signal.)

    Depending on the number of Merlin modules per RF output, interference to signal ratios up to 80 dB could be realized, limited by a dynamic range of 40 dB within one module and additional 40 dB range between two modules. However, the maximum power level of one individual signal is currently limited to -90 dBm. If only one channel per module is used, the maximum power level of this single signal can be increased by another 18 dB (for example, by using one module solely for interference generation and another module for GNSS simulation).

    Figure 8 shows the simulated geometry for an interference scenario based on wideband noise generated by a geostationary satellite, producing –90 dBm signal power at the receiver front end. The interference source is very near to the direction of PRN 22 with a jammer power of –90 dBm, resulting in a jammer to signal ratio of J/S = 25 dB.

    Figure 8. Geometry for the wideband noise interference scenario.
    Figure 8. Geometry for the wideband noise interference scenario.

    Figure 9 shows the two-dimensional antenna pattern as a result of the beam-forming before and after switching on the interferer. The mitigation algorithm tries to minimize gain into the direction of the interferer. As this also decreases gain into the direction of the intended satellite, the C/N0 drops by approximately 10 dB for PRN 22, because its main beam is shifted away from the interference direction. For satellites in other directions, the decrease in C/N0 is less: compare Figure 9 with Figure 10. However, the receiver still keeps tracking the satellite. After switching of beamforming, the signal is lost.

    Figure 9. Beamforming for PRN 22 (light green line in lower plot) to mitigate for interference.
    Figure 9. Beamforming for PRN 22 (light green line in lower plot) to mitigate for interference.
    Figure 10. Tracking is lost after switching off beamforming for individual channels (light blue, purple) and all channels (at the end of the plot).
    Figure 10. Tracking is lost after switching off beamforming for individual channels (light blue, purple) and all channels (at the end of the plot).

    Simulation of Spoofing

    The simulation of a spoofing signal requires twice the resources as the real-world scenario, as every “real” LoS-signal must also be generated for the spoofing source. A simulation of an intentional spoofer who aims to spoof a dedicated position in this context is, however, very similiar to the simulation of a repeater ([un-]intentional interferer) device:

    The repeater (re-)transmits the RF signal received at its receiver position. A receiver tracking this signal will generate the position of the repeater location but will observe an additional local clock error defined by the processing time within the repeater and the travel time between repeater and receiver position. A correct simulation for a multi-antenna receiver therefore has to superpose the code and carrier range as observed at the repeater location (considering geometric range between the transmit antenna of the repeater and the individual antenna elements) with the code and carrier ranges at the receiver location.

    Instead of the location of the repeater P2, however, any intended location Px could be used to simulate an intelligent spoofer attack (Figure 11).

    The simulator can generate such scenarios by configuring the position of the (re-)transmitting antenna and the intended position (for example, the position of the repeater). By calculating the difference between the real receiver position and the position of the transmitting antenna, the additional delay and free-space loss can be taken into account. The user may also configure the gain of the transmit antenna and the processing time within the repeater. Currently, this setup does only support one “user” antenna to be simulated. However, this feature combined with multi-antenna support will enable the simulator to simulate repeater or intelligent spoofer attacks in the future (Figure 12). To distinguish the “real” signal from the “repeated” signal, the “repeated” signal could be tagged as a multipath signal. This approach would allow simulation of the complete environment of “real” and “repeated” GNSS signals in one single simulator.

    Figure 11. Geometry of repeater/spoofer and GNSS receiver.
    Figure 11. Geometry of repeater/spoofer and GNSS receiver.
    Figure 12. Simulator’s capability to simulate a repeater.
    Figure 12. Simulator’s capability to simulate a repeater.

    Manufacturers

    The simulator producing the results described here is the NavX-NCS from IFEN GmbH. The simulator is valuable laboratory equipment for testing not only standard or high-end single-antenna GNSS receivers, but also offers additional benefit for multi-antenna GNSS receivers like the DLR GALANT controlled reception pattern antenna system.

    The GNSS constellation simulator offers up to four phase-coherent RF outputs, allowing the simulation of four antenna elements with two carrier frequencies, each utilizing one single chassis being 19 inch wide and 2 HU high.

    Simulation of intentional and unintentional interference is a possible feature of the simulator and allows receiver designers and algorithm developers to test and enhance their applications in the presence of interference to identify, locate and mitigate for interference sources.


    Thorsten Lück studied electrical engineering at the universities in Stuttgart and Bochum. He received a Ph.D. (Dr.- Ing.) from the University of the Federal Armed Forces in Munich in 2007 on INS/GNSS integration for rail applications. Since 2003, he has worked for IFEN GmbH, where he started as head of R&D embedded systems in the receiver technology division. In 2012 he changed from receiver development to simulator technologies as product manager of IFEN’s professional GNSS simulator series NavX-NCS and head of the navigation products department.

    Günter Heinrichs is the head of the Customer Applications Department and business development at IFEN GmbH, Poing, Germany.  He received a Dipl.-Ing. degree in communications engineering in 1988, a Dipl.- Ing. degree in data processing engineering and a Dr.-Ing. degree in electrical engineering in 1991 and 1995, respectively. In 1996 he joined the satellite navigation department of MAN Technologie AG in Augsburg, Germany, where he was responsible for system architectures and design, digital signals, and data processing of satellite navigation receiver systems. From 1999 to April 2002 he served as head and R&D manager of MAN Technologie’s satellite navigation department.

