Category: Research & Development

  • Simulating signal threats with Safran Electronics & Defense

    Simulating signal threats with Safran Electronics & Defense

    In universities across the world, theory lays the foundation, but in the field, realism builds true expertise.  

    For students studying GNSS engineering, textbooks and simulations alone are no longer enough. Tomorrow’s engineers need to use the same applications and work with the same complex environments that professionals face in the real world. This means using tools that generate actual RF signals, not just software abstractions — tools that recreate urban canyons, interference, jamming, spoofing and satellite dynamics with precision. 

    Safran has established the Minerva Academic Partnership Program, an initiative that brings its Skydel GNSS Simulation Engine to qualified educational institutions worldwide. 

    A Modern, Software-Defined Approach to GNSS Simulation

    At the heart of this initiative is the Skydel simulation engine, a software-defined GNSS simulator. Built to leverage commercially available off-the-shelf (COTS) hardware, Skydel eliminates the need for proprietary hardware. It delivers the full spectrum of satellite constellations — as well as LEO ones — and frequency bands. By integrating Skydel in their projects, researchers now have the tools to pursue ambitious ideas with confidence, such as:

    ■ Designing and testing custom signals or constellations not yet in existence

    ■ Simulating real-world scenarios that can include both environmental and man-made interference

    ■ Integrating and testing additional sensors and platforms through open-source plug-ins and hardware-in-the-loop setups

    ■ Conducting rigorous resiliency testing against jamming and spoofing in a controlled, repeatable environment without real-world risk

    ■ Building their own simulator with existing hardware components around Skydel

    Empowering the Next Generation of PNT Innovators

    Through the Minerva program, Safran provides full-feature Skydel licenses for faculty and student use, creating an environment where learning and innovation thrive. This initiative not only eliminates the barrier to entry but also fosters collaboration between academia and industry –— fueling a new wave of GNSS advancements.

    A Global Initiative

    Today, Minerva includes more than 80 member institutions and boasts a growing portfolio of peer-reviewed publications and conference presentations.

    “This momentum highlights the real-world impact of the program and its role in driving local research excellence and fostering a vibrant, collaborative international GNSS community,” said Pierre-Marie Leveel, program director of PNT simulation at Safran Electronics & Defense. “Safran Electronics & Defense’s Minerva program is more than just a software — it’s a mission to democratize GNSS simulation and nurture the next generation of PNT researchers. As innovation becomes more critical to national sovereignty, transportation, and space exploration, empowering students and researchers has never been more vital.” 

    Elevating GNSS Simulation

    The evolution of Safran Electronics & Defense’s GNSS simulators — across both software and hardware — has been shaped by the growing demands of users and the broader market.

    “The demand for multi-vehicle and multi-antenna scenarios has never been higher, and the same can be said for interference simulation,” said Pierre-Marie Le Veel, program director of PNT Simulation at Safran Electronics & Defense.

    To address these challenges, Safran’s GSG-7 and GSG-8 Gen2 simulators are engineered to handle a range of applications, from basic to advanced GNSS jamming and spoofing resiliency testing.

    The GSG-7 simulator is designed for location-aware applications and systems that depend on navigation or timing. With high-end performance — featuring a 1,000 Hz simulation iteration rate, high dynamics, real-time synchronization, and all-in-view satellite signal simulation — the GSG-7 is well-suited for development and integration projects that demand high performance and extensive constellation licensing. It supports multi-constellation and multi-frequency GNSS simulations and can be configured to operate with all current and upcoming GNSS signals.

    Meanwhile, the GSG-8 Gen2 is the latest iteration of Safran’s GSG-8 model, offering flexible simulation capabilities for any device that relies on GNSS signals. Built on Safran’s Skydel-based simulation platform, the GSG-8 Gen2 helps users model scenarios.

    Powered by high-end GPUs, the GSG-8 Gen2 offers reliable and precise GNSS signal testing. It can simulate thousands of signals, run multiple instances at once, and introduce jamming and spoofing to evaluate system resilience. The turnkey system features a redesigned chassis for greater connectivity, including six front-facing, high-quality RF outputs, a combined output covering the full GNSS bandwidth, and the same high-end simulation iteration rate as the GSG-7. This allows users to quickly get up and running with complex simulation requirements.

    “The market is also demanding realism,” Le Veel said.

    All Safran simulators are powered by the Skydel Simulation Engine, which is updated quarterly. Each release introduces new features, signals, and enhancements, enabling more authentic simulations and offering the flexibility to create virtually any GNSS testing scenario.

    Staying Ahead of Market Changes and Signal Threats

    The recent increase in signal interference threats has driven the demand for enhanced positioning, navigation and timing (PNT) resilience, leading to the broader use of both conducted and over-the-air (OTA) testing. The anticipated deregulation of controlled reception pattern antenna (CRPA) technology also is expected to open the door for civilian markets to perform testing.

    “Throughout the past few years, Safran Electronics & Defense has massively revamped our approach to the Wavefront platform and now offers the GSG-Wavefront for those testing CRPA antennas against jamming and spoofing threats,” Veel said.

    The ability to safeguard GNSS networks from jamming and spoofing attacks has never been more vital. Achieving this level of resilience calls for a GNSS simulator that can generate dedicated RF signals for evaluating the effectiveness of CRPA architectures.

    Safran’s GSG-Wavefront, featuring a shared local oscillator (LO) design, stands out as a field-proven, off-the-shelf solution for CRPA receiver testing. It has a customizable platform that offers upgradable options powered by Skydel — the company’s GNSS simulation engine.

    Le Veel added, “We are working hard to keep up with demand in both the defense and civilian markets.”
    In addition, Le Veel noted that Safran’s GSG-Anechoic is attracting attention from users who work with anechoic chambers, thanks to its multiple, independent RF outputs, automatic antenna mapping, and built-in calibration features for delay and power loss.

    Safran Electronics & Defense supports a wide array of users in both the civilian and defense sectors, spanning aerospace, critical infrastructure and transportation. In recent years, however, the company has seen its fastest growth in the New Space market. Safran’s simulators are used in a range of cutting-edge applications, including satellite navigation, low-Earth orbit (LEO) constellations, and rocket launch and landing systems.

    “We are proud that the flexible tools and features we have included in Skydel are being used in these incredibly robust applications,” La Veel said.

    A challenge for most GNSS simulation suppliers is ensuring compatibility and coherence with a wide range of GNSS receivers. La Veel shared that Safran Electronics & Defense is in a unique position, as it also designs and manufactures its own receivers, such as the newly released Skylight.

    “Additional challenges can arise when developing new signals or constellations, such as the newest LEO ones, said La Veel. “Our close partnerships with both Xona Space Systems and TrustPoint have allowed us to overcome these challenges.”

    A single GSG-8 Gen2 simulator from Safran Electronics & Defense can generate more than 2,000 signals without the need for additional hardware. This capability is essential when modeling legacy signals, multipath effects, jamming and spoofing scenarios, or even LEO-constellations.

    Safran simulators support all legacy signals, including GPS, Galileo, BeiDou, GLONASS, NavIC, QZSS and SBAS, across all bands and security features such as M-code, PRS and Galileo OSNMA. The systems also offer compatibility with emerging LEO constellations, including Xona’s PULSAR X1 and X5, as well as TrustPoint. Custom Signals and Custom Constellation features offer users the flexibility to create entirely new signals and satellite constellations, or to modify existing configurations.

    “It is de rigueur these days for companies to claim or incorporate AI into their solutions. In addition to using AI for tropospheric modeling based on real-world data, Safran Electronics & Defense has also taken a different approach to using AI in GNSS simulation,” Le Veel said.

