Author: GPS World Staff

  • Averna and Skydel Join for Demonstrations at ION GNSS+

    Averna and Skydel Join for Demonstrations at ION GNSS+

    Averna and Skydel Solutions will be showcasing their latest GNSS technology simulation products at The Institute of Navigation (ION) GNSS+ conference, giving show-goers the opportunity to see the RP-6100 in action.

    ION GNSS+, taking place Sept. 14-18 in Tampa, Fla., is the 28th International Technical Meeting of the Institute of Navigation’s Satellite Division and the world’s largest technical meeting and showcase of GNSS and related technology, products and services.

    The companies will be presenting at Booth #100 in the Exhibit Hall, meeting attendees and discussing their latest innovations in GNSS receiver validation, among other topics. They will also be demonstrating two new GNSS solutions:

    • RP-6100 Multi-Channel RF Record & Playback: The RP-100 for RF application testing allows users to tecord real-world signals such as GNSS, HD Radio, LTE and Wi-Fi — plus impairments — to significantly advance projects and harden product designs.
    • GNSS Simulator: New from Averna’s partner Skydel Solutions, this innovative and cost-effective simulator is entirely software driven. It’s a perfect fit with the RP-6100, Averna said, enabling users to test corner cases and future events with a real-time GNSS solution.
    Averna RP-6100 record and playback solution. (PRNewsFoto/Averna)
    Averna RP-6100 record and playback solution. (PRNewsFoto/Averna)
  • TESSCO Introduces Fleet Management Solution at CTIA Super Mobility

    TESSCO Technologies is introducing a low-cost investment vehicle tracking, monitoring and control solution at CTIA Super Mobility, being held Sept. 9-11 in Las Vegas. TESSCO is a provider of the product and value-chain solutions required to build, use and maintain wireless systems. The company is displaying the fleet management solution at booth 5932.

    “Spending in the U.S. logistics and transportation industry totaled $1.33 trillion in 2012. However, fleet management systems have remained largely disjointed and costly for smaller fleets. Our Fleet Management Solution provides choice, convenience, best-in-class products and a total source for all of the elements needed to deploy a management solution faster and at the lowest cost investment,” said Steven Tom, TESSCO VP of Analytics, Innovation & Learning. “We provide the expertise and service built on our deep experience in wireless networks and in-vehicle communications. We deliver the end-to-end products and services including sensors, telematics, vehicle mounts and internet connectivity.”

    Join Steven Tom for his presentation “The Road Ahead: The Future of Fleet Management and Telematics” on the Networked Society & Startup Stage at 2:30 p.m. on Wednesday, Sept. 9. He will share details about the new product offering as well as look ahead to the future of fleet management.

  • GPS-Guided Artillery Rounds Will Arm Dutch Howitzers

    GPS-Guided Artillery Rounds Will Arm Dutch Howitzers

    The latest variant of the Excalibur precision-guided projectile will be used by armies and be available for naval ships.
    The latest variant of the Excalibur precision-guided projectile will be used by armies and be available for naval ships.

    The Netherlands Ministry of Defense is adding Raytheon Company’s Excalibur Ib artillery rounds to its arsenal under a previously announced foreign military sales agreement, underscoring growing international interest in the precision-guided projectile.

    The Netherlands is the second Excalibur lb customer in Europe after Sweden, the U.S. government’s development partner for the 155-mm round. Deliveries are expected to begin later this year.

    “The Netherlands joins a growing list of nations acquiring this highly sophisticated artillery munition, which uses GPS guidance to provide accurate, first-round effects capability at extended ranges,” said Mark Hokeness, Raytheon’s Excalibur program director. “When fired from the Dutch PzH 2000 artillery system, Excalibur can fly up to 50 kilometers, score a direct hit and deliver lethal effects in all types of weather and battlefield conditions.”

    A Dutch Panzerhaubitze 2000 fires a round in Afghanistan. (Courtesy Dutch Ministry of Defense)
    A Dutch Panzerhaubitze 2000 (PzH 2000) fires a round in Afghanistan. (Image courtesy Dutch Ministry of Defense)

    The U.S. Army has determined Excalibur Ib is fully compatible with the PzH 2000, a self-propelled howitzer produced in Germany and fielded by several nations.

    The 
Excalibur precision-guided, extended-range projectile uses GPS guidance to provide accurate, first-round-effects capability in any environment. Excalibur’s level of precision delivers a major reduction in the time, cost and logistical burden associated with using other artillery munitions. Excalibur has been fielded by the U.S. Army, Marines and several international military forces.

    Excalibur Facts

    • Combat-proven: Nearly 770 Excalibur rounds have been fired in combat with exceptional accuracy and lethality.
    • Precise: Excalibur consistently strikes less than two meters from a precisely-located target, Raytheon said.
    • Safe: Excalibur’s precision avoids collateral damage and has been employed within 75 meters of supported troops.
    • Affordable: With its first round effects, Excalibur reduces total mission cost and time and the user’s logistics burden, according to Raytheon.
    • Evolving: Raytheon has demonstrated a dual-mode GPS/semi-active laser seeker Excalibur variant to compensate for target location error, maintain precision in GPS denied or degraded environments, and enable engagement of relocated or moving targets.
    • Navies: With Excalibur N5, navies will be able to deliver extended range, precision naval surface fires from existing 5-inch/127-mm guns.

    Excalibur Video

  • SBG, Viametris Present 3D Indoor Scanning System at INTERGEO

    SBG, Viametris Present 3D Indoor Scanning System at INTERGEO

    The iMS 3D indoor mapping system by Viametris uses an Ellipse-A by SBG for roll and pitch data.
    The iMS 3D indoor mapping system by Viametris uses an Ellipse-A by SBG for roll and pitch data.

    SBG Systems will join Viametris in presenting a new 3D indoor scanning system at the INTERGEO trade show, which will be held Sept. 15-17 in Stuttgart, Germany.

    The iMS 3D is a mobile 3D indoor scanner generating continuous point clouds. For this brand-new model of indoor mobile mapping system, or iMMS, Viametris chose SBG Systems’ miniature Attitude and Heading Reference Sensor (AHRS), the Ellipse-A. The iMS 3D is easier to transport, install and set up than previous iMMS. The iMS 3D also integrates new sensors, including the Ellipse-A from SBG Systems.

    Based on the SLAM technology, the iMS 3D is equipped with three lidar profilers, each taking 40,000 points per second. The main lidar provides the horizontal profile, which also contributes to the continuous calculation of the iMS 3D position in the building. Two lateral lidars give vertical profiles, including the ceiling. While the user walks, pushing the iMS 3D at normal speed, the 3D profile of the room appears on the screen, since the system records 3D measurements of the same room. Easy to manipulate, one person is enough to survey every corner of the building with the iMS 3D.

    During the survey, the 360-degree camera takes a spherical picture every two meters for a full documentation of the building. This solution makes indoor survey 10 times quicker than traditional methods usually using distance meters, Viametris said, adding that the iMS 3D delivers a combination of point density, acquisition speed and accuracy suitable for the building trade industry.

    At the office, the user accesses a centimeter-level accuracy 3D survey as a point cloud and pictures by using the Viametris processing and browsing software. The user can import the point cloud in CAD software (Autodesk Revit, AutoCAD, MicroStation, Rhino, etc.) to easily produce 2D maps or 3D models. The point cloud can be colorized with the colors of the pictures taken during the survey, which greatly improves the environment understanding. Additionally, the user has access to contextual 360-degree pictures, making objects such as radiators, extinguishers or lights simple to distinguish and locate.