    Achim Hornbostel joined the German Aerospace Center (DLR) in 1989 after he received his engineer diploma in electrical engineering from the University of Hannover in the same year. Since 2000, he has been a staff member of the Institute of Communications and Navigation at DLR. He was involved in several projects for remote sensing, satellite communications and satellite navigation.  In 1995 he received his Ph.D. in electrical engineering from the University of Hannover. His main activities are in receiver development, interference mitigation and signal propagation.

  • Innovation: Where Are We?

    Innovation: Where Are We?

    Positioning in Challenging Environments Using Ultra-Wideband Sensor Networks

    By Zoltan Koppanyi, Charles K. Toth and Dorota A. Grejner-Brzezinska

    INNOVATION INSIGHTS by Richard Langley
    INNOVATION INSIGHTS by Richard Langley

    QUICK. WHO WAS THE FIRST TO PREDICT THE EXISTENCE OF RADIO WAVES? If you answered James Clerk Maxwell, you are right. (If you didn’t and have an electrical engineering or physics degree, it’s back to school for you.) In the mid-1800s, Maxwell developed the theory of electric and magnetic forces, which is embodied in the group of four equations named after him. This year marks the 150th anniversary of the publication of Maxwell’s paper “A Dynamical Theory of the Electromagnetic Field” in the Philosophical Transactions of the Royal Society of London.

    Interestingly, Maxwell used 20 equations to describe his theory but Oliver Heaviside managed to boil them down to the four we are familiar with today. Maxwell’s theory predicted the existence of radiating electromagnetic waves and that these waves could exist at any wavelength. Maxwell had speculated that light must be a form of electromagnetic radiation. In his 1865 paper, he said “This velocity [of the waves] is so nearly that of light, that it seems we have strong reason to conclude that light itself (including radiant heat, and other radiations if any) is an electromagnetic disturbance in the form of waves propagated through the electromagnetic field according to electromagnetic laws.”

    That electromagnetic waves with much longer wavelengths than those of light must be possible was conclusively demonstrated by Heinrich Hertz who, between 1886 and 1889, built various apparatuses for transmitting and receiving electromagnetic waves with wavelengths of around 5 meters (60 MHz). These waves were, in fact, radio waves. Hertz’s experiments conclusively proved the existence of electromagnetic waves traveling at the speed of light. He also famously said “I do not think that the wireless waves I have discovered will have any practical application.” How quickly he was proven wrong.

    Beginning in 1894, Guglielmo Marconi demonstrated wireless communication over increasingly longer distances, culminating in his bridging the Atlantic Ocean in 1901 or 1902. And, as they say, the rest is history. Radio waves are used for data, voice and image one-way (broadcasting) and two-way communications; for remote control of systems and devices; for radar (including imaging); and for positioning, navigation and time transfer. And signals can be produced over a wide range of frequencies from below 10 kHz to above 100 GHz.

    Conventional radio transmissions use a variety of modulation techniques but most involve varying the amplitude, frequency and/or phase of a sinusoidal carrier wave. But in the late 1960s, it was shown that one could generate a signal as a sequence of very short pulses, which results in the signal energy being spread over a large part of the radio spectrum. Initially called pulse radio, the technique has become known as impulse radio ultra-wideband or just ultra-wideband (UWB) for short and by the 1990s a variety of practical transmission and reception technologies had been developed.

    The use of large transmission bandwidths offers a number of benefits, including accurate ranging and that application in particular is being actively developed for positioning and navigation in environments that are challenging to GNSS such as indoors and built-up areas. In this month’s column, we take a look at the work being carried out in this area by a team of researchers at The Ohio State University.


    “Innovation” is a regular feature that discusses advances in GPS technology and its applications as well as the fundamentals of GPS positioning. The column is coordinated by Richard Langley of the Department of Geodesy and Geomatics Engineering, University of New Brunswick. He welcomes comments and topic ideas. Email him at lang @ unb.ca.


    GNSS technology provides position, navigation and timing (PNT) information with high accuracy and global coverage where line-of-sight between the satellites and receivers is assured. This condition, however, is typically not satisfied indoors or in confined environments. Emerging safety, military, location-based and personal navigation applications increasingly require consistent accuracy and availability, comparable to that of GNSS but in indoor environments.

    Most of the existing indoor positioning systems use narrowband radio frequency signals for location estimation, such as Wi-Fi, or telecommunication-based positioning (including GSM and UMTS mobile telephone networks). All these technologies require dedicated infrastructure, and the narrowband RF systems are subject to jamming and multipath, as well as loss of signal strength while propagating through walls. In contrast, using ultra-wideband (UWB) signals can, to some extent, remediate those problems by offering better resistance against interference and multipath, and they feature better signal penetration capability. Due to these properties, the use of UWB has the potential to support a broad range of applications, such as radar, through-wall imagery, robust communication with high frequency, and resistance to jamming. Furthermore the impulse radio UWB (IR-UWB), the subject of this article, can be an efficient standalone technology or a component of positioning systems designed for multipath-challenged, confined or indoor environments, where GNSS signals are compromised.

    IR-UWB positioning can be useful in typical emergency response applications such as fires in large buildings, dismounted soldiers in combat situations, and emergency evacuations. In such circumstances, the positioning/navigation systems must determine not only the exact position of any individual firefighter or soldier to facilitate their team-based mission, but also navigate them back to safety. Under these scenarios, a temporary ad hoc network has to be quickly deployed, as the existing infrastructure is usually non-functional, damaged or destroyed at that point. The UWB-based systems may easily satisfy these criteria: (1) nodes placed in the target area can rapidly establish the network geometry even if line-of-sight between nodes is not available, (2) the communication capability allows for sharing measurements, and (3) the node positions may be calculated based on these measured ranges in a centralized or distributed way. Once the node coordinates have been determined, the tracking of the moving units can start. Obviously, the resistance against jamming makes this solution attractive for military applications.