    He added that the company’s upcoming demonstration at ION GNSS+ 2025 will reveal Skydel AI, a new tool designed to make scenario creation and parameter setting as simple as writing an email. “The amount of people who can easily now test their prototypes, products or systems will dramatically increase as the steep curve to learn GNSS simulation is flattened.”

  • Testing GNSS Receivers against Jamming and Spoofing Attacks

    Testing GNSS Receivers against Jamming and Spoofing Attacks

    Markus Irsigler, Sebastian Kehl-Waas, Carsten Stöber, Jürgen Dampf, Rohde & Schwarz GmbH & Co. KG

    GNSS jamming and spoofing pose a significant threat to global security, as satellite-based navigation and timing systems are utilized in various application fields, including critical infrastructure, transportation, military operations and communication networks. These intentional interferences disrupt signals or deceive GNSS receivers, leading to navigation errors, loss of situational awareness and potential safety hazards.

    Local, low-power jamming is often used to deliberately prevent GNSS-capable devices from recording their positions and being tracked. Such jamming devices, known as personal privacy devices (PPDs), are typically used to prevent fleet monitoring, concealing personal travel, or evading toll systems. Although mostly illegal, PPDs are fairly widespread and can pose a significant threat to GNSS availability, at least on a local scale.

    On the other hand, larger-scale incidents are observed very frequently. Regional jamming often occurs in conflict zones to protect military assets or disrupt enemy operations. Jamming has also been reported near critical infrastructure. Spoofing is typically less frequent than jamming, but it poses a more concerning integrity threat when incorrect PVT data is used for navigation. Well-documented events include the (in)famous 2017 incident affecting ships in the Black Sea, where a spoofed GNSS signal led vessels to report incorrect positions. Jamming and spoofing also play an important role in the Ukraine conflict, where it is used to disrupt enemy drones, guided munitions, and navigation. Such events clearly highlight the vulnerability of GNSS-dependent systems and the need for robust mitigation techniques and strategies.

    Against this background, testing how GNSS devices react to such threats has become more and more important, especially if they feature dedicated jamming detection and mitigation techniques. In such cases, the main test objective is to verify that these detection and mitigation techniques work as expected and that the GNSS receiver reacts properly and as expected in response to such attacks.

    Categorization of GNSS Threats

    Although jamming and spoofing can be considered the most critical threats, GNSS signals can be degraded in various other ways. Signal degradation effects can occur anywhere along the path from the GNSS satellite to the user. They can be caused by the transmitting satellite itself, usually in the form of hardware malfunctions, typically referred to as “evil waveforms.” They can also occur along the signal path in the form of ionospheric and tropospheric errors or scintillation effects, or they can be a result of the conditions in the vicinity of the GNSS user. This includes jamming, spoofing, RF interference caused by other signals, as well as signal obscuration and multipath caused by buildings or trees.

    “Evil waveforms” can pose a significant threat to GNSS signal integrity, leading to large positioning errors. However, the occurrence of this effect is very rare and therefore not specifically considered in this article. There are also some atmospheric effects that have the potential to significantly degrade the quality of GNSS signals. Especially ionospheric and tropospheric scintillation due to temporal, fast-changing atmospheric conditions can cause rapid amplitude and phase variations, leading to reduced C/N0 or even loss of lock. Again, this does usually not happen every day and is therefore not discussed in detail below either.

    The most critical and common GNSS threats originate from interference signals that occur in the vicinity of a user receiver. Unlike system-inherent threats that originate from GNSS satellites or atmospheric conditions, these threats can be termed as “man-made” and categorized as shown in Figure 1.

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    Figure 1. Categorization of man-made GNSS threats. Credit: All figures provided by authors.

    Jamming can be divided into two types of attacks. Brute-force jamming aims at completely blocking GNSS reception for a receiver by deliberately emitting interference signals like CW interferers, broadband noise or frequency sweeps with very high-power levels. As a result, the carrier-to-noise values will drop below the receiver’s acquisition and/or tracking threshold, and GNSS signals cannot be processed anymore. In contrast to such a simple jamming attack, where the attacker needs to have only basic knowledge about the GNSS signals (e.g. center frequencies and signal bandwidths), systematic jamming is a much more sophisticated attack, which can be further divided into

    • Intelligent or smart jamming. The objective is to jam only a specific part of the navigation message (e.g. the ephemeris data section), so that the navigation message can never be fully decoded and the receiver will never be able to perform a position fix. All other parts of the navigation message remain unaffected, allowing signal tracking to continue for the receiver. Figure 2 illustrates this attack on the GPS L1 C/A signal.

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    Figure 2. An intelligent jamming attack performed on a GPS L1 C/A signal.

    Smart jamming is much more complicated to implement for an attacker as the jammer must only be active during specific time intervals; this requires that the jammer is somehow synchronized with GNSS/Coordinated Universal Time. Moreover, the attack requires knowledge of the navigation message structure and what information the receiver needs to compute a position. Nevertheless, if done correctly, the attack is rather difficult to detect [1].

    Matched spectrum jamming. The objective is to generate a GNSS-like jammer signal with the same spectral characteristics as the real GNSS signals but without any valuable navigation information (i.e. the navigation message is missing). Matched-spectrum jamming is not straightforward, and to be effective, an attacker must replicate the GNSS signals for multiple visible satellites simultaneously, considering signal characteristics such as pseudo-random noise codes and, ideally, their correct Doppler shifts.
    In contrast to jamming, GNSS deception techniques aim to force the receiver to compute an incorrect PVT solution, compromising the integrity of GNSS-based navigation. The two basic methods are:

    Meaconing. This rather simple approach is based on rebroadcasting a delayed version of live GNSS signals. This can be realized by using a commercial GNSS repeater. Alternatively, previously recorded actual GNSS signals can be replayed.

    Spoofing. This includes generation and broadcast of forged GNSS signals. This is typically done using a GNSS simulator, but specialized, modified GNSS receivers combined with a transmitting unit can also be used. The simulated signals need to be self-consistent, i.e. a GNSS receiver must be able to compute a PVT solution based on the simulated constellation. Spoofing attacks can be rather simple, e.g. broadcasting high power signals that represent a different location than those of the receiver under attack. The aim is to force the receiver into a reacquisition process, tracking and processing only the fake GNSS signals. More sophisticated spoofing attacks are possible [2], but not discussed in this article.

    Additionally, the PVT performance of a GNSS receiver can also be degraded by objects in the vicinity of a GNSS user, causing signal obstruction and reflections from buildings, trees, or the ground. Multipath can cause significant ranging and positioning errors. Multipath effects can hardly be avoided and must be seen as a permanent threat to GNSS signal quality.

    Finally, other existing signals and services can interfere with GNSS, either because there is a frequency overlap (in-band interference) or harmonics from other signals fall into the GNSS bands (out-of-band interference). As an example, the upper part of the DME/TACAN band overlaps with a significant portion the GNSS L5 band. The effect of this type of interference on GNSS receiver performance can be analyzed by performing coexistence tests.

    RX-Internal Detection and Mitigation Methods

    At least some of the threats discussed above can be detected and/or mitigated by the GNSS receiver. The capability of a GNSS receiver to detect and apply countermeasures to threats such as multipath, jamming or spoofing depends on the receiver’s availability of specific features and its basic architecture. Figure 3 shows the basic building blocks of a typical GNSS receiver with a single, fixed reception pattern antenna (FRPA).

    Figure 3. Basic architecture of a FRPA receiver

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    The three basic building blocks are the antenna, the RF front-end and the digital signal processing section. The antenna is responsible for receiving the weak GNSS signals as well as for successive amplifying and band-limiting. It typically features a low noise amplifier (LNA) and a band-pass filter. The signals are then fed to the receiver front-end where the signals are amplified, down-converted to an intermediate frequency and converted to the digital domain. Part of this process is the automatic gain control (AGC) loop; the AGC acts as a variable amplifier, adjusting the power of the incoming signal and keep it constant over time. The sampled and quantized stream of IQ data is then fed to the digital signal processing section, where signal conditioning, acquisition and tracking, and PVT solution computations take place.

