Tag: GNSS

  • NovAtel SAASM to See First Action in Aerial Drones

    The new OEM625S Selective Availability Anti-Spoofing Module (SAASM) GNSS receiver from NovAtel, launched in a cooperative effort with SAASM expert L-3 Interstate Electronics Corporation (IEC), will get its first applications in the unmanned aerial vehicle (UAV) sector. NovAtel has brought forth the new product in part to meet requirements of UAV manufacturers who are now mandated to have SAASM onboard as well, for in-theater operations in areas of military activity.

    “The new SAASM regulations meant that integrators were looking at having to incorporate another receiver alongside their NovAtel unit, complicating user interface factors and increasing onboard space requirements,” said NovAtel Product Manager Neil Gerein. “The OEM625S gives our customers a drop-in form factor that easily replaces their existing NovAtel OEM receiver.”

    “NovAtel has supplied UAV integrators on the civil scientific side almost since our inception,” Gerein said, adding, “the military has become more and more involved in this market in recent years for budget and various other strategic reasons.” He mentioned that in its 20-year history selling GPS products, for the last 17 years NovAtel has provided receivers and expertise to U.S. and Canada defense contractors, and to defense research labs in Allied countries. Antcom, a wholly-owned NovAtel subsidiary specializing in antennas and microwave products, makes the majority of its sales into military areas.

    Examples of such products in this area — not necessarily from NovAtel customers, who remain unidentified — include hand-launched mini-UAVs like the Aerovironment RQ-11 Raven and Elbit Skylark I, and runway-capable tactical UAVs such as Textron RQ-7 Shadow, Aeronautics DS Aerostar, IAI Searcher II, and InSitu’s ScanEagle UAV system, quickly evolving into a mainstay with the U.S. Navy and its allies thanks to a partnership with Boeing.

    The InSitu ScanEagle was first developed to track dolphins and tuna from fishing boats, to ensure that fish labeled “dolphin-safe” actually are so. The same characteristics needed by commercial fishing boats — low infrastructure launch and recovery, small size, 20-hour long endurance, automated flight patterns — are key for naval operations from larger vessels, and for battlefield surveillance.

    At present the OEM625S, combining a commercial dual-frequency NovAtel GNSS receiver with an L-3 IEC XFACTOR SAASM, provides single-point positioning with SAASM for authorized defense customers. The SAASM position is provided via a dedicated communication port, as well as through NovAtel’s software command protocol, allowing for maximum flexibility. The small form factor and low power consumption expands range of potential defense applications requiring robust SAASM GPS positioning.

    The OEM625S measures 60 x 100 x 9.1 millimeters, and runs on field-upgradeable software. NovAtel will accept orders for the OEM625S from authorized customers starting in Q3 2012.

  • Survey/GIS Editor Eric Gakstatter to Conduct GPS/GNSS Workshop at East Carolina University May 10, 2012

    GPS World Survey/GIS editor Eric Gakstatter will conduct a one day workshop at the East Carolina University Center for Geographic Information Science in Greenville, NC on May 10, 2012. The workshop is suited for professional GPS/GNSS users in GIS, land surveying, engineering, construction, agriculture, and other high precision applications.

    Workshop Theme:

    “GNSS technology is going to change much more in the next five years than it has in the past five years”

    Workshop Topics:

    1. GPS/GNSS: How does it work and how accurate is it?
    2. What is GNSS and what can it do for me?
    3. Market survey of professional and consumer GPS/GNSS receivers.
    4. The future of GPS/GNSS receivers. New signals? How much? How accurate?
    5. Real-time corrections or post-processing. Which should I use?
    6. Sources of real-time corrections. Free and subscription-based.
    7. Source of post-processing software and data.
    8. GPS/GNSS for high-precision GIS: The value and the headaches.
    9. Evaluating GPS/GNSS equipment: Which one is right for you?
    10. How to measure the accuracy of a GPS/GNSS receiver. Accuracy vs. Precision
    Venue:
    East Carolina University Center for Geographic Information Science
    Greenville, NC USA
    Date/Time:
    Thursday, May 10, 2012. 8:30a – 5:00p
    Click here for details and registration form.
  • Spectra Precision Introduces ProFlex 800 GNSS for Positioning Applications

     

    Spectra Precision introduced today the new ProFlex 800, a GNSS solution with Z-Blade GNSS-centric technology. The ProFlex 800 delivers fast and reliable RTK positioning, even in environments where GNSS signals may be difficult to acquire, Spectra Precision said. Rugged and IP67 rated, the ProFlex 800 is built to withstand harsh operating conditions for a variety of positioning applications.