    Ad Hoc Network Formation for Emergency Response

    • Quick deployment
    • Sufficient positioning accuracy
    • Robustness against interference (jamming)
    • Signal penetration through solid structures

    Generally, positioning systems, both local and global, require an infrastructure, which defines the implementation of a coordinate frame. For example, the national reference frames and their realizations support conventional land surveying, or the satellite and the GPS tracking subsystems, as well as the beacons in Wi-Fi systems. UWB positioning also follows the same logic; the network infrastructure defines a local coordinate system and allows for range measurements between the network nodes and the tracked unit(s).

    Ad Hoc Sensor Network: Ad hoc networks are temporary, and thus, the node coordinates are not expected to be known or measured a priori; consequently, they are calculated based on measuring the ranges between the units in the initial phase, and can be updated subsequently if the network configuration changes.

    Anchored Networks: The network nodes’ coordinates are known. If only local coordinates are known, then to connect to a global coordinate frame, at least one node’s global coordinates and a direction vector must be known to anchor and orient the network.

    Anchor-Free Networks: No node coordinates are known, thus the localization problem is underdetermined. Nevertheless, the problem is still solvable, if it is extended with additional constraints.

    Tracking: Once a network is established, static/moving objects can be positioned in the network coordinate system.

     

    Ultra-Wideband Ranging

    At the beginning of the 21st century, the Federal Communications Commission (FCC) introduced new regulations that enabled several commercial applications and initiated research on UWB application to PNT. The current FCC rules for pulse-based positioning or localization implementations require the applied bandwidth be between 3.1 and 10.6 GHz and the bandwidth to be higher than 500 MHz or the fractional bandwidth to be more than 0.2.

    The typical IR-UWB ranging system consists of multiple transceiver units, including the transmitter and the receiver components. The transmitter emits a very short pulse (high bandwidth) with low energy, and the receiver detects the signal after it travels through the air, interacting with the environment. After reaching objects, the emitted pulse is backscattered as several signals, which likely reach the receiver at different times. In contrast, conventional RF signals are longer in duration, thus the backscattered waves overlap each other at the receiver, forming a complex waveform, and may not be distinguishable individually. Due to the shortness of the UWB signals, measurable peaks are nicely separated, representing different signal paths.

    The wave shape of the impulse response of the transmission medium highly depends on the environment complexity due to multipath. Detections in the received wave are determined by a peak-detecting algorithm. Note that the travel time is generally determined from the first detection, as it is assumed to be from the shortest path, although other peak detection algorithms also exist.

    In the experiments discussed in this article, a commercial UWB radio system was used. This sensor’s bandwidth is between 3.1 and 5.3 GHz, with a 4.3-GHz center frequency. Three methods are available to obtain ranges: (1) coarse range estimation, based on the received signal strength with dynamic recalibration; (2) precision range measurement (PRM), which uses the two-way time-of-flight technique; and (3) the filtered range estimates (FRE) method that refines the PRM solution using Kalman filtering. In our investigations, PRM data were used in static situations, when both the unit to be positioned and the reference units were static (such as when determining network node coordinates), and FRE was logged in kinematic scenarios.

    Localization in a UWB Network

    Commercial UWB products usually provide capabilities for all three applications: communication, ranging and radar imaging. In positioning applications, identical units are used for both the rovers — that is, the units to be localized — and the static nodes of the network. The general terminology, however, is that the rover unit with unknown position is called the receiver, and units deployed at known locations are called transmitters. We will also use the terms rover and stations. The positions are typically defined in a local coordinate system. The usual ranging methods used in RF technologies, including signal strength and fingerprinting, time of arrival, angle of arrival, and time difference of arrival, are also applicable to UWB systems. TABLE 1 lists the ranging methods and typical performance levels; the achievable accuracies are based on external references. Note that the accuracy depends on the sensor hardware and network configuration, applied bandwidth, signal-to-noise ratio, peak detection algorithm, experiment circumstances, formation and the environment complexity.

    TABLE 1. Typical accuracy of the different UWB localization techniques. Note that the results depend on the hardware, antenna, applied bandwidth, experiment circumstances and geometric configuration; * denotes indoor environment with area coverage of a few times 10 × 10 meters, with line-of-sight conditions, and ** refers to the maximum error in the outdoor test area of about 100 × 100 meters).
    TABLE 1. Typical accuracy of the different UWB localization techniques. Note that the results depend on the hardware, antenna, applied bandwidth, experiment circumstances and geometric configuration; * denotes indoor environment with area coverage of a few times 10 × 10 meters, with line-of-sight conditions, and ** refers to the maximum error in the outdoor test area of about 100 × 100 meters).

    Signal Strength. The received signal strength (RSS) requires modeling of the signal loss, which is a challenging problem since signals at different frequencies interact with the environment in different ways, and thus the resulting accuracy is generally inadequate for most applications. The fingerprinting approach is also applied to UWB positioning; the signal-strength vector received from the transmitters identifies a location by the best match, where the vector-location pairs are measured in a calibration/training phase and stored in a database.

    Time of Flight. The time-of-flight method requires the synchronization of the clocks of the UWB units, which is difficult, in particular, in the low-cost systems. Therefore, most UWB systems are based on the two-way time-of-flight method, which eliminates the unknown clock delay between the sensors, although it also has its own challenges. The range between two units is obtained by measuring the time difference of the transmitted and received pulses plus knowing the fixed response time of the responding unit.