    Ellipse-A.
    Ellipse-A.

    Already integrated in other Viametris ultraportable technologies, the Ellipse-A has been chosen for this new generation of indoor mobile mapping system, or iMMS. “We integrated an Ellipse-A in our 2D system and were very happy with the results. It was obvious to us that the Ellipse-A will be part of our new iMMS,” said Jérôme Ninot, president of Viametris. The Ellipse-A is used to correct the horizontal profile. While the user is pushing the iMS 3D through the rooms, unevenness, slopes and ramps, cables or door thresholds can cause noise in the point cloud. The Ellipse-A keeps the point cloud clean by correcting the horizontal lidar data frames used to build the trajectory.

    The Ellipse-A AHRS provides roll and pitch data accurate to 0.2° at 200 Hz. “The Ellipse sensors are much more efficient than the previous IG-500 product line,” said Mr. Ninot.

    Keeping lidar and camera data precisely synchronized can be difficult because the camera focal time is susceptible to vary. In mobile scanning, even a slight latency might cause an offset. For example, the picture will not be located on the right place inside the point cloud. Viametris decided to connect the camera and the three lidars to the Ellipse-A to ensure a highly accurate and repeatable synchronization.

    At INTERGEO 2015, the iMS 3D will be presented at stand # B4.049 and the ELLIPSE-A will be presented at stand # G4.079.

     

  • Leica GS14 GNSS Features Hybrid Communication Technology

    Leica GS14 GNSS Features Hybrid Communication Technology

    Leica Viva GS14
    Leica Viva GS14

    Leica Geosystems, manufacturer of the Leica Viva GNSS Unlimited series and GS14 GNSS receiver, has added a new hybrid communication technology to its compact and powerful GNSS smart antenna. The latest generation Leica Viva GS14 GNSS now supports Verizon CDMA solutions along with all standard 2G/3G networks and UHF TX/RX radio in a single device, making it a professional GNSS receiver with all three communication systems built in. Users simply slide in their SIM card to experience instant connectivity for faster and easier field communications and SmartNet RTK corrections, the company said.

    The Leica Viva GS14 3.75G&UHF supports 2G GPRS, 3G HSPa+, CDMA (EV DO) and UHF TX/RX radio between 450 and 470 MHz in one compact housing. Professionals can choose whether they want to use the UHF radio to transmit or receive work, a 2G/3G cellular network, or Verizon CDMA. No external equipment is required.

    “The Leica Viva GS14 with its hybrid communication technology is the most advanced compact GNSS receiver in the market,” said Bernhard Richter, Leica Geosystems GNSS business director. “The addition of CDMA modem capability in a unique all-in-one design offers unmatched flexibility in communication choices.”

    The Leica Viva GS14 3.75G&UHF is available today throughout the United States. Ordering information and details are available from all authorized U.S. Leica Geosystems representatives and dealers.

  • Northrop Grumman Gives Award to Curtiss-Wright for Global Hawk

    Northrop Grumman Gives Award to Curtiss-Wright for Global Hawk

    An RQ-4 Global Hawk soars through the sky to record intelligence, surveillence and reconnaissance data. Air Force and Navy officials met to discuss joint training with the RQ-4. (Courtesy USAF)
    An RQ-4 Global Hawk soars through the sky to record intelligence, surveillence and reconnaissance data. (Courtesy USAF)

    Curtiss-Wright Corporation’s Defense Solutions division was honored by Northrop Grumman for its role as a supplier in support of the RQ-4 Global Hawk unmanned aircraft system (UAS).

    Global Hawk has flown 150,000 total flight hours supporting diverse global missions. Carrying a variety of intelligence, surveillance and reconnaissance sensor payloads, Global Hawk supports anti-terrorism, humanitarian assistance, disaster relief, airborne communications and information-sharing missions.

    A ceremony was held Aug. 19 at Curtiss-Wright’s Integrated Systems facility in Santa Clarita, Calif., for the program to receive the James G. Roche Sustainment Excellence Award for a third year in a row. During the ceremony, an award was presented by Mick Jaggers, Global Hawk UAS vice president and program manager, Northrop Grumman Aerospace Sector, and accepted by Lynn Bamford, senior vice president and general manager, Defense Solutions division. The event was also attended by Rep. Steve Knight, U.S. Congressman for California’s 25th District.

    (From left) Knight, Bamford and Jaggers with the award.
    (From left) Knight, Bamford and Jaggers with the award.

    “We extend our sincerest congratulations to the US Air Force on this award and Northrop Grumman for their stellar job as the prime contractor on the milestone setting RQ-4 Global Hawk UAS,” said Ms. Bamford. “We take great pride in Curtiss-Wright’s role as an industry leader in providing advanced rugged electronics that help lower this important aircraft’s cost through the use of commercial-off-the-shelf technologies.”

    During the ceremony, Jaggers remarked, “An aircraft as sophisticated as the Global Hawk comes together with the help of many partners, and one of the most crucial sustainment partners on the Global Hawk is Curtiss-Wright.”

    The Sustainment Excellence Award is granted by Headquarters U.S. Air Force Logistics, Installations and Mission Support. It is named for Dr. James G. Roche, the 20th Secretary of the Air Force, a position he held from 2001 to 2005.

  • Antenova Shows GNSS Antenna Integration for Telematics at CTIA

    Antenova Shows GNSS Antenna Integration for Telematics at CTIA

    The Antenova ODB fully assembled.
    The Antenova ODB (on-board devices) design fully assembled.

    Antenova Ltd., manufacturer of antennas and RF antenna modules for M2M and the Internet of Things, has built a model design for on-board devices (OBD) and vehicle telematics, which the company will be showing at CTIA Supermobility 2015.

    The OBD design uses three new antennas inside an OBD housing to link to GNSS satellite, Bluetooth and a terrestrial network, while obtaining optimum performance from all three antennas simultaneously. The design also features a new small GNSS RF module to fix location, which Antenova is showing for the first time.

    Antenova is using the latest antennas from it product ranges in the OBD design:

    • the Armata 3G FPC antenna for penta-band frequencies which operates at 824-960 MHz and 1710-2170 MHz
    • a new GNSS antenna named Bentoni operating at 1559-1609 MHZ,
    • the tiny Weii PCB-mounted antenna, which provides a Bluetooth connection at 2.4GHZ.

    All three are new antennas Antenova released this year.

    The new GPS/GNSS module (Antenova part number M10578) is a complete receiver that provides accurate location tracking for OBDs. It uses the latest MediaTek chipset with an additional LNA to give added performance when mounted under dashboards and out of line of sight with the sky.

    Antenova’s product designers recently introduced the concept of “Design For Integration” (DFI), which considers how the RF antenna will operate when it is embedded with a manufacturer’s product. Antenova’s antennas are always used within a customer’s design, so they are designed to provide superior RF performance from within the device, and to make the integration of the RF elements easier for the designer. In addition to this, Antenova provides its customers with technical support during the design, integration and testing phases.

    “We are demonstrating how a design for an OBD can give great performance, even when new antennas are added to an existing design,” explained Colin Newman, Antenova’s managing director. “OBD devices are growing fast in popularity, and the design of the RF components is critical to the overall performance of a device. In particular, Antenova’s engineers have invested many years in designing antennas that work effectively in very small spaces, whilst maintaining the efficiency of the antenna.”