    “The ProFlex 800 is an ideal solution for customers wanting a single GNSS receiver for multiple applications,” said François Erceau, general manager of Trimble’s Spectra Precision, Nikon and Ashtech Business Area. “It offers a unique design with a range of mounting and communications options.”

    Used as a backpack rover or reference station, the ProFlex 800 with Z-Blade technology is a flexible GNSS solution for land surveying. Its innovative design also makes it ideal for hard-mounted survey applications such as coastal work, dredging, bathymetry or offshore vessel operations.

    The weatherproof, high-impact-resistant molded aluminum housing allows the ProxFlex 800 to operate in harsh conditions.

    In addition to a 3.5G internal cellular modem, the ProFlex 800 can use a variety of internal or external UHF modules, providing stable and reliable wireless communications. It can be used as a rover or a base without additional accessories in the field. Its Z-Blade long-range RTK capability combined with industry-leading UHF options help to ensure maximum productivity while in the field.

    With its built-in Ethernet capability and embedded web server, users can access the ProFlex 800 from any computer connected to the Internet. This capability allows instant real-time multi-data streaming over an Ethernet connection to build an RTK corrections server without any additional software or equipment, the company said.

    Spectra Precision ProFlex 800 CORS Receiver. The Spectra Precision ProFlex 800 is also available as a Continuously Operating Reference Station (CORS). This configuration is an optimal solution when collecting, storing and transferring high-quality GNSS raw data for post processing surveys, geodetic and other applications. Automatic sessions programming, a user-friendly Web-interface, an embedded RINEX converter, FTP push functionality and many other advanced CORS features make the ProFlex 800 CORS a powerful, robust and easy-to-use GNSS solution.

    Advanced Ashtech Z-Blade Technology. Z-Blade is a new GNSS centric signal processing technology. Z-Blade uses all of the available satellite signals equally, without preference to any particular satellite constellation, maximizing the user’s ability to obtain reliable GNSS positions in tough conditions. Z-Blade allows users to receive and maintain RTK positioning even if GPS coverage is insufficient. In many work locations, just a few GPS and GLONASS satellites may be visible due to obstacles such as trees or buildings.

    The ProFlex 800 is now available through the Spectra Precision global dealer network. For more information visit: www.spectraprecision.com and www.ashtech.com or email: [email protected]

  • Hemisphere GPS Introduces miniEclipse Compact OEM Modules with GNSS Support

    Today, Hemisphere GPS announces the Eclipse P300 and Eclipse P301 OEM modules — its next-generation high‑performance compact modules for RTK GNSS applications. Based on new Hemisphere GPS multi-function application firmware and Eclipse GNSS multi‑constellation technology, P300 and P301 provide the ability for tracking commercially available GNSS signals for precise positioning.

    P300 is a drop-in board replacement for Hemisphere GPS’ successful Crescent L1 board as well as the first‑generation miniEclipse P200 GPS-only OEM board. P301 is the company’s 20‑pin OEM module configured as a drop-in replacement for a different industry standard interface. Eclipse P300 and P301 improve GNSS positioning performance, particularly with RTK applications, through Hemisphere GPS’ patent-pending SureTrack technology. Benefits include extended and more robust RTK solutions as the rover RTK receiver will process all available signals even if they are not common with the base receiver. RTK solutions are therefore better maintained in challenging environments, with baselines of up to 50 km, and reacquisition times are improved resulting in more robust overall performance, the company said.

    P300 and P301 are designed for OEM system integrators who demand the highest level of multi-frequency positioning, accuracy, fast initialization time, and GNSS RTK solutions. Hemisphere GPS’ miniEclipse series includes a single frequency L1 GPS + L1 GLONASS model named P202. Both series are designed for developing integrated high-precision and control applications for geomatics, survey, machine control, and unmanned vehicle solutions.

    “P300, P301, and P202 all improve upon our already successful miniEclipse OEM modules adding GNSS support to our most compact modules for excellent accuracy and affordability,” said Phil Gabriel, vice president and general manager, Precision Products, for Hemisphere GPS. “System integrators have a wider range of Hemisphere GPS solutions from which to choose to develop world‑class high‑precision products.”