    Computing Position in a Network. Once the ranges are known in a network environment, the position is determined by circular lateration. The principle for the 2D case with three stations is shown in FIGURE 1. Note that each range determines a circle around the known stations (stations 1, 2 and 3 in the figure), thus, if the stations’ coordinates are known, the unknown position can be calculated as the intersection of these circles. The problem is treated as a system of non-linear equations; note that the lateration requires at least three or four nodes in an adequate spatial distribution for 2D and 3D positioning, respectively. The measured ranges, characterized by the error terms usually modeled with a normal distribution, are depicted by the dotted parallel circles around the solid “perfect” range in Figure 1. Note that this is an optimization problem, which can be solved with direct numerical approximation, such as gradient methods, or by solving the respective linear system after linearizing the problem with close initial position values.

    FIGURE 1. Circular lateration.
    FIGURE 1. Circular lateration.

    Time Difference and Angle of Arrival. The time difference of arrival (TDoA) approach is useful when the time synchronization is not established. The unknown time delays are eliminated by subtracting the travel times between the rover and the stations, and the response time of the responding unit must be known. The location estimation is similar to the time of arrival case, but rather than the intersection of the circles, hyperbolic function curves representing constant TDoA values are used to determine the rover position. Also, if errors are present in the measurements, the position calculation becomes an optimization problem instead of finding the root of an equation. The TDoA can be combined with the angle of arrival (AoA). This method assumes that the set of UWB antennas are arranged in an array, and the angle can be calculated as the time difference of the first and the last detection from different antennas of the array.

    Calibration

    The ranges obtained by UWB sensors could be further improved by calibration — for example, by estimating antenna and hardware delays. In our outdoor tests, the joint calibration model (see Two Calibration Models box) was used, and coefficients of various model functions were estimated. During these tests, the UWB units were placed at the corners of a 15  × 15 meter area (see FIGURE 2).

    FIGURE 2. Outdoor test configuration.
    FIGURE 2. Outdoor test configuration.

    At two diagonal corners, two UWB units with a 1.5-meter vertical separation were installed on poles, while at the two other corners only one unit was used. These six units formed the nodes or the stations of the network. In all cases, a GPS antenna was fixed to the top of the poles to provide reference data. A pushcart with two UWB units, a logging laptop computer, a GPS antenna and a receiver formed the rover system. The reference solution was obtained by using the GPS measurements, with the accuracy around 1 centimeter after kinematic post-processing using precise satellite orbit and clock data. During calibration, the pushcart was collecting stationary data at points 1 to 12, marked on a 5 × 5 meter grid, as shown in Figure 2.

    Two Calibration Models

    1. Individual sensor calibration is the approach where the sensor delays are determined separately, for example, Inno-Cal-E1, where Inno-Cal-E2 is the measured range between stations A and B, Inno-Cal-E3and Inno-Cal-E4 are the calibration functions, and Inno-Cal-E5 is the corrected range.
    2. Joint calibration model is the approach where the calibration function does not provide the offset per station, but rather gives the relative offset between the two stations, where Inno-Cal-E6.

    The calibration model as a function of the measured distance can be constant, linear or a higher-order polynomial.

     

    After acquiring range data between the rover and network stations, three types of joint calibration functions were investigated: constant, linear and polynomial models. The coefficients of these functions were estimated from the measured ranges and GPS-provided reference positions at all grid points. The estimated functions with respect to the six network nodes are shown in FIGURE 3. Our hypothesis was that the accuracy is assumed to depend on the rover-station distance, and thus, the detected discrepancies between the rover and reference points are expected to be higher if the distance is larger. The results indicate that a constant correction (that is, an antenna delay) is generally sufficient, indicating that the calibration may be applicable to similar installations. In some cases, a linear trend (a distance dependency) may be recognized due to slight data changes, but the observed regression lines are either increasing or decreasing, which clearly rejects the distance-dependency hypothesis. The linear and second-order polynomial functions likely model only local effects. The corrections provided by these functions depend on the environment, and consequently, are valid only in that configuration and where they were observed.

    FIGURE 3. Calibration models.
    FIGURE 3. Calibration models.

    Error surfaces, derived as the approximation of a second-order surface from the residuals at the grid points between the receiver and the six station units, show that the discrepancies can be as large as 0.5 meter. Calibrated results using the constant model show that all the discrepancies are less than 10 centimeters with an empirical standard deviation of 3.6 centimeters. This suggests that, at least, the constant-model-based calibration is needed.

    Tracking Outdoors and Indoors

    If the coordinates of the network nodes and the calibration parameters are known, the location of the moving rover can be calculated with circular lateration. The experiment described in this section is based on the same field test as presented earlier. For assessing the outdoor tracking performance, a random trajectory of the pushcart inside and outside of the rectangle defined by nodes was acquired (see FIGURE 4). The reference trajectory was obtained by GPS and the UWB trajectory was calculated with circular lateration.

    FIGURE 4. Trajectory solutions.
    FIGURE 4. Trajectory solutions.

    TABLE 2 presents a statistical comparison of the coordinate component differences between the GPS reference and the UWB trajectory based on calibrated ranges. The mean of the X and Y coordinate differences are around 0 centimeters, and their standard deviations are 9.7 and 13.2 centimeters, respectively, with the largest differences being less than half a meter in both coordinate components. Note that the vertical coordinates have large errors due to the small vertical angle, which translates to weak geometric conditions for error propagation.