    Antenova offers a range of antennas for Bluetooth, ZigBee, Wi-Fi, ISM, 802.11, 3G, GSM, GPRS, Edge, UMTS, WCDMA, LTE, GLONASS, BeiDou and Gallileo.

  • Calgary Company Switches from GPS Handhelds to TerraGo

    Calgary Company Switches from GPS Handhelds to TerraGo

    The Trans-Alaska Pipeline System in Interior, Alaska
    The Trans-Alaska Pipeline System in Interior, Alaska.

    Enmapp, a pipeline services company based in Calgary, Alberta, Canada, has replaced its proprietary GPS handhelds with TerraGo Edge and Eos Arrow receivers. TerraGo Edge is a mobile GPS data collection platform that integrates with the Eos Arrow series of GNSS receivers to bring advanced sub-meter and centimeter real-time accuracy to any smartphone or tablet.

    Enmapp provides data collection services to energy companies for pipeline construction and maintenance. Before TerraGo Edge, Enmapp relied on all-in-one GPS handheld devices, but became convinced the cost, features and performance were increasingly out of line with the mobile revolution fueled by Apple and Android solutions. After an extensive evaluation, Enmapp selected TerraGo Edge and Eos Arrow 100 receiver for a field trial so they could compare their performance against the GPS handhelds.

    Eos Positioning's Arrow 200 Bluetooth receiver now supports Hemisphere's Atlas correction service,
    Eos Positioning’s Arrow 200 Bluetooth receiver now supports Hemisphere’s Atlas correction service,

    After downloading the app on the crew’s iPads and pairing the Eos Arrow 100 via Bluetooth, they were up and running within minutes. “The results were astounding,” reads a TerraGo press release. “Not only did the Eos GPS receiver meet the GPS handheld’s accuracy requirements, in some cases it was much better. The efficiency of the crews was far superior with the native iPad features of TerraGo Edge, versus the old-style stylus and PDA screens of the legacy equipment. The labor costs were also reduced because they were able to use real-time GPS from the Eos Arrow 100 and reduce post-processing. Enmapp declared TerraGo Edge and Eos the clear winner, and have now deployed TerraGo Edge on all field personnel iPads, along with a Bluetooth-connected, sub-meter GPS receiver, the Eos Arrow 100.”

    “The hardware savings are enormous with the new GPS kit at less than $10,000 compared to the old kit which was over $70,000. But the ongoing reduction of project labor costs is even more valuable over time,” said Lance Fugate, program manager at Enmapp. “The cost reductions and efficiency improvements are a game-changer for us. As our industry continues to look for innovation from its service providers, TerraGo Edge enables us to deliver more efficiently. We can pass these savings directly to our customers with each and every future project.”

    The TerraGo Edge is available for either iOS or Android.

    Below is an exclusive interview with John Timar about TerraGo Edge from the GEOINT 2015 conference.

    Jean-Yves Lauture of Eos Positioning discusses the Arrow 200 GNSS receiver at the Esri User Conference.

  • Galileo 9 and 10 in the Zone for This Week’s Launch

    Galileo 9 and 10 in the Zone for This Week’s Launch

    Galileos 9 and 10 are lowered onto the Fregat upper stage.
    Galileos 9 and 10 are lowered onto the Fregat upper stage.

    Galileo 9 and 10 are ready for launch atop a Soyuz rocket at 23:08 local time on Sept. 10 (02:08 GMT and 04:08 CEST on Sept. 11) from Europe’s Spaceport in French Guiana.

    After being attached to their carrier last week, the pair of fully fueled satellites was carefully lowered onto the Fregat upper stage on Wednesday, Sept. 2, in the 3SB preparation building of the Guiana Space Centre. The following day was devoted to functional checks and inspections, preparing the Galileos plus Fregat to be encapsulated within the halves of their Soyuz rocket fairing, which took place on Sept. 4. This complete “upper composite” was then transported to the launch site and attached vertically to the first three stages of the Soyuz ST-B, the 12th Soyuz to be operated from the spaceport.

    As much a spacecraft as a launcher stage, the re-ignitable Fregat will take the Galileos the bulk of the way to their designated medium-altitude orbit once the first three stages achieve low orbit, 9 minutes and  24 seconds after launch. A pair of Fregat firings will be separated by a 3-hour, 13-minute coast up to their target 23,222 km orbital altitude and 57.394° inclination.

    Soyuz in Launch Zone. The basic three-stage vehicle for Arianespace’s Sept. 10 Flight VS12 rolled out from its MiK integration building in the Spaceport’s northwestern sector this morning, and was transferred horizontally to the ELS launch zone by a transporter/erector rail car.

    The Soyuz rocket is moved to the launch pad and lifted into a vertical position.
    The Soyuz rocket is moved to the launch pad and lifted into a vertical position.

    The Soyuz was then erected in a vertical position and suspended over the launch pad, held in place by four large support arms. This was followed by the 53-meter-tall mobile gantry’s move-in to protect the launcher, providing a safe environment for installation of the “upper composite” containing the Galileo satellites.

    Galileo 9 and 10 are the fifth and sixth Galileo FOC (full operational capability) spacecraft, and have been designated “Alba” and “Oriana” — continuing the naming process after children who won a painting competition organized by the European Commission in 2011. The satellites were built by OHB System, with Surrey Satellite Technology Ltd. supplying their navigation payloads.

    The European Commission is managing and funding Galileo’s FOC phase — during which the network’s complete operational and ground infrastructure is being deployed. The European Space Agency has been delegated as the design and procurement agent on the Commission’s behalf.

    Two More this Year. Two further satellites are scheduled for launch by the end of this year. One is under test at ESA’s ESTEC technical centre in Noordwijk, the Netherlands, while the other has already completed its checks and is awaiting transportation to Kourou in the second half of October. In addition, the first satellite of the following batch (Galileo 13) has arrived at ESTEC and is undergoing its thermal-vacuum test. The next will arrive by mid-September.

    Follow Arianespace’s launch activity on its website.

    ESOC serves as the Operations Control Centre for ESA missions and hosts ESA's Main Control Room (shown here), combined Dedicated Control Rooms for specific missions and the ESTRACK Control Centre, which manages ESA's worldwide ground tracking stations.
    ESOC serves as the Operations Control Centre for ESA missions and hosts ESA’s
    Main Control Room (shown here), combined Dedicated Control Rooms for specific
    missions and the ESTRACK Control Centre, which manages ESA’s worldwide ground
    tracking stations.

    Mission Control’s Mission. When the next pair of Galileo satellites is boosted into orbit on Friday, a team of mission control experts in Darmstadt, Germany, will spring into action, working around the clock to bring the duo through their critical first days in space. The fiery ascent to space will last just over nine minutes, after which the Fregat upper stage will fire twice to place the satellites into their release orbit.

    Separation from Fregat, about 3 hours and 48 minutes into flight, marks the start of the critical early orbits for the team at ESA’s European Space Operation Centre in Darmstadt. Within the combined flight control team from ESA and France’s CNES space agency, each position is paired with its counterpart from the other agency and mixed “CNESOC” shifts will rotate to conduct operations around the clock. The same team conducts all the Galileo early operations alternately from ESOC and from the CNES control centre in Toulouse, France.