    In contrast to using a single antenna with a fixed antenna pattern, some receivers use an adaptive antenna array, also referred to as controlled reception pattern antenna (CRPA). The idea is to weigh the signals received by each element according to dedicated optimization criteria. Typical optimization criteria are to minimize the signal’s output power towards a dedicated direction (“null-steering”), or to maximize the signal to interference or signal to noise ratio (“beamforming”). The underlying receiver architecture is more complex as signal weighting mechanisms must be added to the signal processing chain. These can be integrated before the digital processing block (“pre-correlation”) or implemented as an additional processing step between the correlation and tracking stages in the digital signal processing section (“post-correlation”). Both approaches are very effective in mitigating jamming and spoofing attacks, as they can either form a null in the direction of a strong jammer/spoofer or form beams towards the wanted signals from GNSS satellites, thereby de-weighting any unwanted signals coming from other directions.

    Pre-correlation architecture of a 4-channel CRPA receiver
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    Post-correlation architecture of a 4-channel CRPA receiver
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    Within the processing chain of a GNSS receiver, there are different approaches and methods to detect and mitigate interfering signals, which are summarized in the following table:

    AGC monitoringMonitoring of the gain in the AGC loop. A sudden drop of the AGC gain can be an indication of an interfering signal; detection of high-power interferers; low-power spoofing attacks very difficult to detect
    Spectrum monitoringDetection of interferers and jammers above the noise floor; especially suited for detecting CW interferers. Not suited for the detection of matched-spectrum jammers, spoofers and meaconing attacks as their spectrum is typ. identical to the GNSS spectrum.
    Frequency domain adaptive filteringDynamically identifies and suppresses unwanted frequency components (e.g., interference or multipath) by adjusting (notch) filter parameters.
    Pulse blankingPulse blanking is a time-domain interference detection and mitigation technique used in GNSS receivers to detect and suppress short-duration, high-power pulses, typically caused by pulse jammers or Radar transmitters. Monitors the incoming signal power in short time windows and “ignores” this signal part in case certain power level thresholds are exceeded. Effective to mitigate pulsed jammers, not suited for multipath mitigation or anti-spoofing measures.
    C/N0 monitoringMonitoring over time and/or comparison against theoretical max. value; detection of all types of interferers; low-power spoofing attacks very difficult to detect
    Time jump detectionTime jumps (backwards or forwards) are clear indications for meaconing or spoofing attacks.
    PVT monitoring, incl. RAIMExample: The computed position can be constantly compared against a known reference position. Not possible to distinguish between jamming/spoofing or other environmental effects like multipath. This also includes receiver-autonomous integrity monitoring (RAIM) schemes, that can be considered as a special form of PVT monitoring.
    Doppler monitoringCompare Doppler against theoretical/geometrical values; monitored Doppler profiles may show irregularities in case of an attack. Difficult to be separated from environmental or atmospheric effects.
    CMC monitoring„Code minus Carrier“ observable shows irregularities and increased noise in case of an attack. Difficult to be separated from environmental or atmospheric effects.
    Signal Quality Monitoring (SQM)Sampling of the correlation function using a few correlators; can detect distortions of the correlation function resulting from multipath, jamming or spoofing attacks.
    Massive multi-correlator monitoringContinuous, high resolution observation of the code/Doppler space. Can be done during signal acquisition and tracking. Can detect multipath, jamming, meaconing and spoofing attacks.

    Derived Test Requirements

    Based on the typical threat signal and attack characteristics, as well as the receiver-internal detection and mitigation methods discussed above, the test and simulation requirements listed in the table below can be derived. In addition to the requirements related to threat simulations (grey background), the table also contains “base requirements” for the simulation of realistic GNSS scenarios (blue background):

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    Testing: Methods, Setups and Challenges

    The test methods, strategies and setups used depend on the architecture of the GNSS receiver being tested, the receiver features that need to be evaluated and the specific testing objectives.

    A first categorization can be made by examining the origin of the GNSS signals being used for testing. The signals may come from real GNSS satellites and be used instantly and on-site (live GNSS testing) or recorded, stored, and played back in the lab (record/replay). Alternatively, testing can be done entirely in a lab environment using GNSS simulators. There are also hybrid test methods that will be discussed later in this article. In comparison to using real GNSS signals – either via live testing or the record/replay approach – using GNSS simulators in a lab environment offers significant benefits.

    Simulation vs. Live GNSS Testing. One major drawback of using live signals is that the system conditions are often unknown at a given point in time, and – most importantly – they change over time. The locations of the satellites — and thus the geometric conditions — change as the satellites move along their orbits. Errors, such as atmospheric effects, are also time- and location-dependent. One of the most unpredictable error influences is multipath. The magnitude of multipath errors depends on a variety of different parameters, including the number of reflections, the distance between the reflection points and the antenna or the strength of the reflected signal. The latter is determined by the material properties of the reflecting surface. Both the geometric conditions and the material properties of the reflectors change or may change over time – the geometric conditions due to the permanent motion of the satellites and the reflector properties due to meteorological influences like rain, dew, or snow.

    As a result, when using live signals, one must expect that the conditions change permanently and unpredictably and will never be the same for two distinct points in time. It is therefore very unlikely that two successive test runs can be performed under identical conditions. Repeatable testing, which is one of the most important test requirements, is impossible when using live GNSS signals.

    Well-defined and controlled simulation conditions can only be ensured by using a GNSS simulator. A simulator typically offers fully customizable and repeatable scenarios (i.e., one and the same test scenario) that can be repeated as often as needed, producing the same signals with the same characteristics. Moreover, a simulator is often a more cost-effective and efficient solution, whereas using live signals would be time-consuming, complex, expensive or even impractical (e.g. test of airborne and spaceborne receivers).

    The following discussion of typical test setups therefore focuses on the use of signal generators for GNSS testing. In terms of test scenarios, the focus will be on jamming, spoofing and coexistence testing. Testing against multipath influences is not specifically discussed below.

    Basic simulator setups. The basic approach for testing against GNSS threats is to combine a “clean” reference GNSS simulation scenario with interfering signals and add the combined signals to the device under test (DUT). This basic concept can be implemented using two separate signal generators or an integrated solution that combines GNSS simulation and threat signal generation in a single instrument. Based on the architecture of the integrated solution (1 RF output vs. multiple RF outputs), GNSS and interfering signals are already combined internally, or GNSS and interfering signals can be fed to different RF outputs and combined with an external combiner before fed to the DUT.

    Using two separate signal generators for GNSS threat testing. The interference generator (red) can either be a second GNSS simulator for generating spoofing signals or any other signal generator providing non-GNSS signals for jamming or coexistence tests. 
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    Using a GNSS simulator with integrated interference generation capabilities. The signal generator features 1 RF outputs. GNSS and interfering signals are combined internally. An external combiner is not needed, but the dynamic range between GNSS and interferer (J/S) is usually limited.
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    Using a GNSS simulator with integrated interference generation capabilities. The signal generator features 2 RF outputs. GNSS and interfering signals fed to individual RF ports and combined externally. This requires an external combiner, but with the benefit that very high J/S ratios can be achieved.
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    Conducted testing vs. OTA testing. The basic setups introduced above only work if the receiver has dedicated and accessible input connectors to feed the antenna signal to the receiver’s front end. This is sometimes not the case, so that conducted testing is not possible and over-the-air (OTA) tests must be considered. A classic example of such DUTs is mobile phones, where no antenna connector is available, at least not without dismantling the device.