    Measuring 71 mm long and 41 mm wide, miniEclipse allows for easy integration, especially for integrators who are accustomed to Hemisphere GPS’ Crescent and miniEclipse OEM module performance and footprint.

    All miniEclipse modules are available through the Hemisphere GPS Precision Products global dealer network.

  • Bluetooth Group Adopts GNSS Standard

    The Bluetooth Special Interest Group, which publishes specifications for Bluetooth, has adopted the GNSS Profile version 1.0 for devices using Bluetooth 2.0 and up. The GNSS profile provides a means for a GPS enabled device to share its position data with another device via a Bluetooth wireless technology based connection.

    The unified standard, which has been in progress for several years, will likely make it easier for location-aware Bluetooth devices to share information. Currently, devices can use proprietary formats or other formats not covered by the Special Interest Group. Developers can download the profile here (PDF).

    Revision history on the standard began in 2006, with a two-year gap in 2009 and 2010.

  • The System: Glitches and Vulnerabilities

    A range of unrelated events in September show that GPS, the world’s preeminent GNSS, remains a work in progress.

    The first in a series of deviations from normal GPS signal broadcasts during September was noted by researches at the University of New Brunswick, among others around the globe, who found that normal signals from the L1 and L2 transmitters on the GPS satellite PRN01/SVN49 were unavailable for more than two hours on the morning of September 4.

    The satellite did not transmit useful signals on L1 and L2 from about 12:00 to 14:11 UTC, as reported by International GNSS Service stations in Europe. The L5 test signal continued to be tracked by some receivers but not others.

    One possible explanation for the inability to track PRN01 is that the satellite rejected an upload and automatically went into non-standard mode, resulting in GPS receivers being unable to track the L1 and L2 signals. In other words, the L1/L2 transmitters were still on but transmitting a non-standard signal.

    “It is not known for sure what actually happened with the satellite, but perhaps it is related to the ongoing issues with the signal reflections on the satellite and that the GPS Wing was conducting further tests,” said Richard Langley, GPS World’s Innovation editor and professor at the University of New Brunswick. “Luckily, the problem was short lived.” As to why some receivers continued to track the L5 signal but others did not, Langley speculates that some receivers may need to acquire and track the L1 signal before they can track the L5 test signal.

    HDOP Warning. On September 10, the U.S. Coast Guard Navigation Center (USCG NavCen) issued a high dilution of precision (DOP) warning for certain locations in the U.S., Asia, and Oceania, reporting that GPS users might experience a temporary degradation in GPS reception in parts of the southwest and central United States from 13:02 UTC to 13:23 UTC on September 11.

    “The warning is based on a best-four satellite scenario: what the DOPs would be if we only used the best four satellites (the combination providing the lowest DOP value) of all the satellites in view at a particular location,” said Langley.

    “However, most civil receivers these days track eight or 10 or all satellites in view. I contacted the Coast Guard about this, and they did another analysis and confirmed DOP spikes for all-in-view users too. Prompted by that, I did my own analyses and found that with PRN31 out of action for the delta-V and PRN01 not yet declared healthy, only five satellites above 5 degrees elevation angle (and almost colinear in the sky) will be visible at the stated locations and times, resulting in GDOP spikes approaching 100!

    “So, in this case, the warning is for all users in the affected areas, not just receivers with only four channels.”

    Although a window stretching from 00:30 to 15:00 UTC had been allocated for the PRN31 delta-V maneuver, prompting the high DOP alert, the GPS Wing avoided any problem to users by delaying the start of the operation until 01:27 UTC and completing it in little more than one hour. The satellite was back on line by 02:37 UTC.

    Sat Moves. After 22:00 UTC September 12, system operators began transitioning satellite SVN25 (PRN25) into the broadcast almanac for all satellites. Meanwhile, they moved satellite SVN24 (PRN24) out of the almanac.

    The current GPS operation control system (OCS), known as AEP, cannot handle 32 satellites. However, the recent move gave rise to speculation that the maximum number of operable satellites has now been reduced from 31 to 30, for some reason. Apparently, the military cannot allow more than 30 space vehicles to be in active service at any one time. So when a new SV is activated, one must be deactivated. SVN24 will be placed in caretaker status, ready to be brought back on line should the situation change or the 30 SV limit be overcome.

    Recent pronouncements by GPS Wing personnel on the benefits of the next operating system, OCX, have stated that it will be able to handle many more satellites, as many as 60. This figure now appears in doubt.