    “Upon separation, the team will be very focused, and we’ll be watching for a number of critical events on the satellites to happen automatically at the right time and in the right order,” said ESA’s Liviu Stefanov, lead flight director for this phase. “The satellite must switch on, go into a basic flight configuration, deploy its solar wings for power, orient them towards the Sun and acquire Sun-pointing attitude. “As soon as we get communications, we’ll check its health and start sending commands to configure the satellite after completion of the automatic sequence and prepare it for the next major activity: pointing Galileo towards Earth.”

    The intense activity will begin the 10-day early operations phase, during which the joint team will work 24 hours/day to oversee steps to prepare the satellites for handover to the Galileo Control Centre in Oberpfaffenhofen, for routine operations, and ESA’s Redu Centre in Belgium, for detailed payload testing.

    The logos of the two new satellites in the Galileo constellation are placed on the launcher fairing.
    The logos of the two new satellites in the Galileo constellation are placed on the launcher fairing.

    Photo Gallery

  • McMurdo Introduces Next-Gen Software for Satellite-Aided Search and Rescue

    McMurdo Introduces Next-Gen Software for Satellite-Aided Search and Rescue

    In a typical Cospas-Sarsat search and rescue process, a Distress Beacon signal is sent via Satellite to a Local User Terminal. A Mission Control Center validates the emergency and sends critical information to Rescue Coordination Centers. MEOSAR, the next-generation version of Cospas-Sarsat, will provide several unique features including a Return Link Service function to acknowledge receipt of the distress signal.
    In a typical Cospas-Sarsat search and rescue process, a distress beacon signal is sent via satellite to a local user terminal. A mission control center validates the emergency and sends critical information to rescue coordination centers. MEOSAR, the next-generation version of Cospas-Sarsat, will provide several unique features including a return link service function to acknowledge receipt of the distress signal.

    McMurdo has introduced PRISMA MCCNet, a new software solution with several new features to improve the Cospas-Sarsat satellite-aided search and rescue process, and for use in the future MEOSAR system. The software, which is part of McMurdo’s suite of PRISMA (Preparation, Response, Identification, Surveillance, Management, Acceleration) software solutions, provides mission control center (MCC) operators with critical tools to better identify, locate and manage distress situations.

    In a typical Cospas-Sarsat search and rescue scenario, a distress signal from an emergency beacon is sent via satellite to a fixed ground receiving station or local user terminal. The nearby MCC confirms the emergency, analyzes location data and provides this information to the various rescue coordination centers for the actual rescue operation. PRISMA MCC’s improved functionality includes built-in system redundancy, unified communications and automated reporting to improve the MCC operation and streamline the search and rescue process.

    The international Cospas-Sarsat satellite system is best known for detecting and locating emergency beacons activated by aircraft, ships and backcountry hikers in distress and has been credited with saving 37,000 lives since 1982. The system includes satellites in low-altitude Earth orbit (LEO) and geostationary Earth orbit (GEO). The future Cospas-Sarsat system will include medium-altitude Earth orbit (MEO), which will form the MEOSAR system. Satellites in the MEOSAR system include GPS, Galileo and GLONASS satellites, which are incorporating search and rescue payloads.

    “PRISMA MCCNet provides Mission Control Center operators with a powerful, comprehensive and reliable software tool that provides the most accurate data and most up-to-date information to expedite the search and rescue process,” said Jacob Blankenship, search and rescue business manager for McMurdo. “With several advanced features and innovative functions based on our years of experience working with the leading search and rescue authorities around the world, the end result will be faster decision making and, ultimately, more lives saved.”

    McMurdo’s PRISMA MCCNet software will help improve a Cospas-Sarsat satellite-aided search and rescue system that has helped to save 37,000 lives since 1982.
    McMurdo’s PRISMA MCCNet software will help improve a Cospas-Sarsat satellite-aided search and rescue system that has helped to save 37,000 lives since 1982.

    PRISMA MCCNet provides significant improvements in several key areas to enhance mission control center operations including:

    • High Availability with Support for Automatic Failover — PRISMA MCCNet includes new automatic failover and built-in redundancy features to maximize availability and uptime of the search and rescue system.
    • Unified Inbox and Communications — Easy to use and organize, PRISMA MCCNet’s Unified Inbox displays all actionable events that require operator interactions including beacon alerts, narrative messages, or system level alarms on a single screen. This information, which traditionally required the use of multiple screens, can be sent easily and reliably to rescue authorities via multiple communications protocols and redundant link transmission.
    • Advanced Monitoring and Reporting — PRISMA MCCNet’s built-in automatic diagnostic and analytical tools continuously detect, trace, and report malfunctioning components and processes. Quality Management System (QMS) analysis tools provide real-time tracking of system performance.
    • Client-Server Architecture — Unlike traditional MCC systems, PRISMA MCCNet is based on a secure and scalable client-server architecture allowing multiple MCC workstations to access consistent data and information from a centralized or distributed server configuration.
    • Commissionable LEOSAR/GEOSAR/MEOSAR MCC — PRISMA MCCNet was developed in close association with Cospas-Sarsat, National Oceanic and Atmospheric Administration (NOAA), NASA and other search and rescue authorities. This ensures a seamless commission/certification process for LEOSAR/GEOSAR/MEOSAR MCCs.
    McMurdo’s PRISMA MCCNet software streamlines Mission Control Center operations with industry-first features including built-in system redundancy, a Unified Inbox and advanced monitoring tools.
    McMurdo’s PRISMA MCCNet software streamlines mission control center operations with features including built-in system redundancy, a unified inbox and advanced monitoring tools.

    “The launch of PRISMA MCCNet is yet another milestone in McMurdo’s journey to become the global leader in emergency readiness and response,” said Jean-Yves Courtois, McMurdo CEO. “It provides a solid foundation upon which we can build a world-class, integrated ecosystem of products, technologies and services for preventing emergencies, protecting assets and saving lives.”

    McMurdo provides the world’s only complete, end-to-end emergency readiness and response solution including distress beacons, search and rescue satellite infrastructure, mission control and rescue coordination centers and maritime domain awareness solutions including coastal surveillance and vessel monitoring systems. The world’s leading search and rescue authorities in the U.S. (NOAA and NASA), Australia (Australia Maritime Safety Authority), New Zealand (Maritime New Zealand), Cyprus, South Africa, Argentina and other countries use McMurdo search and rescue systems.

    Images: McMurdo

  • YellowScan Lidar for UAVs Aided by Inertial Nav, GPS RTK

    YellowScan Lidar for UAVs Aided by Inertial Nav, GPS RTK

    A UAV carries the YellowScan lidar.
    A UAV carries the YellowScan lidar.

    SBG Systems joins YellowScan to present a lightweight lidar with inertial and GPS for UAVs. The new product will be presented at the INTERGEO trade show in Stuttgart, held Sept. 15-17.

    The YellowScan lidar is designed for fixed or rotary-wing UAVs, with an embedded Ellipse-E, a miniature inertial navigation system from SBG Systems, which helps obtaining a clear and accurate point cloud.

    The UAV market is continuously growing, especially for professional applications like 3D surveying. Developed for such applications, YellowScan’s R&D team has worked closely with researchers and professionals in industries such as construction, surveying, mining and natural resources to create a comprehensive, high-performance and easy-to-use LiDAR.

    Ellipse-E. The ready-to-use YellowScan is operational at up to 75 meters and delivers a highly dense point cloud accurate to 10/15 centimeter. The solution includes a lidar with a ±50 degree angle that measures 40,000 points per second, an Ellipse-E inertial navigation system coupled with a centimeter-level RTK GPS, an on-board computer, and an integrated battery.