    Testing such devices against interfering signals is still possible by using a shield box. The shield box has an RF input to feed in the combined GNSS and interfering signals. The signals are then retransmitted into the inside of the box and the DUT uses its integrated antenna to receive and process the signals coming from the GNSS simulator.

    Using a GNSS simulator in combination with a shield box to test GNSS devices with integrated antennas.
    OTA GNSS threat simulation using a shield box with 2 RF inputs and 2 transmit antennas. The GNSS signals and the interfering signals are fed separately (uncombined) into the shield box.  

    An alternative setup is to use a shield box with two RF inputs. In this case, the wanted signals and the interfering signals are not combined externally but are fed to the shield box via separate RF input connectors and transmitted to the GNSS DUT via separate transmit antennas.

    Additional aspects and challenges must be considered when performing OTA tests using mobile phones as a GNSS DUT. This includes conducting a proper cold start, removing all preexisting navigation-related information from its memory, and disabling any other sensors that may contribute to computing the phone’s position, including any assisted GNSS services. This is typically not a concern for most standalone GNSS receivers that feature dedicated cold start procedures and usually have no other positioning sensors on board. On the other hand, initiating a real cold start for GNSS modules in mobile phones can be tricky. Just rebooting the phone does not necessarily work, and the availability of dedicated settings also depends on the phone’s operating system (e.g. iOS vs. Android).

    Another challenge during OTA testing of mobile phones is how to assess and analyze the impact of any interfering signals on signal acquisition, tracking and positioning. This requires detailed analysis and monitoring features on the mobile phone, which are typically not a standard feature of the phone’s operating system. Specialized GNSS monitoring apps can be used instead. To get access to the data during the test, special screen mirroring apps can be installed on the mobile phone.

    Testing with live signals. GNSS tests may also be performed in combination with live GNSS signals using already existing field infrastructure such as GNSS receivers installed at mobile base stations. A typical use case is to add one or several jamming/spoofing signals, or even an entire (stronger) “spoofing constellation” to an existing “live GNSS constellation” and test how the GNSS receiver reacts to such an attack. The typical test setup is illustrated in Figure 4.

    Photo: Figure 4. The receiver’s response to interference is evaluated by introducing jamming or spoofing signals, alongside normal satellite signals using existing field infrastructure. This setup is often used to assess reactions to attacks.
    Photo: Figure 4. The receiver’s response to interference is evaluated by introducing jamming or spoofing signals, alongside normal satellite signals using existing field infrastructure. This setup is often used to assess reactions to attacks.

    This approach may be a good alternative to simulating everything with a GNSS simulator, as much more HW, i.e., more GNSS channels and more RF paths, are required with a simulator-internal approach. On the other hand, there are also some challenges associated with this test method, e.g., the signal generators, which need to be operated in a field environment. Moreover, for more sophisticated spoofing attacks, a prerequisite is the capability to time-synchronize the GNSS simulation with the live GNSS constellation.

    CRPA testing. For testing GNSS receivers with multiple antenna inputs, particularly CRPA systems, several RF sources/paths need to be combined and synchronized. The following illustration shows a possible setup for testing a 4-channel CRPA receiver against jamming or spoofing attacks. It is based on the 2-path architecture introduced above. It consists of two signal generators for generating GNSS signals for each antenna (left part of the setup) and two signal generators for generating the jammer/spoofer signals (right part of the setup). GNSS and interfering signals are combined per antenna element and fed to the RF inputs of the CRPA receiver under test.

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    For CRPA testing, generating phase-coherent signals is a must, i.e., it must be ensured that the phase relations between the GNSS signals and between the interfering signals represent the actual geometrical conditions and, above all, remain consistent throughout the simulation. To achieve this, a common LO signal needs to be used for generating the GNSS and interferer signals in all signal paths.

    Another challenge is related to calibration. To correctly simulate the directions of the satellite signals and the interference signals, the test system must be calibrated at the RF interface to the DUT with respect to amplitude, phase and propagation time. This means that the amplitude, phase and propagation time differences between the individual RF paths, resulting for example from cables orRF components, must be compensated.

    Rohde & Schwarz Solution

    With GNSS test solutions from Rohde & Schwarz, all the relevant requirements for testing GNSS receivers against GNSS threats can be addressed. Available test solutions range from simple, single-channel, waveform-based signal generation with limited simulation time up to multi-frequency, multi-constellation GNSS simulators with 2 RF outputs, hundreds of GNSS channels and internal threat simulation capabilities, including non-GNSS signals for jamming and coexistence tests. For these advanced GNSS tests, the R&SSMW200A high-end vector signal generator is the ideal choice. It can be equipped with a multitude of GNSS options and feature sets.

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    Photo: Testing against GNSS threats with the R&S SMW200A

    Jammer simulation. There are several ways to generate jamming and coexistence signals with Rohde & Schwarz signal generators in general and especially with the R&SSMW200A. Simple interference signals like noise or a CW interferer can be generated by using an optional integrated noise generator. For coexistence testing, the instrument can be equipped with signal generation capabilities for various standard-conforming communication signals, such as LTE. Customized interferer signals in the form of waveform files can be created by external software tools like MATLAB or Python and replayed by the instrument.

    Customized jamming signal as well as entire jamming and coexistence scenarios can also be created using the R&SPulse Sequencer. The software allows to generate typical simple GNSS jamming signals like CW interferer, frequency sweeps, or pulsed interferers, but also complex jamming scenarios with consideration of moving interference sources and moving GNSS receivers, user-defined antenna patterns and scans. Depending on the signal characteristics, the jammer and receiver positions and the antenna arrangement, the software calculates the correct amplitude, phase angle and signal propagation times for the jamming signals.

    Further reading

    [1] Curran, James T. et. al. (2017): A look at the Threat of Systematic Jamming of GNSS, InsideGNSS, September/October 2017

    [2] Dovis, Fabio et. al. (2015): GNSS Interference Threats and Countermeasures, GNSS Technology and Application Series, Artech House, 2015

  • Safran’s Skydel simulator now supports Xona’s Pulsar LEO navigation signals

    Safran’s Skydel simulator now supports Xona’s Pulsar LEO navigation signals

    Safran Electronics & Defense‘s Skydel GNSS simulation platform is now fully certified to support simulation of Xona Space Systems’ low-Earth orbit positioning, navigation and timing (LEO-PNT) signal, Pulsar.

    According to the companies, this certification is the culmination of a rigorous multi-phase validation program jointly led by Safran and Xona engineering teams. It underscores Safran’s commitment to advancing robust, high-fidelity testing for next-generation LEO-PNT services. With this milestone, engineers can now use Skydel to evaluate Pulsar’s performance in environments that reflect real-world complexity, interference and operational demands.

    Skydel now simulates Xona’s Pulsar X1 signals, delivering centimeter-level precision, 100x signal strength and enhanced resilience — capabilities that Pulsar will soon bring to orbit.

    “With Skydel-powered simulators certified for Pulsar X1, our customers have more possibilities than ever,” said Pierre-Marie Le Veel, program director of PNT simulation at Safran Electronics & Defense. “They can test LEO and legacy constellations side by side, introduce complex interference, and explore entirely new scenario combinations — all from a single, flexible platform. This is a major step forward in enabling engineers to push the boundaries of GNSS testing.”

    Beyond accuracy, Skydel enables advanced resilience testing, including jamming, spoofing and other NAVWAR threats. Its modular, future-ready architecture ensures seamless integration of new Pulsar signal types and constellation updates, offering the agility needed to keep pace with the evolving LEO PNT landscape and demands for trusted, high-integrity PNT.

    “Validation is the bridge between innovation and trust,” said Tyler Reid, CTO of Xona. “By replicating Pulsar at full fidelity, Skydel empowers engineers to design and validate solutions for the most demanding navigation and timing challenges — without waiting for on-orbit availability.”