    TABLE 2. Statistical results for the coordinate components.
    TABLE 2. Statistical results for the coordinate components.

    Indoor UWB positioning is more challenging than outdoor, as propagation through walls modifies the RF signals resulting in attenuations and delays. Furthermore, the geometric error propagation conditions (that is, the shape of the network) may also reduce the quality of positioning. In the indoor tests, a personal navigation system demonstration prototype built in our lab (shown in FIGURE 5) was used as a rover. During the tests, the person was moving at a normal pace, and the rover unit recorded the ranges from the reference stations. Concerning the network, two point types are defined: (1) network nodes depicted by a double circle in the figure, which are used in the tracking phase; and (2) reference points marked by a single circle, which support the validation of the positioning results.

    FIGURE 5. Indoor test configuration.
    FIGURE 5. Indoor test configuration.

    Since no reference solution was available during the indoor testing, the calibration method’s consistency was evaluated based on the relative or internal accuracy metric, which is the a posteriori reference standard deviation error:

    Inno-Eq1

    where v is the vector of residual errors and r=dim(ATA) – rank(ATAis the degrees of freedom of the network with A being the design matrix describing the geometry of the network. The m0 values are shown in FIGURE 6. This parameter describes the statistical difference of the measurements from the assumed model (circular lateration). The average m0 is 7.6 centimeters without calibration, and higher if any of the outdoor calibration models are used.

    FIGURE 6. The indoor test results showing values of m0 at the epochs.
    FIGURE 6. The indoor test results showing values of m0 at the epochs.

    To estimate the absolute or external accuracy without a reference trajectory, points 1002 and 1004 were used as checkpoints with known coordinates. Obviously, these points were not part of the network. The UWB rover unit was placed at these points, and data were acquired in a static mode. The coordinates were continuously calculated after measuring at least three ranges. TABLE 3 presents the statistical results. Note that the average is not 0, thus the result is biased, indicating that the signal penetration and/or multipath effects are present in this complex indoor environment. Also, note that no calibration was performed, as no indoor calibration results were available, and using the outdoor calibration models only decreased the positioning accuracy. In addition, the standard deviations indicate the average m0 is consistent with the external error for point 1002, while this hypothesis is rejected for point 1004.

    TABLE 3. Differences between the UWB position estimations and the correct coordinates at points 1002 and 1004.
    TABLE 3. Differences between the UWB position estimations and the correct coordinates at points 1002 and 1004.

    Taking a closer look at the results of point 1004, the ambiguity problem of the circular lateration can be observed. The random measurement error can be large enough to cover two possible intersections in circular lateration, thus the estimator may oscillate between two solutions. Two main causes for this ambiguity are a weak network configuration and the large ranging errors (see FIGURE 7).

    FIGURE 7. Ambiguity of lateration.
    FIGURE 7. Ambiguity of lateration.

    Ad Hoc UWB Sensor Network

    We have also carried out tests on an indoor ad hoc sensor network using different coordinate estimation methods. Indoor distance measurements typically do not follow a normal or Gaussian error distribution but rather a Gaussian mixture distribution, which demands the use of a robust estimation method. Our results showed that the maximum likelihood estimation technique performs better than conventional least squares for this type of network.

    Conclusion

    Ultra-wideband technology is an effective positioning method for short-range applications with decimeter-level accuracy. The coverage area can be extended with increasing network size. The technology can be used independently or as a component of an integrated positioning/navigation system. GPS-compromised outdoor situations and indoor applications can be supported by UWB in permanent and ad hoc network configurations. While UWB technology is relatively less affected by environmental conditions, signal propagation through objects or other non-line-of-sight conditions can reduce the reliability and accuracy.

    Acknowledgments

    This article is based, in part, on the paper “Performance Analysis of UWB Technology for Indoor Positioning,” presented at the 2014 International Technical Meeting of The Institute of Navigation, held in San Diego, Calif., Jan. 27–29, 2014.

    Manufacturer

    The experiments discussed in the article used a Time Domain Corp. PulsON 300 UWB radio system.


    ZOLTAN KOPPANYI received his B.Sc. degree in civil engineering in 2010 and his M.Sc. in land surveying and GIS in 2012, both from Budapest University of Technology and Economics (BME), Hungary. He also received a B.Sc. in computer science from the Eötvös Loránd University, Budapest, in 2011. He is a Ph.D. student at BME and was a visiting scholar at the Ohio State University (OSU), Columbus, in 2013. His research area is human mobility pattern analysis and indoor navigation.

    CHARLES K. TOTH is a research professor in the Department of Civil, Environmental and Geodetic Engineering at OSU. He received an M.Sc. in electrical engineering and a Ph.D. in electrical engineering and geo-information sciences from the Technical University of Budapest, Hungary. His research expertise covers broad areas of 2D/3D signal processing; spatial information systems; high-resolution imaging; surface extraction, modeling, integrating and calibrating of multi-sensor systems; multi-sensor geospatial data acquisition systems, and mobile mapping technology.

    DOROTA A. GREJNER-BRZEZINSKA is a professor in geodetic science, and director of the Satellite Positioning and Inertial Navigation (SPIN) Laboratory at OSU. Her research interests cover GPS/GNSS algorithms, GPS/inertial and other sensor integration for navigation in GPS-challenged environments, sensors and algorithms for indoor and personal navigation, and Kalman and non-linear filtering.