    The Ellipse-E miniature inertial navigation system by SBG Systems.
    The Ellipse-E miniature inertial navigation system by SBG Systems.

    Once mounted on the drone, the user pushes the yellow button and YellowScan is ready to survey. LED lights give useful information on YellowScan state, for instance if the GPS is receiving RTK corrections or not. The user can launch the UAV and begin the survey. Once the task accomplished, a USB stick is used for downloading the data. An office software visualizes the point cloud in a few clicks, before opening it in an industry specific software like Terrasolid, AutoCAD or ESRI.

    The YellowScan research and development team was searching for a high-performance, light and ITAR-free inertial navigation system for motion compensation and data georeferencing. They tested the Ellipse-E, the new miniature inertial navigation systems from SBG. Weighting 12 grams as an OEM version, it provides roll-and-pitch data accurate to 0.2 degree. The heading is accurate to 0.5° with only one antenna. Indeed, the heading computation relies on GPS and accelerometers data. This method is used when GPS positioning is widely available and punctuated by frequent accelerations, such as turns. The R&D team found the test results satisfying, and a point cloud highly clean. “We are very satisfied with this little Ellipse-E. It perfectly matches our technical needs, and we even gained 5 percent on the total weight of the YellowScan,” said Tristan Allouis, CTO at YellowScan.

    Ellipse-E Coupled with External GPS Receiver. The Ellipse-E inertial navigation system is able to connect to any survey-grade GPS receiver and to fuse in real-time GPS position with inertial information. Ellipse-E maintains a reliable position even if GPS masks occur. In this application, the Ellipse-E is coupled with the AsterX-m OEM card from Septentrio, a receiver that uses GPS and GLONASS constellations and works with all types of RTK reference stations.

    At INTERGEO, YellowScan will be in booth # F8.014, and SBG Systems will present the Ellipse-E at booth # G4.079.

    A point cloud made with YellowScan.
    A point cloud made with YellowScan.
  • Innovation: Getting There by Tuning In

    Innovation: Getting There by Tuning In

    Using HD Radio Signals for Navigation

    By Ananta Vidyarthi, H. Howard Fan and Stewart DeVilbiss

    INNOVATION INSIGHTS by Richard Langley
    INNOVATION INSIGHTS by Richard Langley

    THE YEAR WAS 1906. On Christmas Eve of that year, Canadian inventor Reginald Fessenden carried out the first amplitude modulation (AM) radio broadcast of voice and music. He used a high-speed alternator capable of rotating at up to 20,000 revolutions per minute (rpm). Connected to an antenna circuit, it generated a continuous wave with a radio frequency equal to the product of the rotation speed and the number of magnetic rotor poles it had. With 360 poles, radio waves of up to about 100 kHz could be generated. However, Fessenden typically used a speed of 10,000 rpm to produce 60 kHz signals. By inserting a water-cooled microphone in the high-power antenna circuit, he amplitude-modulated the transmitted signal. On that Christmas Eve, he played phonograph records, spoke and played the violin with radio operators being amazed at what they heard.

    Fessenden had earlier worked with spark-gap transmitters, as these were standard at the time for the transmission of Morse code, or telegraphy, the wireless communication method already in use. But they couldn’t generate a continuous wave and couldn’t produce satisfactory AM signals. But as telegraphy was the chief means of communication, they remained in use for many years along with high-powered alternators and the Poulsen arc transmitter, which could also generate continuous waves.

    Although other experimental AM broadcasts were carried out using alternators or arc transmitters, voice transmissions — and in particular sound broadcasting — didn’t take off until the invention of amplifying vacuum tubes. Just before World War I, it was found that they could be used in an oscillator circuit to produce continuous waves, which could be easily modulated to make an AM transmitter. Such transmitters could be used for point-to-point communications but also for broadcasting, and a number of experimental broadcasting stations were established in Europe and North America during and just after the war. Tubes were also instrumental for improvements in receiver technology. “Where there was one licensed station in America in 1920, there were nearly 600 stations just five years later, and the number of radio receivers went from thousands of crystal sets to millions of vacuum-tube circuits.” — from The Science of Radio by Paul J. Nahin, one of my favorite writers on electronics and mathematics.

    AM radio broadcasting used frequencies in the long-wave, medium-wave and short-wave frequency bands, and still does. But AM signals often have low audio quality due to bandwidth limitations imposed by regulators and interference from other stations, atmospheric disturbances and electrical noise. So, over the past decade or so, many broadcasters have abandoned long-wave and medium-wave frequencies and moved to the frequency modulation or FM broadcast band with its superior signal capability.

    However, this migration pattern might be slowed or stopped if digital broadcasting were to be fully embraced on the AM broadcast bands. A digital technique developed by the iBiquity Digital Corporation is gradually being adopted by broadcasters in the United States and elsewhere. The technique provides FM-quality sound in the medium-wave band by supplementing existing AM signals or replacing them altogether. It can also supply data about the transmitting station and its broadcast. Some 240 AM radio stations in the U.S. already use the technology. (It can also be used in the FM band to provide CD-like quality.)

    But these digital signals in the AM broadcast band might serve an additional purpose beyond improving the listening experience. In this month’s column, our authors tell us about some extensive simulation work they have carried out to demonstrate the feasibility of using digital radio signals for navigation. In the future, you may be able to turn on your radio and tune in to get to where you’re going.


    “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.


    It is well known that the GPS signals are weak and are therefore subject to interference and blockage due to obstruction. Signals of opportunity (SOO), on the other hand, which are designed for other purposes such as communication, may also be used for navigation and have relatively greater signal power than GPS. They are plentiful and relatively more resistant to blockage and jamming compared to GPS. Many authors have presented methods and algorithms utilizing SOO such as AM and FM broadcast signals, TV broadcast signals and 3G/4G wireless communication signals (see Further Reading for examples). These signals are robust and have very good received power levels compared with GPS, and are capable of penetrating through buildings. In addition, these signals are readily available and there is no need for any additional installation of transmitting devices or infrastructure.

    In this article, we present the results of a study using AM HD Radio, digital radio in the 540–1700 kHz band of the frequency spectrum, with known transmitter locations, to locate and track receiver locations that are otherwise unknown. HD Radio, originally meaning hybrid-digital radio, is a trademarked term for iBiquity Digital Corporation’s digital radio technology. Unlike analog AM radio signals, digital radio signals are well structured and more immune to co-channel interference, and hence could be better adapted for navigation. In addition, with the proliferation of software-defined radios (SDRs), digital AM radio may eventually replace analog AM radio.

    The challenges of navigation using digital radio signals include narrow signal bandwidths, long symbol durations and lack of synchronization among transmitters. Therefore, digital radio signals are not an ideal choice for accurate position estimation, similar to many other SOO that aren’t designed for navigation. Nevertheless, in this work, we have designed algorithms to overcome such difficulties to obtain a good level of location accuracy, making it a feasible alternative for SOO navigation.

    Signal Format of Digital AM Radio

    Digital AM signals have a well-defined structure called in-band-on-channel (IBOC) that can be exploited for localization purpose. It employs sophisticated digital radio waveforms, which can deliver compact-disc-like sound quality, free of interference and noise, to radio listeners. It uses the existing AM and FM analog broadcasting bands and channel schemes to transmit digital signals. The IBOC digital radio transmitter system encodes analog audio into binary form for transmission.