    Skydel’s certified Pulsar simulation capability is available now to partners and customers worldwide.

  • Safran launches AI tool for GNSS simulation automation

    Safran launches AI tool for GNSS simulation automation

    Safran Electronics & Defense has unveiled Skydel AI, a breakthrough in GNSS simulation technology that uses artificial intelligence (AI) to automate and simplify simulation scenario setups.

    Skydel AI streamlines GNSS simulation scenario creation through intelligent automation and an intuitive interface. Using natural language commands, Skydel AI allows users to query GNSS/Skydel topics, request assistance and dynamically configure simulation parameters by creating Python code for use by Skydel. The technology eliminates complexity and significantly reduces setup time.

    “Soon available as part of Safran’s Support offerings, Skydel AI can help customers drastically improve their development cycles by accelerating manual scenario tuning and reducing long test cycles within Skydel,” said Pierre-Marie Leveel, program director for PNT at Safran. “Already established as the most flexible, robust, and accurate GNSS simulation engine, Skydel never stops innovating and delivering what the market requires – whether it is more realism, higher accuracy, more environment complexity, or ease of use.”

    The company also introduced an AI-powered tropospheric model that enhances Skydel’s tropospheric simulation using real-time weather data and AI predictions to improve wet delay accuracy. Integrated with the Open-Meteo API and Skydel’s system, it relies on a neural network trained on 14 million samples from 221 GNSS stations, delivering up to 88% more accuracy. This model will be available in a future Skydel release.

    The technical breakthrough reflects Safran Electronics & Defense’s commitment to redefining GNSS simulation with intelligent, adaptable and high-performance solutions for mission-critical applications.

  • Qascom delivers Moon test bed

    Qascom delivers Moon test bed

    Qascom S.R.L. (IT) has successfully delivered the final presentation of the NAVISP-EL2-081 –  MOOD  (Moon testbed) project, marking the culmination of a multi-year effort to develop a cutting-edge GNSS simulation testbed for lunar, cislunar and space-based PNT applications.

    For this purpose, Qascom upgraded its QA707 GNSS simulator introducing advanced features such as lunar-specific ranging strategies, support for multiple coordinate reference systems, custom signal transmitters (including LunaNet AFS), and a 3D Viewer for real-time scenario visualization. It also integrates BeiDou B1C signal simulation and dual-frequency RF streaming capabilities.

    Key achievements include successful validation of LunaNet and BeiDou signals, implementation of Moon Principal Axis (Moon-PA) ranging, and integration with open-source and COTS receivers. The simulator has already supported the project NAVISP-EL1-062 – DEMOS-1(Lunar Surface PNT Beacon Demonstrator) and is now Qascom’s flagship GNSS simulation product.

    Looking ahead, Qascom plans to enhance QA707 with direct dual-frequency RF output and integration with SDR hardware, being developed under the project NAVISP-EL2-090 – JNRS (Joint Navigation Radio System).

    The project was supported through NAVISP Element 2 for PNT competitiveness for European industry. The slides of this final presentation can be found here.

  • Safran Federal Systems upgrades BroadSim product line

    Safran Federal Systems upgrades BroadSim product line

    Safran Federal Systems introduced BroadSim Genesis, the latest addition to its BroadSim product line, at the Institute of Navigation’s 2025 Joint Navigation Conference in the Greater Cincinnati area.

    Developed for the U.S. defense community, BroadSim Genesis advances GNSS simulation and NAVWAR testing with significant improvements in signal capacity, operational flexibility and user experience. The system delivers high-fidelity, threat-representative environments designed to support next-generation positioning, navigation and timing (PNT) resiliency.

    BroadSim Genesis can generate up to 2,000 signals, enabling advanced multi-constellation simulations across medium Earth orbit, low Earth orbit and alternative PNT sources within a single test environment. The system is engineered to meet modern NAVWAR requirements, supporting multi-antenna and multi-vehicle configurations, M-Code, and integrated jamming and spoofing capabilities to counter sophisticated signal threats.

    The user interface features an integrated front panel with N-type connectors, removable drives and an onboard timing card, offering ease of use, security and field readiness.

    “BroadSim Genesis is built for operators who demand flexibility, fidelity and performance in their GNSS simulation tools,” said Trevor Dougherty, vice president of sales at Safran Federal Systems. “Whether validating mission equipment, training for NAVWAR scenarios or assessing new PNT architectures, BroadSim Genesis gives defense users the edge they need”

  • LabSat launches scalable solutions for GNSS signal testing

    LabSat launches scalable solutions for GNSS signal testing

    LabSat has expanded its GNSS signal record, replay and simulation portfolio with the introduction of three new LabSat 4 variants: LabSat 4, LabSat 4 Core and LabSat 4 Lite. LabSat seeks to provide engineers and developers with scalable solutions tailored to a wide range of testing requirements and budgets.

    LabSat 4 delivers advanced capabilities, including up to 12-bit I&Q quantization and support for recording and replaying external data such as CAN-FD, RS232, and digital inputs. This model is designed for demanding GNSS signal testing, offering high precision and extensive customization to address complex modern testing scenarios.

    LabSat 4 Core offers the same features as the original LabSat 4, except it is limited to a maximum of 4-bit I&Q quantization. This makes it a cost-effective choice for applications where the highest signal capture resolution is not necessary, while still providing a comprehensive feature set.

    LabSat 4 Lite is optimized for affordability, featuring streamlined 2-bit I&Q quantization and omitting external data recording and replay. It is well-suited for production line testing and other scenarios where quantization depth is not a critical factor.

    All LabSat 4 variants include three RF channels with selectable bandwidths up to 60 MHz, adjustable quantization options depending on the model, manual gain control, multi-unit synchronization, and full backward compatibility with LabSat 3 Wideband file formats. The series is compact, portable, and designed for efficient use in both field and laboratory environments.

    A key benefit of the LabSat 4 range is the ability to upgrade between models via a license file, allowing users to start with LabSat 4 Lite and move to Core or the full LabSat 4 as their testing needs evolve, without replacing hardware. Customers can also select between Replay-Only and Record-and-Replay configurations across all variants.

  • JAXA selects Spirent’s PNT simulation solution for lunar navigation program

    JAXA selects Spirent’s PNT simulation solution for lunar navigation program

    The Japan Aerospace Exploration Agency (JAXA) has selected Spirent Communications to supply its lunar positioning, navigation and timing (PNT) simulation solution. The solution will support JAXA’s lunar exploration efforts and aid in developing essential navigation infrastructure for future moon missions.

    Spirent’s PNT X solution allows JAXA to simulate lunar PNT services in a controlled laboratory setting before their deployment on the moon. This capability is critical for testing and validating navigation equipment for lunar missions in accordance with the emerging LunaNet specifications, which include adaptable S-band frequency solutions. The system also ensures scalability for future space exploration.

    Using the PNT X system, JAXA can experiment with novel S-band signals and evaluate the performance of receivers that rely on standalone S-band Lunar PNT signals or a combination of Lunar PNT and Earth-based L-band GNSS infrastructure. The simulation of these signal combinations demands high levels of precision, which Spirent’s specialized architecture is designed to meet.

    This collaboration builds on a longstanding relationship between Spirent and JAXA. In 2011, JAXA utilized Spirent’s simulation technology to verify the performance of early Quasi-Zenith Satellite System (QZSS) receivers. Since then, Spirent simulators have supported multiple advancements in QZSS.

    Spirent’s lunar PNT simulation solution seeks to present new opportunities for space agencies developing lunar constellations, satellite and receiver developers and organizations planning lunar missions or seeking to establish additional PNT infrastructure on the moon.