    Russian Vision. Grigory Stupak and Mark Shmulevich reported Russia’s plans to restore a full GLONASS constellation of 30 space vehicles, laying out a road map leading to full interoperability with GPS. They envisaged a world orbited by 117 navigation satellites, with GLONASS operating alongside GPS, Galileo, and China’s COMPASS, supported by a further 29 augmentation satellites. That would certainly mitigate many of the vulnerabilities of GNSS due to propagation effects — but not those from interference in the frequency bands they will all share.

    Solutions Sought to GNSS Vulnerabilities

    Baska conference report by David Last

    The second conference on GNSS Vulnerabilities and Solutions, September 2–5 in Baska, Croatia, focused on GNSS vulnerability to space weather, unintentional interference, jamming, and multipath propagation.

    The conference was a joint venture by the Royal Institute of Navigation, London, and Nottingham University’s Institute of Engineering Surveying and Space Geodesy. Sixty-four delegates, mostly European, came from 21 countries.

    Nearly half the papers focused on space weather and ionospheric and tropospheric propagation, taking in long-term and short-term solar effects, scintillation, signal attenuation, tropospheric delay variations, meteorological influences, and even gravity waves. The approach of the physicists was: Understand these things and maybe you can mitigate your vulnerability to them.

    GNSS vulnerability can threaten safety-critical and mission-critical systems, including navigation in the air, maritime automatic identification systems, and the transportation of nuclear waste and other dangerous materials on land. Mitigations include EGNOS (the European WAAS) and GBAS (ground-based augmentation systems.)

    Road Tolling. An unexpectedly hot topic was the enthusiasm of European governments to deploy road-user charging schemes based largely on GNSS technology. Some say road pricing is a rare and novel case of GNSS users who are hostile to the technology and seeking to exploit its vulnerability to the maximum. To enforce charges through the legal system may require levels of integrity approaching those of aircraft instrument-approach systems.

    Suggestions for jamming defenses came mostly from Germany: Ulrich Engel and Angelika Hirrle proposed exciting new mathematical techniques to help separate GNSS signals from noise and interference, while Michael Felux sought refuge in low-cost inertial systems.

    Hank Skalski of the U.S. Department of Transportation laid out U.S. government plans to detect and track down sources of GPS jamming. The SETS (Space Event Tracking System) will deploy aircraft, vans, fixed-base units, and trained technicians.

    See Last’s report on low-cost jammers in criminal employ in Expert Advice, October 2009.

    Smartpath Approved

    The U.S. Federal Aviation Administration (FAA) has certified Honeywell’s Smartpath precision-landing system for airport installations. As this magazine went to press, neither the FAA nor the Department of Transportation had issued an official release, but industry contacts were notified in mid-September.

    The ground-based augmentation system provides aircraft with precise navigation data for CAT I approaches and landings, enabling closely spaced parallel and curved path approaches to increase airport capacity. It asserts improved navigation accuracy over instrument landing systems (ILS), using differential GPS and broadcasting both pseudorange corrections for each satellite in view as well as approach path information in a digital broadcast.

    According to Honeywell, most current-production Airbus and Boeing aircraft now carry GBAS avionics or offer it as an option. Future Smarpath upgrades include the ability for CAT III approaches.

    Arctic Passage Traversed by Merchant Ships

    Two German merchant ships traversed the Northeast Passage from South Korea, leaving in late July, to Siberia, and plan to continue their journey to Rotterdam in the Netherlands.

    A sea lane traditionally blocked by heavy ice floes or solid sheet ice, this route has opened because of to global warming. In 2007, Arve Dimmen, director of maritime safety for Norway’s Coastal Administration, told the U.S. National Space-Based Positioning, Navigation, and Timing Advisory Board that disappearing ice across the Arctic poses potential threats: 25 percent of undiscovered oil resources lie in that region, and the route could now be used by supertankers and large container ships, as it is more economical and less time-consuming.

    Precision navigation faces more challenges north of the Artic Circle, from atmospheric affects in polar regions and the low elevation of SBAS satellites at those latitudes. A June 2009 study on GNSS use in the high Arctic by Richard Langley, however, found that conventional horizontal (marine) navigation works well north of the Arctic Circle. Still, others held that “this is another reason why eLoran is so important: someone at USCG/State/Commerce needs to use this as a wake-up call!”