    The design provided by IBOC AM radio has two service modes with two new waveform types: hybrid (denoted by MA1) and all-digital (denoted by MA3). The hybrid waveform retains the analog AM signal, while the all-digital waveform completely replaces the analog AM signal. In the hybrid service mode, the bandwidth of the analog audio signal waveform can be 5 kHz or 8 kHz. The digital signal is transmitted on both sides of the analog host signal in the primary and secondary sidebands. It is also transmitted on the tertiary sidebands, which are 20 dB beneath the analog signal as shown in FIGURE 1.

    FIGURE 1. Logical channels and sidebands on the frequency spectrum; hybrid mode with 5-kHz analog signal bandwidth. (After iBiquity.)
    FIGURE 1. Logical channels and sidebands on the frequency spectrum; hybrid mode with 5-kHz analog signal bandwidth. (After iBiquity.)

    For the 8-kHz configuration, the secondary sidebands are also beneath the analog host signal. The greatest system enhancements are realized with the all-digital system, as shown in FIGURE 2. In this system, the analog signal is replaced with the all-digital primary sidebands whose power is increased relative to the hybrid system levels. Secondary and tertiary sideband powers are also increased to the level of the hybrid waveform. Reference subcarriers are also provided to convey system control information. The end result is a higher power digital signal with an overall bandwidth reduction.

    FIGURE 2. Logical channels and sidebands on the frequency spectrum; all-digital mode. (After iBiquity.)
    FIGURE 2. Logical channels and sidebands on the frequency spectrum; all-digital mode. (After iBiquity.)

    Digital radio offers distinct advantages over analog, including mitigation of transmission artifacts and improved audio quality. These changes provide a more robust digital signal that is less susceptible to adjacent channel interference, thereby reducing the noise in the system. An overview of the AM digital system for both the service modes, MA1 and MA3, is given in the following paragraphs. However, in the simulation study we carried out, we used the all-digital AM (MA3) mode. The all-digital AM system has a smaller bandwidth than the hybrid signal. If reasonable localization results can be obtained with it, then we can predict that better localization results may be obtained with the hybrid signal.

    IBOC uses an orthogonal frequency-division multiplexing (OFDM) waveform for signal modulation. Each OFDM subcarrier channel has a spacing of 181.7 Hz. The hybrid MA1 service mode comprises 163 subchannels indexed from -81 to 81 over a total bandwidth of 29.4 kHz as shown in Figure 1. The all-digital MA3 service mode has only 105 subchannels indexed from -52 to 52 over a total bandwidth of 18.9 kHz as shown in Figure 2. Therefore, when compared to the all-digital mode, hybrid mode contains more training symbols per OFDM symbol duration. The training symbols are important since these symbols are known and will be used to perform correlation to estimate the signal time of arrival. We predict that since the hybrid mode contains more training symbols than the all-digital mode, detection accuracy will be higher for the hybrid mode. Hence, choosing the all-digital MA3 service mode for the localization will be more challenging, and this is another reason for our decision to use MA3. Demonstrating the capability of the all-digital MA3 service mode for localization would imply that the hybrid mode could be used for the same, with at least the same or better performance.

    Interleaving in time and frequency is used to mitigate the effects of burst errors. The interleaver output is according to a structured matrix (not shown here). Each interleaver matrix consists of information associated with a specific portion of the transmitted spectrum, and consists of eight interleaver blocks, with each block of size of 32 × 25. Hence, each block has 800 symbols to be filled, out of which 50 are known training symbols. Since this work entirely relies on training symbols, understanding interleaving is important so we know exactly where the training symbols are in a signal data stream. From the interleaving matrix, the positions of all training symbols are given, which have a periodic appearance of every 16 rows.

    The OFDM subcarrier mapping transforms interleaver output into scaled 16 quadrature amplitude modulation (QAM) and 64 QAM and binary phase-shift keying (BPSK) symbols and then maps them to specific OFDM subcarriers. The inputs to OFDM subcarrier mapping are according to the interleaver matrices, which map respective symbols to the primary, secondary, tertiary, Primary IBOC Data Service (PIDS) and reference subcarriers. One row of each active interleaver matrix and one bit of the system control vector are mapped into each OFDM symbol (every Ts seconds) to produce one output vector X, where Ts = 5.805 × 10-3 seconds.

    OFDM signal generation takes the complex frequency domain OFDM symbol X as generated above and outputs a time-domain representation of the digital signal. Let Xn be the vector X for the nth OFDM symbol, and Xn[k] be the kth element of Xn, which is the complex scaled constellation points for the subcarrier mapping for the nth symbol, where k = 0, 1,…, L-1 is the subcarrier index in the frequency-domain input to the signal generation for transmission. The input vector X is transformed into a shaped time-domain baseband pulse yn(t) defining the nth OFDM symbol as

    Inn-E1

    where n = 0, 1, …, ∞, Inn-E2.  Note that n indexes consecutive OFDM symbols, L = 105 is the maximum number of OFDM subcarriers, Ts and ∆f are the OFDM symbol period and OFDM subcarrier spacing, respectively, and W(t) is the time-domain pulse shaping function.

    Time of Arrival Acquisition

    Since the training symbols are known, a local copy can be generated at a receiver to correlate with the received digital AM signal to measure signal time of arrival (TOA). Measuring TOA accurately from a correlation peak is crucial, since any error in TOA measurement directly affects localization accuracy. The relatively narrow bandwidths and hence long symbol durations of the digital AM radio signals pose a challenge as they give rise to potentially large timing errors, thereby greater localization errors. To improve the location accuracy, strong digital AM signal levels are used to our advantage so methods such as curve fitting and time averaging can be performed. Moreover, unlike the structures of the civil GPS signals, which are all known, only the training symbols and their positions in the digital AM signals are known. Other data in the digital AM signals are random and cannot be used for correlation. Therefore, using long correlation vectors will help in detecting peaks as there will be more training symbols.

    Sampling. Correlation is performed, of course, after sampling. So we first discuss how to choose an appropriate sampling frequency. After correlation, if we detect the peak and record it as TOA only at the corresponding sampling instant, a maximum distance error of c/2fs can occur between two adjacent samples, where c is the speed of light and fs is the sampling frequency. At the Nyquist sampling frequency, say 40 kHz, this error could be as large as 3,750 meters. Sampling at a frequency much higher than the Nyquist can help to improve accuracy, but this improvement diminishes as the sampling frequency increases beyond a certain value, because the narrow signal bandwidth makes the peak of its correlation function rounded, so detection of the actual peak becomes less accurate. In our simulations, we found that this point of diminishing returns is at about fs = 10 MHz, at which the error between two adjacent samples is 15 meters, much better than that at the Nyquist sampling rate. This high sampling rate is easily doable with today’s digital technologies. However, this 15-meter error is the ranging error between one transmitter and one receiver. Five or more transmitters have to be considered for the location algorithm presented in a later section. Then, the ranging error of 15 meters may magnify to the order of a few kilometers as location errors. Clearly, there is a need to detect TOA of a correlation peak between two adjacent samples; that is, we need interpolation to achieve a smaller TOA error.

    Interpolation. To calculate the TOA between two adjacent samples, we interpolate by curve fitting the correlation data and estimate the TOA by solving polynomial functions. It was observed that the correlation peak is asymmetric, so the correlation curve is shaped differently to the left and right of the peak value. This is illustrated in FIGURE 3. Therefore, we need to fit two different curves on each side of the correlation peak. By a trial-and-error process, we determined that a quadratic polynomial is sufficient to fit the correlation values close to the peak. Therefore two simple quadratic functions are fitted for the correlation data points to the left and right of the peak.