    Further Reading

    Authors’ Conference Paper

    Performance Analysis of UWB Technology for Indoor Positioning” by Z. Koppanyi, C.K. Toth, D.A. Grejner-Brzezinska, and G. Jozkow in Proceedings of ITM 2014, the 2014 International Technical Meeting of The Institute of Navigation, San Diego, Calif. January 27–29, 2014, pp. 154–165.

    U.S. Regulations on Ultra-Wideband

    “Ultra-Wideband Operation” in Code of Federal Regulations, Title 47, Chapter I, Subchapter A, Part 15, U.S. National Archives and Records Administration, Washington, D.C., October 1, 2014. Available online.

    Introduction to Ultra-Wideband

    “History and Applications of UWB” by M.Z. Win, D. Dardari, A.F. Molisch, W. Wiesbeck, and J. Zhang in Proceedings of the Institute of Electrical and Electronics Engineers, Vol. 97, No. 2, February 2009, pp. 198–204, doi: 10.1109/JROC.2008.2008762.

    Ultra-Wideband and GPS: Can They Co-exist” by D. Akos, M. Luo, S. Pullen, and P. Enge in GPS World, Vol. 12, No. 9, September 2001, pp. 59–70.

    Ultra-Wideband Signal Peak Detection and Ranging

    Ultra-Wideband Ranging for Low-Complexity Indoor Positioning Applications by G. Bellusci, Ph.D. dissertation, Delft University of Technology, Delft, The Netherlands, 2011.

    “Ultra-Wideband Range Estimation: Theoretical Limits and Practical Algorithms” by I. Guvenc, S. Gezici, and Z. Sahinoglu in Proceedings of ICUWB2008, the 2008 Institute of Electrical and Electronics Engineers International Conference on Ultra-Wideband, Hannover, Germany, September 10–12, 2008, Vol. 3, pp. 93–96, doi: 10.1109/ICUWB.2008.4653424. 

    Received Signal Strength Fingerprinting

    “Increased Ranging Capacity Using Ultrawideband Direct-Path Pulse Signal Strength with Dynamic Recalibration” by B. Dewberry and W. Beeler in Proceedings of PLANS 2012, the Institute of Electrical and Electronics Engineers / Institute of Navigation 2012 Position, Location and Navigation Symposium, Myrtle Beach, S.C., April 23–26, 2010, pp. 1013–1017, doi: 10.1109/PLANS.2012.6236843.

    “Indoor Ultra-Wideband Location Fingerprinting” by H. Kröll and C. Steiner in Proceedings of IPIN 2010, the 2010 International Conference on Indoor Positioning and Indoor Navigation, Zurich, September 15–17, 2010, pp. 1–5, doi: 10.1109/IPIN.2010.5648087.

    Ultra-Wideband Time-of-Arrival and Angle-of-Arrival“Ultra-Wideband Time-of-Arrival and Angle-of-Arrival Estimation Using Transformation Between Frequency and Time Domain Signals” by N. Iwakiri and T. Kobayashi in Journal of Communications, Vol. 3, No. 1, January 2008, pp. 12–19, 10.4304/jcm.3.1.12-19.

    Maxwell’s Equations

    The Long Road to Maxwell’s Equations” by J.C. Rautio in IEEE Spectrum, Vol. 51, No. 12, December 2014, North American edition, pp. 36–40 and 54–56, doi: 10.1109/mspec.2014.6964925.

    A Student’s Guide to Maxwell’s Equations by D. Fleisch, Cambridge University Press, Cambridge, U.K., 2008.

  • Arianespace Soyuz Begins Integration for March 27 Galileo Launch

    The Soyuz launcher for Arianespace’s upcoming mission with two European Galileo navigation satellites is taking shape at the Spaceport for a March 27 liftoff from French Guiana.

    “During activity in the Spaceport’s Soyuz Launcher Integration Building, the medium-lift workhorse began to assume its iconic form with integration of the four first-stage strap-on boosters to the Block A core second stage,” Arianespace wrote in an statement.

    “The next step will be the mating of Soyuz’ Block I third stage to the launcher’s core, completing the basic build-up, and readying the vehicle for its rollout to the launch pad — where the payload will be mated.”

    The March 27 flight will be the 11th Soyuz flight from French Guiana since the launcher’s introduction at the Spaceport in October 2011. It is designated Flight VS11 in Arianespace’s numbering system for its launcher family, which also includes the heavy-lift Soyuz and lightweight Vega.

    For the upcoming Soyuz mission, Arianespace will loft Galileo’s third and fourth Galileo Full Operational Capability (FOC) satellites to further expand the constellation. Flight VS11’s two satellites were built by OHB System, with Surrey Satellite Technology Ltd. supplying their navigation payloads.

    Galileo’s complete operational network and its ground infrastructure will be deployed during the program’s Full Operational Capability phase, which is managed and funded by the European Commission. The European Space Agency has been delegated as the design and procurement agent on the Commission’s behalf.

  • Langley’s Ionosphere Research Focus of CBC Report

    Langley’s Ionosphere Research Focus of CBC Report

    Richard Langley describes the ionosphere study to CBC News reporter Shawn Fowler.
    Richard Langley describes the ionosphere study to CBC News reporter Shane Fowler. (Screen capture from CBC News video)

    CBC News interviewed GPS World Innovation Editor Richard Langley about his ionosphere interference research project with NASA, reported on earlier this week.

    Langley, a professor at the University of New Brunswick, is working with the Jet Propulsion Laboratory in California to better understand how the ionosphere is disturbed by a variety of phenomena including solar outbursts and other natural hazards such as tsunamis. They are using the signals from GPS satellites to probe the ionosphere with the signals being picked up by receivers both on the ground and in low-Earth-orbiting satellites. The research could help find ways to mitigate ionospheric interference to GPS signals themselves as well as to other types of radio communications.