  • Innovation Insights: It starts with the physics

    Innovation Insights: It starts with the physics

    Click to read the full Innovation article, “Innovation: A look back at 35 years of ‘Innovation’


    Innovation Insights with Richard Langley
    Innovation Insights with Richard Langley

    IT’S ALL PHYSICS. How things work, that is. Well, maybe a little chemistry too in some cases. I might be a little biased in my opinion given that I’m an applied physicist by training. Radio? Satellite navigation? Yes, the principles of their operation are all governed by physics. Many physicists of my generation started out as radio tinkerers. I’ve recounted in this column before that I built my first radio (from a kit) when I was 14 (not counting the crystal radio that my father helped me to put together when I was 8 or 9). I built a few more during high school, got into radio astronomy as an undergraduate and did a Ph.D. in the application of very long baseline (radio) interferometry to geodesy.

    The great American physicist Richard Feynman was also a radio tinkerer in his youth. He recounts in one of his autobiographical books how he used to fix radios. Since he would approach the task of repairing each non-functioning set by first contemplating why it wasn’t working, he got the reputation of fixing radios by thinking!

    One of Feynman’s special abilities was in explaining how things worked. In fact, he has been called “The Great Explainer.” He authored what is arguably the best physics textbooks ever produced: The Feynman Lectures on Physics. The three-volume set, developed from his Caltech lectures to undergraduates between 1961 and 1964, covers mechanics, radiation, electromagnetism, matter and quantum mechanics. Many students and practicing physicists have learned or relearned aspects of physics from the famous “red books.” Many more will now thank Caltech, which recently put the Lectures online for anyone to read.

    In the February 2016 column, we learned about the development of a microprocessor-controlled multi-element GNSS antenna array for interference rejection. While there are many textbooks that describe how multi-element antennas work, Feynman explains their operation in his Lectures from first principles–from the principles of physics. The phenomenon governing the behavior of antennas with multiple elements is called interference.

    If we combine two electromagnetic waves, they will interfere with each other with a result that depends on the relative phase (or phase difference) of the waves. The waves might reinforce each other leading to a larger net amplitude, called constructive interference, or partially or fully null each other out, called destructive interference. When we apply this concept to the signals transmitted by a pair of antennas making up an array in a horizontal plane, we find that the array has directionality. That is, if we space the antennas by one-half wavelength of the signal to be transmitted and feed the antennas in phase (zero phase difference), we will transmit a strong signal in the directions perpendicular to the baseline connecting the antennas (say east-west) and no signal in the orthogonal directions (north-south). If we use this antenna pair for receiving, we will have a null in the reception pattern to the north and to the south and will be insensitive to signals arriving from those directions. And as Feynman describes in his lectures, by adding more antennas to the array and “some cleverness in spacing and phasing our antennas,” we can have a fairly narrow pattern null in a chosen direction. In the case of a GNSS antenna array, that direction might be that of a jamming signal and so we can null out the jammer and maintain a positioning capability.

    There is more to it in developing a practical microprocessor-controlled GNSS antenna array, but it starts with the physics.

  • Innovation: A look back at 35 Years of ‘Innovation’

    Innovation: A look back at 35 Years of ‘Innovation’

    Innovation Insights with Richard Langley
    Innovation Insights with Richard Langley

    Click to read the full Innovation Insights column, Innovation Insights: It starts with the physics”

    This is my 300th and last “Innovation” column in GPS World. I have mixed feelings about stopping the column. I’ve really enjoyed doing it for the past 35 years, but editorial deadlines can be difficult to meet sometimes, especially when I’ve got other things to get done or if they come in the middle of a vacation.

    To rephrase the old adage, editorial deadlines wait for no one. Looking back, I don’t know how I managed to initially produce six and then 10 columns each year, along with all my other duties as a university professor. Mind you, as I’ll soon discuss, most of the articles in the columns were authored by others. My job mostly was to edit the articles to help the authors tell their stories in a particular GPS World style and sometimes to improve their submitted figures. Additionally, in 2006, I started to write a sidebar called “Insights” to provide some basic background material about each column’s topic. A few years ago, I became editor-in-chief of the Institute of Navigation’s journal NAVIGATION, which takes up a bit of my time, along with lecturing and managing a research team. So, at 75, I thought it might be a good time to lessen the load a little bit.

    In this last column, I’m going to tell the story of how “Innovation” came to be and review some of the column’s developments over the years.

    How it all began

    In the fall of 1989, GPS World’s founding editor, Glen Gibbons, approached Dave Wells, Ph.D., a fellow faculty member in the then Department of Surveying Engineering at the University of New Brunswick (UNB) – about assisting with a “technology/product development column” in the magazine he was about to start. Glen wanted it to provide “an analysis and commentary on the research, development, product issues and needs of the GPS community.” And, since GPS World readers would have marked differences in their knowledge and expertise in the GPS area, “the column should deal with issues that have broad application and interest and are presented in terms that are accessible to as wide a range of readers as possible,” Glen said in a letter to Dave.

    Glen had heard about Dave’s (and UNB’s) early involvement with GPS. When I came to UNB in 1981, UNB was already carrying out some of the first theoretical studies on how GPS could be used by surveyors and geodesists for precise positioning. Shortly afterwards, UNB participated in some of the first surveys using the Macrometer V-1000 and Texas Instruments TI 4100 receivers and developed software to process the resulting data. In 1983, Dr. Gerhard Beutler from the Astronomical Institute of the University of Bern came to UNB on a sabbatical and began developing his own GPS data processing software that would eventually become the Bernese GNSS Software or just “Bernese” to those in the know. Somehow, in between our GPS algorithm and software development, teaching, mentoring graduate students and other duties, we managed to self-publish the first textbook on GPS, Guide to GPS Positioning. With a publication date of December 31, 1986, it went on to sell more than 12,000 copies in the English version alone. It was also translated into Chinese, Spanish and Vietnamese. So, perhaps it is not surprising that Glen came to knock on UNB’s door when he was starting up his magazine.

    Getting back to Glen’s letter, he went on to say, “It would be possible to handle the preparation or presentation of the column in one of several ways: We could identify a single person who would have primary responsibility for writing all the columns and whose byline would appear on them; we could have a person act as the coordinating editor responsible for obtaining suitable contributions from various authors; or we could establish a collective or institutional editorship with column responsibilities shared among a pool of contributors.”

    The letter arrived in early November 1989, and Dave, I and Alfred Kleusberg, Ph.D., who was a research fellow in the department (and subsequently a professor), began to discuss whether we wanted to take on the responsibility for the column and, if so, how we would manage it. I shortly departed to the University of Bern, where I would spend the better part of two months during my first sabbatical. Communication had to take place using e-mail, although phone, telefax and telex were also possible. Universities had e-mail before most other organizations thanks to BITNET (known initially in Europe as the European Academic and Research Network or EARN), a computer network that predated the Internet. My BITNET e-mail address was lang@unb or [email protected]. As I recall, the personal part of the address was limited to at most four characters. So, when UNB joined the Internet, I basically kept the same e-mail address: [email protected]. I talked about GPS and the Internet in the November 1995 edition of the column. But I’m getting ahead of myself.