    FIGURE 3. Asymmetric correlation peak denoting different slopes on either side.
    FIGURE 3. Asymmetric correlation peak denoting different slopes on either side.

    FIGURE 4 shows curve fitting for the correlation of a received signal and a local signal sampled at 10 MHz. The maximum time error due to sampling is Tsamp/2, which equals 5 ×10-8 seconds. This translates into a distance error of 15 meters and localization error of a few kilometers as mentioned before. From Figure 4, it is seen that the intersection point, which is taken as the measured TOA, is much closer to the actual TOA resulting in a much smaller distance error.

    FIGURE 4. Enlarged views of Figure 3 near the peak.
    FIGURE 4. Enlarged views of Figure 3 near the peak.

    Based on the HD Radio documentation, a normal signal-to-noise ratio (SNR) is calculated to be 52 dB. However, in case of adverse channel conditions, lower SNR levels of 30 dB and 10 dB have also been considered. Our simulations show that, with additive white Gaussian noise, the TOA estimation errors are affected by SNR very little above 10 dB, and are improved by an order of magnitude compared with no curve fitting. To make sure the TOA estimation error for the 10 dB SNR case can be used for the purpose of localization, we carried out a Monte Carlo simulation. Twenty-one different random signals were simulated, and the TOA measurement errors after curve fitting were recorded at different delays. The ensemble average of these TOA estimation errors was within 2 ×10-9 seconds. These results confirm that a 10 dB SNR signal can be very well used for localization. Thus, we used an SNR of 10 dB for all the simulations discussed later in this article.

    Differential Time-Difference of Arrival

    Once all the TOAs from different transmitters are obtained, they are sent to a processing station, which could be one of the receivers. Due to lack of synchronization in digital AM radio transmitters as well as unknown clock offsets in digital AM radio receivers, the obtained TOAs are not aligned, so they cannot be directly used for location determination. A technique called differential time-difference of arrival (dTDOA), which is similar to GPS double differencing and was published by the authors elsewhere (see Further Reading), is employed here to overcome this problem.

    Consider the case where there are two transmitters, A and B, and two receivers, C and D, as shown in FIGURE 5.

    FIGURE 5. Principle of differential time-difference of arrival (dTDOA).
    FIGURE 5. Principle of differential time-difference of arrival (dTDOA).

    When transmitter A is transmitting, its signal is received at different time instances by receivers C and D due to different propagation delays. The internal clock of each receiver records the correlation peak with respect to its local time at the corresponding receivers. TOAs of the signal from transmitter A at both receivers C and D are recorded as Inn-TAC and Inn-TAD, which also contain the unknown transmitter A clock time offset. Differencing these two TOAs Inn-TAC-TAD , the unknown transmitter A clock time offset is cancelled. But this TDOA is unsynchronized, so it cannot be used for location determination. Then we find the similar unsynchronized TDOA from transmitter B, Inn-TBC-TBD. To eliminate the unknown receiver clock offsets we difference the two TDOAs, resulting in a dTDOA:

    Inn-E3

    Thus, by using a minimum of two transmitters and two receivers, a dTDOA cancels receiver clock offsets and transmitter clock offsets, thus avoiding the need of precise clock synchronization. The number of independent dTDOA equations required to solve for the locations of n receivers is given by (m-1)(n-1) where m is the number of transmitters, and n is the number of receivers. For two receivers, there are four unknowns in a two-dimensional positioning plane, so we need a minimum of five transmitters to obtain four independent equations to solve for four unknown location parameters. If one of the receivers is permanently stationary with a known location such as in differential GPS, then we only need three transmitters to solve for two unknown horizontal location parameters, or four transmitters for three unknown location parameters in 3-D .

    The above dTDOA equations, when expressed in terms of receiver locations, are non-linear. The non-linear over-determined or exact system of equations can be solved using iterative procedures, such as non-linear least squares or the Levenberg-Marquardt (LM) technique. In the simulations we ran, we found that the LM method was more robust than the Gauss-Newton method because it was capable of converging to the solution in the global minimum even if the initial guess was relatively far away. But a reasonable initial estimate of the solution can help with faster convergence. If the initial estimate is too far away, the solution often converges to a local minimum instead of the global minimum.

    Therefore, a good initial estimate of the solution is crucial. An approximate initial estimate can be calculated in several ways. For example we can solve linearized equations based on the non-linear dTDOA equations. Or we can use a simple table lookup if we have some a priori knowledge of roughly where the receivers are located.

    Once the initial locations are found, the next step is to track the locations of the receivers when they are moving. A Kalman filter should be used for tracking. A Kalman filter can also incorporate the non-linear dTDOA equations with TOA measurement as input for close coupling between localization and tracking. Or, for simplicity, short of using a Kalman filter, the previous locations can be fed into the LM method to find the next locations. The LM method for this kind of tracking has faster convergence than for repeated initialization, so the next locations can be calculated quickly.

    Time Averaging. Due to error in tracking, the computed locations are not exact but are usually around the actual location. Time averaging is then used to further improve tracking performance. Time averaging can also be used to smooth the TOA measurements or the locations computed from dTDOA equations as input to a Kalman filter.

    Repeated use of the LM method, as shown in FIGURE 6, for estimating a stationary receiver’s coordinates always forms an error ellipsoid because of the noise and computation error. The estimated points are depicted by black points in Figure 6. The small yellow circle in the middle corresponds to the actual location. By simulation, it was found that averaging all the possible estimated locations produced a location much closer to the actual location, as depicted by the red cross in Figure 6. Obviously the more points to average — that is, the larger the time-averaging window — the more accurate the averaged location will be. In general, such time averaging can improve location and tracking performance by an order of magnitude.

    FIGURE 6. Image depicting time averaging of a stationary receiver’s location.
    FIGURE 6. Image depicting time averaging of a stationary receiver’s location.

    For a moving receiver, there is a trade off in choosing the time-averaging window. The larger the time-averaging window, the better the averaged location accuracy, but the larger the resulting time delay in the averaged location. This time delay is also affected by how frequently we update the tracked locations. Receiver velocity and the Doppler effect also affect the choice of the time-averaging window.

    Simulation Results

    We performed a comprehensive computer simulation study. The primary aim of this simulation study was to prove that the accuracy of digital AM signals for navigation can be improved using the methods introduced in the previous sections, despite the narrow bandwidth of the signals, thereby making digital AM a viable choice for navigation. A number of factors will affect the performance of navigation using digital AM signals including the sampling frequency, SNR, time-averaging window and location update frequency. In this simulation study, these factors have been taken into consideration.

    To simulate a realistic environment, we chose the city of Chicago, where there are many digital AM transmitters providing good coverage to the city. We chose the six best transmitters in Chicago based on the power of the signal and location. The working range of the receivers is large enough to perform a detailed study of all the navigation techniques. The locations of the radio station transmitters are shown in FIGURE 7. All figure axes are in kilometers. Colored dots are transmitter locations; colored circles are their ranges. Green tracks are the chosen routes for a fast-moving receiver. Short brown tracks are those of the other receiver, somewhere in the same zone and traveling slowly.