    “GPS satellites are much higher than the ionosphere,” Langley told CBC News reporter Shane Fowler. “So the signals from the satellites have to come down through the ionosphere to receivers on or near the Earth’s surface. And as they come down through the ionosphere they get a little distorted. When you see auroras in the sky, that’s when you can tell the ionosphere is a bit disturbed. The average consumer may not notice these variances, but high-precision applications, like for scientific applications, we actually always see the effect of the ionosphere.”

    Screen capture from CBC news video.
    Screen capture from CBC news video.

    The research could also help develop early-detection systems for tsunamis. “The energy from that water displacement actually propagates up all the way into the atmosphere, all the way to the ionosphere,” Langley told CBC. “It basically moves around the electrons up there and GPS signals coming down from the satellites, through the ionosphere, pick up those small variations. It has the potential to save a lot of lives.”

    Solar flares can also affect GPS signals. The Carrington Event, a solar storm in 1859, knocked out some of Earth’s telegraph systems. “The effect on the Earth’s magnetic field was so strong that currents were set up,” Langley told the CBC. “Those currents were so strong that telegraphs could run without batteries. There was enough current from this disturbance that it could run the telegraphs. And in some cases there was too much and rumour has it started small fires. Luckily we haven’t had one of those again; it seems to be a one-in-100-year, or a one-in-a-200-year, event.”

  • MWC 2015: Rohde & Schwarz Adds Testing for Russia’s Emergency Calling

    Rohde & Schwarz adds ERA GLONASS to its reliable test solution for in vehicle emergency call systems.
    Rohde & Schwarz adds ERA GLONASS to its reliable test solution for in vehicle emergency call systems. Photo: Rohde & Schwarz

    Effective January 1, 2015, all new car models introduced to the Russian market must be equipped with the automatic ERA-GLONASS emergency call system. Rohde & Schwarz now offers a standard compliant test solution for manufacturers and suppliers of these in-vehicle systems.

    Rohde & Schwarz is demonstrating its ERA-GLONASS test setup at Mobile World Congress, being held this week in Barcelona, Spain.

    The test setup consists of the R&S CMW500 wideband radio communication tester and R&S SMBV100A vector signal generator as a GNSS simulator. This setup allows manufacturers and suppliers of automatic in-vehicle systems (IVS) to perform reliable and reproducible pre-conformance tests on their ERA-GLONASS modules in the lab.

    In the Russian Federation, ERA-GLONASS works much like the European Union’s eCall system. When an accident occurs, the IVS connects with a public safety answering point (PSAP) via the local wireless communications network and transmits a standardized minimum set of data (MSD). In addition to GLONASS or GPS coordinates, the MSD also contains data with information about the accident vehicle as specified in ERA-GLONASS. If no voice connection can be made or if data cannot be transferred via the voice channel, the MSD is sent to the PSAP via SMS. This fallback option is a special ERA-GLONASS feature. The Russian system is also certified for 2G and WCDMA networks.

    Rohde & Schwarz developed its R&S CMW-KA095 application software to meet ERA-GLONASS requirements in line with Russia’s GOST specification. Based on the R&S CMW-KA094 eCall software, the R&S CMW-KA095 simulates a PSAP and controls the R&S CMW500 emulating a wireless communications network in the lab. The software also controls the GNSS simulator that supplies the coordinates required for vehicle localization. With this solution, users can verify whether their IVS modem is able to successfully initiate an emergency call, transmit the correct MSD and establish a voice connection with a PSAP. The results are interpreted in line with the GOST specification.

    The ERA-GLONASS SMS protocol has also been integrated into the test solution, making it possible to test the SMS functionality of the IVS modem when no voice connection is available.

    The test solution is fully automated because of the R&S CMWrun sequencer software. The R&S CMW-KT110 eCall/ERA-GLONASS test package provides a user-friendly, automated functional test in line with GOST55330, enabling users to verify the operability of an entire system in the lab and document it in a report.

  • The Accidental Super Power

    Geography Paints Both Rosy and Grim Picture of the World

    In the late ’80s, as a graduate student at UNC Charlotte, I was learning about “New Geography” using a cutting-edge technology called GIS (Geographic Information Systems). One of our professors coined a perfect definition of what made this New Geography different from traditional cataloging of locations and attributes. Quoting Dr. Gerald Ingalls, “Old geography dealt with the simple question: What is where? New geography, using analytical tools such as GIS, is now able to answer: Why what is where.” So knowing the quantifiable “why” hopefully gives us insight into ways to shape and mitigate geography-related problems.

    bookIt’s easy to focus on the technology aspects of GIS and forget the reason for our tradecraft. I was reminded of that reason when I recently read a book that took me back to our geospatial roots and demonstrates New Geography exceptionally well. The book, The Accidental Superpower by Peter Zeihan, effectively uses geography and analytics to explain how the world has been shaped and is evolving. In his book, Mr. Zeihan links many current geopolitical events to geography, demographics and the 1944 Bretton Woods settlement which to me is one of the clearest examples of American exceptionalism.