    FIGURE 1: First page of Dave Wells’ notes from December 31, 1989 on how UNB would manage the “Innovation” column. (Photo: GPS World archives)
    FIGURE 1: First page of Dave Wells’ notes from December 31, 1989 on how UNB would manage the “Innovation” column. (Photo: GPS World archives)

    That December, the three of us more or less agreed that we would handle the column in some form. From Switzerland, I sent Dave a list of 12 possible topics for the column, but I added the rider: “Note that I am not necessarily volunteering to write any of the articles.” As we know, things turned out a little differently. During the university’s Christmas break, after I returned to Fredericton, we met at Dave’s house to discuss how we would manage the column in more detail. We met on New Year’s Eve — a Sunday afternoon — and decided that Alfred Kleusberg and I would manage the column as co-editors, with Dave serving as one of the inaugural members of the magazine’s Editorial Advisory Board. The column editorship was to be a blend of the second and third of Glen’s suggestions. The task wasn’t supposed to be too onerous. After all, the magazine was to be published bimonthly. Lots of time to get someone to write an article and for Alfred and I to edit it. Or so we thought. And the column was to be called, simply, “Innovation.” I don’t recall who came up with the name — whether it was one of the three of us or Glen, but the notes from that Sunday afternoon meeting have “Innovation” written at the top of the first page (see FIGURE 1). Ideally, as per Glen’s suggested guidelines, column articles were to be tutorial in style or written in a way that they could be understood, for the most part, by non-experts in the field.

    At that Sunday afternoon meeting, we decided that Dave and Alfred would write the article for the first column. It was an introduction to GPS and some possible applications titled “GPS: A Multipurpose System.” With a couple of iterations of the article back and forth with Glen via fax (GPS World didn’t have e-mail until a few years later) and a figure delivery by FedEx, the column debuted in GPS World, Volume 1, Issue 1, January/February 1990.

    It used three different positioning scenarios to explain how GPS could provide positioning accuracies from a Selective Availability-constrained 100 meters down to the sub-centimeter level. It also outlined GPS’s ability to determine platform attitude with multiple antennas and its use for accurate time transfer.
    There was a brief introductory couple of paragraphs, which would be a column standard (later extended to a sidebar). That first introduction went as follows:

    “‘Innovation’ will be a regular column in GPS World and will comment on GPS technology, product development, and other issues and needs of the GPS community. Coordinating editors are Alfred Kleusberg, Ph.D. and Richard Langley, Ph.D. both of the Department of Surveying Engineering at the University of New Brunswick in Fredericton, New Brunswick, Canada, as is David Wells, Ph.D., co-author of this initial column.

    “The first few columns will introduce GPS World readers to GPS technology. This first column focuses on the many capabilities of GPS. The next column will look at the flip side — what are the limitations of GPS? ‘Innovation’ will discuss some intriguing questions in future columns: Why is the GPS signal so complicated? How have surveyors been able to use it to get such accurate results? How serious is selective availability? We will also devote columns to exploring in depth some of the issues raised in this column: GPS and electronic charts, GPS and geographical information systems and prospects for using GPS and GLONASS together. We welcome readers’ comments and topic suggestions for future columns.”

    That introduction listed the topics for the first year of “Innovation.” They were written by Alfred, me, both of us, or other researchers at UNB and, in one case, by colleagues at the Canadian Hydrographic Service. We had a very positive response to our first few column articles, so Glen kept us on, but at some point in 1990, he told us the magazine was going to 10 issues a year. There were just too many GPS-related developments to be covered in just six issues. So now there would be a monthly column except for the July/August and November/December issues.

    In the second year, Alfred and I continued to write some tutorial articles for the column, but we started to invite others to submit articles, which we would then edit for style and space, and that became the tradition. Over the years, we have had hundreds of leaders in GNSS technology development and applications pen articles. In the second and third years of the column, for example, we featured articles by Stephen DeLoach on precise real-time dredge positioning, Jack Klobuchar on ionospheric effects on GPS, Edward Krakiwsky on GPS vehicle location and navigation, Yehuda Bock on continuous monitoring of crustal deformation, Keith D. McDonald on GPS in civil aviation, David Coco on GPS as satellites of opportunity for ionospheric monitoring, Derrick Peyton on using GPS and remotely-operated vehicles to map the ocean, Oscar Colombo and Mary Peters on precision long-range DGPS for airborne surveys, Adam Freedman on measuring the Earth’s rotation and orientation with GPS, Christian Rocken and Thomas Kelecy on high-accuracy GPS marine positioning for scientific applications, Marvin May on measuring velocity using GPS, Thomas Yunck describing a new chapter in precise orbit determination, and Gregory Leger on using GPS-equipped drift buoys for search and rescue operations. And the list goes on and on.

    As I mentioned, in the second year of GPS World, there were 10 issues. That changed in 1993, when the magazine went to 12 issues a year, but the September and December issues were “Showcase” issues featuring more industrial news and announcements of new products. It was also to include “The Almanac” — an update on the GNSS constellations, which I also looked after. Eventually, the “Showcase” issues became regular issues but with “Innovation” replaced by “The Almanac” at the “back of the book.”

    Figure 2A Different eras of “Innovation” throughout the years; the January 1993 edition (left) and the January 2000 edition (right). (Photo: GPS World archives)
    Figure 2A Different eras of “Innovation” throughout the years; the January 1993 edition (left) and the January 2000 edition (right). (Photo: GPS World archives)

    The column look changed a few times over the years, typically coinciding with magazine makeovers, with the logo changing from the original 3D terrain graphic to a logo of people with stuff in their hands starting in January 1999, to a “bits” logo from January 2001, to a somewhat plain format from September 2003, with the “Insights” sidebar and my photo from April 2006, to a circle photo from November 2015, and with a new photo from January 2016. FIGURES 2A, 2B and 2C show representative column snapshots for each era.

    Figure 2B Different eras of “Innovation” throughout the years; the January 2003 edition (left) and the September 2003 edition (right). (Photo: GPS World archives)
    Figure 2B Different eras of “Innovation” throughout the years; the January 2003 edition (left) and the September 2003 edition (right). (Photo: GPS World archives)

     

    FIGURE 2c  Different eras of “Innovation” throughout the years; the April 2006 edition (left) and the February 2016 edition (right). (Photo: GPS World archives)
    FIGURE 2c Different eras of “Innovation” throughout the years; the April 2006 edition (left) and the February 2016 edition (right). (Photo: GPS World archives)

    The tutorials

    As I mentioned earlier, right from the beginning of “Innovation,” we decided to have essentially two types of articles in the column: discussions of recent advances in GPS (and later GNSS) applications and related technology written by guest authors and tutorials explaining the fundamentals of GNSS including how the three main components of GNSS work: the satellites, the control segment and the user equipment. Here is a list of some of the tutorials written by the UNB team (mostly me) that were featured in “Innovation”:

    • GPS: A Multipurpose System (January/February 1990)
    • The Limitations of GPS (March/April 1990)
    • Why is the GPS Signal So Complex? (May/June 1990)
    • The Issue of Selective Availability (Sept./Oct. 1990)
    • Comparing GPS and GLONASS (Nov./Dec. 1990)
    • The GPS Receiver: An Introduction (Jan. 1991)
    • The Orbits of GPS Satellites (March 1991)
    • The Mathematics of GPS (July/August 1991)
    • Time, Clocks, and GPS (Nov./Dec. 1991)
    • Basic Geodesy for GPS (February 1992)
    • The Federal Radionavigation Plan (March 1992)
    • Precise Differential Positioning and Surveying (July 1992)
    • The GPS Observables (April 1993)
    • Communication Links for GPS (May 1993)
    • GPS and the Measurement of gravity (Oct. 1993)
    • RTCM SC-104 DGPS Standards (May 1994)
    • NMEA 0183: A GPS Receiver Interface Standard (July 1995)
    • Mathematics of Attitude Determination with GPS (Sept. 1995)
    • A GPS Glossary (Oct. 1995)
    • GPS and the Internet (Nov. 1995)
    • The GPS User’s Bookshelf (Jan. 1996)
    • Coordinates and Datums and Maps! Oh My! (with Will Featherstone; Jan. 1997)
    • The GPS Error Budget (March 1997)
    • GPS Receiver System Noise (June 1997)
    • GLONASS: Review and Update (July 1997)
    • The UTM Grid System (Feb. 1998)
    • A Primer on GPS Antennas (July 1998)
    • RTK GPS (September 1998)
    • The GPS End-of-Week Rollover (Nov. 1998)
    • The Integrity of GPS (March 1999)
    • Dilution of Precision (May 1999)
    • GPS, the Ionosphere, and the Solar Maximum (July 2000)
    • Navigation 101: Basic Navigation with a GPS Receiver (October 2000)
    • Getting Your Bearings: The Magnetic Compass and GPS (Sept. 2003)
    • GPS by the Numbers: A Sideways Look at How the Global Positioning System Works (April 2010); this was the 200th “Innovation” column.