     
    Created from nearly 200 Envisat scenes, this Arctic mosaic reveals that the most direct route of the Northwest Passage (the orange line) across northern Canada is fully navigable. The blue line traces the Northeast Passage along the Siberian coast, which is only partially obstructed by ice; see story, page 16. Envisat advanced synthetic aperture radar mosaic produced by the Danish National Space Center.
  • Integer ambiguity validation: Still an open problem?

    By Sandra Verhagen

    High-precision Global Navigation Satellite System (GNSS) positioning results are obtained with carrier phase measurements, once the integer cycle ambiguities have been successfully resolved.

    The position solution is obtained in four steps:

    1. Float solution:least-squares, discarding integer nature.

    2. Integer solution: real-valued float ambiguities mapped to integer-valued ambiguities.Examples of integer estimators (Teunissen, 1998a):

    • Integer Least-Squares: optimal, requires search to obtain solution.
    • Integer Bootstrapping: may perform close to optimal (decorrelating ambiguity transformation required), no search required (e.g. widelaning, CIR, TCAR).
    • Integer Rounding: the simplest of all methods.

    3. Integer acceptance test: decision whether or not to accept integer ambiguity solution. Examples: ratio test, distance test, projector test.

    4. Fixed solution: if the integer solution is accepted, the fixed baseline is computed.

    The third step is often referred to as the ‘integer validation’ problem. In Verhagen (2004) this problem was addressed, and different approaches were compared.

    As an example, we will now consider the popular ratio test, which is defined as:

    Source: GPS world staff

    Where ȃ is the float solution with Qȃ, the corresponding variance matrix; and ă and ă’, the corresponding integer estimate and the second-best integer candidate, respectively; δ is the critical value. Note: in practice, often the reciprocal of the ratio test, as specified here, is used.

    The underlying principle of the ratio test can be explained with a 2-dimensional example, see the figure below. Assume we have two ambiguities in our model. The black hexagons are the so-called integer least-squares pull-in regions: if the float ambiguity estimate falls inside a certain hexagon, the integer solution is equal to the grid point in the center of this pull-in region. Applying the ratio test, however, implies that this integer solution is only accepted if it falls inside one of the red regions. Otherwise, the float ambiguity is considered to be too close to the boundary of a pull-in region, such that the integer solution is not sufficiently more likely than the second-best integer candidate.

    RTIA-web

    Note that the size of the regions is controlled by the critical value, δ, see Verhagen and Teunissen (2006), and Teunissen and Verhagen (2007), where it is described how this value should be chosen.

    It can be seen that the acceptance regions are invariant for translations with an integer value. As such, the ratio test is invariant to integer biases. In fact, the ratio test is not suitable for testing the correctness of the solution. A model error, such as a bias in the observations, will propagate into the float ambiguities, but it does not necessarily mean that the float ambiguity will be close to the boundary of a pull-in region.

    Hence, the ratio test is not a model validation test, and should only be applied in order to test whether or not the integer solution can be regarded sufficiently more likely than any other integer candidate.

    With regard to GNSS model validation, we can make the following remarks:

    1. Classical testing theory based on statistical hypothesis testing is not applicable due to the integer nature of the carrier-phase ambiguities (Teunissen, 1998b).

    2. Testing theory for testing the presence/absence of a model error is not yet available.

    3. Questions that need to be answered are:

    • What are the appropriate test statistics?• How are they distributed under the null-hypothesis and alternative hypothesis?
    • What are the appropriate acceptance/rejection regions?

    References

    Teunissen, P.J.G. (1998). “A class of unbiased integer GPS ambiguity estimators.” Artificial Satellites, 33(1): 4-10.

    Teunissen, P.J.G. (1998b). “GPS carrier phase ambiguity fixing concepts.” In: Teunissen, P.J.G. and A Kleusberg. GPS for Geodesy, Springer-Verlag, Berlin.

    Teunissen, P.J.G. and Verhagen, S. (2007). “GNSS phase ambiguity validation: a review.” Proceedings Space, Aeronautical and Navigational Electronics Symposium SANE2007, The Institute of Electronics, Information and Communication Engineers (IEICE), Japan, 107(2): 1-6.

    Verhagen, S. (2004). “Integer ambiguity validation: an open problem?” GPS Solutions, 8(1): 36-43.

    Verhagen, S. and Teunissen, P.J.G. (2006). “New global navigation satellite system ambiguity resolution method compared to existing approaches.” Journal of Guidance, Control and Dynamics, 29(4): 981-991.

    Dr.ir. Sandra Verhagen,
    DEOS-MGP, TU Delft