    Bretton Woods

    For those of you not familiar with Bretton Woods, it was pretty much the United States telling the rest of the world how things will be after the pending end of WWII. The U.S. had turned the tide of war, built up its own industrial power while not suffering home-front damage, and had fashioned the world’s strongest Navy. You can imagine the shock of world leaders when they learned that the U.S. was not looking for reparations or even new land other than enough to bury their dead. Instead, the U.S. was going to open its markets to the world, use its Navy to protect free trade, and even help rebuild devastated countries with programs like the Marshall Plan. All has been pretty good for the past 70 years as Bretton Woods created a global holiday from instability. However, according to Mr. Zeihan, the forces of geography, demographics and new technology will unravel Bretton Woods and slowly change the world.

    The Bretton Woods Conference, 1944.
    The Bretton Woods Conference, 1944.

    Geographic Factors in the Analysis

    We all learned in high school geography that severe climates such as frigid or oppressive tropical climates stifle civilizations, while more temperate climates help civilizations advance. Those are very broad generalizations, but the world is more complex than that, and Peter Zeihan has woven detailed geography into a complex picture of the world. He cites many factors that uniquely and collectively benefit the United States but are shortcomings to a greater or lesser extent in other countries. Key factors included farmable land, rivers and coastal ports for economic trade, oil, industrial capacity, education, demographics and others. In the lottery of world geography, the U.S. has been blessed. I would add that the character of its citizens also plays a key role.

    MS "E.R. Shanghai"

    Although there are critics of some of Zeihan’s conclusions and predictions, there is no doubt that his book is an exceptionally detailed compendium of countries and the geopolitical pressures that affect them. He focuses strongly on the presence of rivers, since they provide very cheap transportation of commodities thus reducing the need for many transportation infrastructure projects. The book gets into great detail about countries that most of us can’t even point to on a world map such as Kazakhstan, Turkistan, Uzbekistan and other stans. He explains why many factors bode well for Uzbekistan, but not so much for Russia and China. He shows why Russia considers keeping Ukraine in its camp absolutely vital to its own survival.

    One surprise was the case he built that Alberta, Canada, may be motivated to leave its non-supportive national government to join a more like-minded and geographically connected United States. This would completely open the U.S. market for Alberta grain and oil while providing seamless transportation throughout the U.S. Additionally, as a state, the Keystone pipeline would not fall under State Department or executive review.

    Demographics

    Mr. Zeihan addresses the importance of demographics using a well-known example, Japan. Low birth rates and limited immigration have placed Japan into the difficult position of supporting an increasingly older population with fewer and fewer young citizens. This inverted population pyramid is a pure numbers issue that cannot be solved quickly. He shows how many European countries are trending in the same direction on a slightly later schedule. Russia is suffering from both lower birth rates and decreased education of its population. By contrast, better birth rates and better educated immigrants are preventing an inverted pyramid here in the U.S.

    Technology

    Mr. Zeihan highlights technology as playing an important role in raising or lowering the importance of some geographic factors. Two in particular have snuck up on the radar: fracking and 3D printing. Who would have thought that the U.S. would be on a path to becoming the world’s largest energy producer thanks to fracking? This will obviously diminish our need for Mideast oil and have a very serious effect on small unfriendly oil producers such as Venezuela, who is already seeing a drop in sales of its relatively hard-to-refine black oil. (Note the political unrest there this week as oil revenues decline.)

    I wrote about the potential impact on industry of 3D printing last year, and Peter Zeihan seems to share that opinion. As manufacturing moves closer to the consumer, jobs in China will decline, as will the need of transoceanic shipment of finished goods. The result: the U.S. will see a rebirth of local manufacturing.

    Rings containing superconducting magnets will confine the plasma inside the reaction chamber. (Credit: Eric Schulzinger/Lockheed  Martin)
    Rings containing superconducting magnets will confine the plasma inside the reaction chamber. (Credit: Eric Schulzinger/Lockheed Martin)

    If fracking and 3D printing are going to be significant factors, imagine what will happen to the world order if the recent announcement by Lockheed Martin that its researchers have cracked compact fusion comes to fruition. This was announced too late for inclusion in Mr. Zeihan’s book, but my guess is that he would consider it to be the quintessential game changer. It would affect many geographic factors — lower the cost of all transportation, expand industry, desalinate water cheaply, make marginal land farmable, negate the limitations of oil/gas access and do all of this while reducing pollution, increasing safety and eliminating the ability to militarize this form of nuclear power.

    Conclusion

    I was only able to touch on a few key points in Peter Zeihan’s book. The total picture is very complex. It was clearly well researched and logically thought through. I have only two criticisms. First, Mr. Zeihan stated that he has “always loved maps,” but this book has mediocre black-and-white maps that are less than ideal to display complex geography. It screams for decent color maps, if not in print at least as supplemental website PDFs.

    Second, the book delves into significant predictions that I believe should be read with a very critical eye. There are many wild cards and personalities that can steer geopolitics. As a former analyst for the geopolitical security firm Stratfor, Mr. Zeihan worked for George Friedman, the co-author of the 1991 book The Coming War with Japan. I’m glad that didn’t come true.

    I know that for many of you working in the intel community this will be very basic information and analysis that is your daily bread and butter. For the rest of us, it’s a good overview and I recommend getting this book. It will be a handy reference, if for no other reason than to sound knowledgeable at water cooler debates. However, I believe that its value is more serious than that and will prove repeatedly useful as an overarching insight as history unfolds.

  • what3words Uses 3 Words as Coordinates to Identify Location

    what3words explains its coordinates system based on words while at the 2015 Esri Federal GIS Conference, held Feb. 9-10 in Washington, D.C. what3words splits Earth’s surface into 57 trillion 3-meter by 3-meter squares, and gives each square a unique combination of three words — replicated in eight languages — that identifies the area.