    As you can see, the tutorials became fewer as the years went by. As my research career expanded, I just didn’t have the additional time to write more tutorials. I had taken over sole responsibility for the column in 1997, shortly after Alfred Kleusberg left UNB to pursue a career opportunity in Germany.

    However, the tutorial columns were (and still are) popular judging by the comments sent to GPS World and the number of citations for some reported by Google Scholar. For example, the one on dilution of precision has been cited in papers, theses, and reports 837 times to date. While not as many as a paper on an important medical breakthrough, it’s not a bad record for an article on a navigation topic.

    Changes at the top

    The column has seen four changes of editorial leadership at GPS World. Glen Gibbons, the founding editor, stepped down as editor-in-chief in July 2005 and shortly afterward started up his own publishing company to produce the magazine Inside GNSS. Alan Cameron took over the job in 2006, and subsequently became the magazine’s publisher and editor-at-large. Tracy Cozzens became the senior editor in 2019 with responsibility for “Innovation,” and then Matteo Luccio became editor-in-chief of the magazine in May 2021. I’m happy to say I got along well with all of these “bosses,” and they continued to put up with me even when I got the column in at the last moment. Additionally, the magazine’s various art directors over the years have always made the column look good.

    However, after I took over sole responsibility for the column, there were no changes at the bottom. So, I’ve ended up being the longest serving GNSS rapporteur or editor, with Glen and Alan and Tracy having retired at different epochs during the past decade. In addition to the column, I have contributed a number of shorter articles to the magazine and the GPS World website over the years, sometimes joined by colleagues from different organizations, in particular the German Aerospace Center.

    A bit of my own history

    I wasn’t going to bother with an “Insights” sidebar for this last column. The column isn’t about a single topic that needs any background information. But you might be wondering how I got this gig as the “Innovation” editor (apart from what I’ve already told you) or got my job at UNB for that matter. So, I’m repurposing the “Insights” sidebar from the February 2016 issue of GPS World, in which I talk a bit about antenna arrays and my own radio tinkering. It doesn’t mention that after getting my Ph.D., I spent two years at MIT as a postdoctoral fellow working under the famous physicist Irwin Shapiro on analyzing lunar laser ranging data to uncover subtle changes in Earth’s rotation due to the fluctuating winds of its atmosphere. Even as a graduate student, I was involved with satellite navigation and helped to uncover a bias in the coordinate system used by the U.S. Navy Navigation Satellite System, commonly known as Transit, by comparing station coordinates with those I obtained in my very long baseline interferometry research. I’ve always been a radio nerd both in my day job and as an avid shortwave radio hobbyist. So, it is not too surprising that I got involved with GPS and then GNSS (including ionospheric studies) and established a GNSS research group at UNB with some stellar graduates over the years.

    The archives

    I would like to report that all 300 “Innovation” columns are available for download on the Internet. Unfortunately, that is not the case — yet. Perhaps that’s something that could be done when I actually do retire. However, the first two years of the column are available here: gauss.gge.unb.ca/gpsworld/innovation.html. Hopefully, we can continue to keep that URL alive for a few years. If it should disappear, just Google it or consult the “Wayback Machine” at archive.org. The columns since June 2008 (with a few more before that) are available here. Full digital versions of each issue of the magazine since January 2009, including the “Innovation” column, are available here.

    The end

    And there you have it. It only remains for me to thank all of the authors who have shared their research and understanding of the many facets of GNSS in the column over the past three-and-a-half decades, the staff at GPS World for getting the column into the print and later the electronic editions on the Web, the readers whose positive feedback encouraged me to keep the column going, and to my wife, Marg, who let me spend the long hours on the column when I should have been attending to things around the house. So, now, to paraphrase a much better journalist than I: Goodbye, and good luck.


    The November 2024 issue of GPS World features Professor Richard Langley’s 300th and final “Innovation” column. His first one appeared in the January/February 1990 issue, the magazine’s very first. In celebration of Richard’s decades-long contribution to GPS / GNSS / PNT, we are publishing a selection of testimonials and photos from some of his colleagues and friends, gathered by his former students Sunil Bisnath and Attila Komjathy. Click here to read the testimonials.

  • Labsat shares results of Jammertest 2024

    Labsat shares results of Jammertest 2024

    Labsat has released updates from Jammertest 2024, where the team addressed real-world challenges related to GNSS jamming and spoofing attacks. According to Labsat, the team was on-site with the Labsat 4 GNSS Record & Replay device, which effectively captured the entire GNSS RF environment during the tests. The team shared that this technology has allowed Labsat to collect more than 20 TB of data, enabling them to reproduce complex signals under laboratory conditions.

    Labsat recorded GNSS signals at 12 bits of I&Q resolution across multiple frequency bands to accurately capture the RF conditions. With this data, LabSat 4 users can recreate these signals on their test benches, allowing them to evaluate their GNSS receiver performance against the same challenges encountered during the event.

    Labsat said it plans to make these recordings available to its LabSat 4 users, allowing them to experience a full range of jamming and spoofing scenarios firsthand. This offers GNSS engineers a unique chance to prepare their technology for real-world threats.

    Photo:
    Labsat 4 GNSS Record & Replay device. (Photo: Labsat)

  • Safran unveils GNSS/PNT simulator

    Safran unveils GNSS/PNT simulator

    Photo: Safran Navigation and Timing
    Photo: Safran Navigation and Timing

    Safran Navigation and Timing has unveiled its latest GNSS simulator, the Skydel GSG-8 Gen2, an evolution of its GSG-8 simulator. This new positioning, navigation and timing (PNT) test solution is part of Safran’s family of Skydel-based simulators.

    The GPU-based GSG-8 Gen2 simulator delivers high-end GNSS signal testing capabilities in a user-friendly, turnkey package. It seeks to support the growing demand for location-aware applications and systems requiring navigation or timing.

    It features six front-facing RF outputs and a combined output. It covers the entire GNSS bandwidth and offers a 1,000 Hz simulation iteration rate, high dynamics, real-time synchronization and simulation of all-in-view satellite signals.

    This simulator is ideal for development, NavWar testing and integration projects that require high performance, increased constellation and satellite visibility and multi-vehicle/multi-antenna scenarios. It allows users to generate RF signals that simulate real-world receiver device reactions under user-defined parameters. Users can control various simulation aspects, including receiver trajectories with six degrees of freedom (DoF), multipath signals, advanced jamming and spoofing and atmospheric interferences.

    The simulator can recreate various types of interference, both benign and malicious. Users can adjust power levels, interference signal types, spoofing signals, location, antenna patterns, and transmitter trajectories. In-band and out-of-band jamming signals can be generated without additional hardware.

    The GSG-8 Gen2 can simulate up to 2,000 GNSS signals simultaneously across multiple bands, leveraging GPU power to overcome the limitations of FPGA-based simulators. A single GSG-8 Gen2 can run and control multiple instances, each representing an independent trajectory, vehicle or antenna with its own output connector.

    As a low-Earth orbit (LEO) PNT signal simulator, the GSG-8 Gen2 can generate many signals required for LEO PNT simulations alongside legacy GNSS signals, threats and multipaths. It also supports S-Band signal generation.