    FIGURE 7. Transmitter locations and two different routes considered for simulation with two receivers. (Map courtesy of Google.)
    FIGURE 7. Transmitter locations and two different routes considered for simulation with two receivers. (Map courtesy of Google.)

    We simulated two receivers moving along the chosen green and brown routes, but we will only show the navigation results of the faster moving receiver along the green routes. A minimum of five transmitters is needed. The entire simulation was done in Matlab. The time-domain digital AM received signals were modeled according to the specifications described previously. Delays corresponding to transmitter and receiver locations were calculated and simulated into the signals received at the two receivers. An SNR of 10 dB was used for all received signals. Along Route 1 (upper left corner of Figure 7), five transmitter signals can be received, whereas along Route 2 (center right in Figure 7), six transmitter signals are received. Simulation conditions and results for these two routes are given in TABLES 1 and 2.

    TABLE 1. Simulation parameters and results of Route 1 (five-transmitter zone).
    TABLE 1. Simulation parameters and results of Route 1 (five-transmitter zone).
    TABLE 2. Simulation parameters and results of Route 2 (six-transmitter zone).
    TABLE 2. Simulation parameters and results of Route 2 (six-transmitter zone).

    In addition, the tracking results for the fast-moving receiver are laid on top of photo maps of the routes, and are shown in FIGURES 8 and 9. The worst-case situation happens when, for example, transition of zones or handover of transmitters happen, for which no specific additional measures were taken in the simulations as shown in Figure 8.

    FIGURE 8. Worst-case result for five-transmitter tracking. (Photo map courtesy of Google.)
    FIGURE 8. Worst-case result for five-transmitter tracking. (Photo map courtesy of Google.)

    However, the typical tracking result in Figure 9 happens most of the time. Clearly, the more transmitters that can be used, the better the accuracy results. Use of more than two receivers or use of a stationary receiver with a known location can reduce this demand on the number of transmitters.

    FIGURE 9. Typical six-transmitter tracking result. (Photo map courtesy of Google.)
    FIGURE 9. Typical six-transmitter tracking result. (Photo map courtesy of Google.)

    The fast sampling frequency, the curve fitting and the time-averaging window are the most important factors affecting the accuracy of this work, and are easily adjustable. In our simulations we used a time-averaging window of 1 second. We expect that the accuracy would further improve as the time-averaging window is increased, but this would result in increased latency. The velocity of the receiver is one limiting factor in choosing the time-averaging window. For a receiver traveling at a maximum speed of 145 kilometers per hour, a time-averaging window of 1 second corresponds to 20.14 meters of tracking lag. Any greater tracking lag may become intolerable. In general, our simulations show that curve fitting alone and time averaging alone each improved localization accuracy by an order of magnitude. When curve fitting and time averaging were combined, the localization accuracy was improved by two orders of magnitude. If a Kalman filter were used for tracking, we would expect further accuracy improvement.

    Other challenges that deserve further study to make this concept a mature technology include multipath propagation and its mitigation, incorporation of estimating digital AM carrier phase, and incorporation of a Kalman filter for tracking. Further increased location accuracy is expected by incorporation of these techniques.

    Acknowledgment

    This article is based, in part, on the paper “A Navigation Solution Using HD Radio Signals” presented at the 2015 International Technical Meeting of The Institute of Navigation, Dana Point, Calif., Jan. 26–28, 2015.


    ANANTA VIDYARTHI graduated from Anna University, India, in 2009 with a B. Tech. degree in electronics and communication engineering. She came to the University of Cincinnati in the fall of 2009 and earned her M.S. degree in 2012 in electrical engineering. Currently, she is working with Cummins Inc. in Columbus, Ind.

    H. HOWARD FAN graduated from the University of Illinois in Urbana-Champaign with a Ph.D. in electrical engineering in 1985. He has been on the faculty of the University of Cincinnati since then, where he is a professor of electrical engineering and computing systems. His research interests are in digital signal processing, system identification, signal processing for communications, interference mitigation, direction finding, and navigation and location.

    STEWART DEVILBISS graduated from Ohio State University with a Ph.D. in electrical engineering in 1994. Since 2007 he has served as the technical advisor for the Navigation and Communication Branch at the Sensors Directorate of the Air Force Research Laboratory, headquartered at Wright-Patterson Air Force Base, Ohio. His primary research interest is in technologies to improve navigation robustness and accuracy.

    FURTHER READING

    • Authors’ Conference Paper

    “Navigation Solution Using HD Radio Signals” by A. Vidyarthi and H.H. Fan in Proceedings of ION ITM 2015, the 2015 International Technical Meeting of The Institute of Navigation, Dana Point, Calif., Jan. 26–28, 2015, pp. 285–292.

    • HD Radio

    The IBOC Handbook: Understanding HD Radio Technology by D.P. Maxson. Published by Focal Press, Burlington, Mass., 2013.

    HD Radio Air Interface Design Description – Layer 1 AM, Doc. No. SY_IDD_1012s, Revision E. Published by iBiquity Digital Corporation, Columbia, Md., March 22, 2005.

    HD Radio AM Transmission System Specifications, Doc. No SY_SSS_1082s, Revision F. Published by iBiquity Digital Corporation, Columbia, Md., Aug. 24, 2011.

    • Differential Time-Difference of Arrival

    “Asynchronous Differential TDOA for Non-GPS Navigation Using Signals of Opportunity” by C. Yan and H.H. Fan in Proceedings of ICASSP 2008, the IEEE 2008 International Conference on Acoustics, Speech and Signal Processing, Las Vegas, Nev., March 31–April 4, 2008, pp. 5312–5315, doi: 10.1109/ICASSP.2008.4518859.

    • Positioning Using Analog AM Signals of Opportunity

    Opportunistic Navigation: Finding Your Way with AM Signals of Opportunity” by J. McEllroy, J.F. Raquet and M.A. Temple in GPS World, Vol. 18, No. 7, July 2007, pp. 44–49.

    “Phase Measurements Using Direct Conversion AM Radio Navigation” by A. Dinh, R. Mason, R. Palmer and K. Runtz in Proceedings of WESCANEX 97, the IEEE 1997 Conference on Communications, Power and Computing, 22–23 May 1997, pp. 280–285, doi: 10.1109/WESCAN.1997.627154.

    • Positioning Using TV Signals of Opportunity

    “Cooperative position location with signals of opportunity” by C. Yang, T. Nguyen, D. Venable, M. White and R. Siegel in Proceedings of NAECON 2009, the IEEE 2009 National Aerospace and Electronics Conference, Dayton, Ohio, July 21–23, 2009, pp. 18–25, doi: 10.1109/NAECON.2009.5426658.

    Prime Time Positioning: Using Broadcast TV Signals to Fill GPS Acquisition Gaps” by M. Martone and J. Metzler in GPS World, Vol. 16, No. 9, Sept. 2005, pp. 52–60.

    “A New Positioning System Using Television Synchronization Signals” by M. Rabinowitz and J. J. Spilker, Jr. in IEEE Transactions on Broadcasting, Vol. 51, No. 1, March 2005, pp. 51–61, doi: 10.1109/TBC.2004.837876.

    • Positioning Using 3G Cellar Signals of Opportunity

    “A Signals of Opportunity Based Cooperative Navigation Network” by M.A. Enright and C.N. Kurby in Proceedings of NAECON 2009, the IEEE 2009 National Aerospace and Electronics Conference, Dayton, Ohio, July 21–23, 2009, pp. 213–218, doi: 10.1109/NAECON.2009.5426626.