Resources & FAQs

Thermal batteries are a class of primary reserve batteries ideal for applications demanding high power density, extremely long inert storage, and rapid activation within a single operational window. Unlike conventional batteries, they use a solid electrolyte that becomes ionically conductive only when heated by an internal pyrotechnic charge. This unique design grants them an inert shelf life often exceeding 20 years and robust operation across extreme temperature ranges once activated. For precision GNC components used in defense, aerospace, or specialized industrial systems like missiles, projectiles, or guided munitions, thermal batteries ensure that critical sensors—such as fiber optic gyroscopes, MEMS accelerometers, and associated processing units—receive stable, high-current power precisely when needed, enabling reliable navigation and control throughout the mission.

In safety-critical aircraft flight control systems, the reliability of GNC components is paramount. GNC Tech components, such as fiber optic gyroscopes and quartz accelerometers, contribute to fault tolerance through built-in redundancy and diverse integration strategies. This often involves employing multiple GNC sensor units, either identical (hot or cold standby) or dissimilar (e.g., FOGs alongside MEMS for cross-validation), to provide continuous, validated data. Advanced flight control systems utilize sophisticated algorithms to cross-check sensor outputs, detect discrepancies, and seamlessly switch to or fuse data from healthy components in the event of a primary sensor failure. This design philosophy ensures that a single component malfunction does not compromise the aircraft's stability or navigation, upholding the highest standards of safety and operational continuity.

Thermal runaway in precision GNC components signifies a critical positive feedback loop where increased temperature leads to further heating, potentially causing irreversible damage or catastrophic failure. For components like fiber optic gyroscopes (FOGs), MEMS sensors, or quartz accelerometers, maintaining stable operating temperatures is paramount for consistent precision. Prevention strategies involve meticulous thermal design, including optimized heat dissipation pathways, efficient heat sinks, and robust power management to prevent localized hotspots. Active temperature control systems may also be employed to keep sensitive elements within their optimal thermal envelope. Failure to manage thermal risks can result in degraded sensor accuracy, increased drift, or complete component failure, severely compromising the reliability and performance of any control system relying on their output for accurate guidance and navigation.

Precision GNC control systems, especially in mission-critical applications, demand power sources that can activate rapidly and deliver stable, high-quality power. Thermal batteries excel here because they are inert until needed, then activate in milliseconds to provide full power. Their electrochemistry ensures a consistent discharge voltage and current, minimizing power fluctuations that could compromise the accuracy or stability of sensitive FOGs, MEMS sensors, or accelerometers. This combination of swift readiness and stable electrical output is vital for reliable system initialization and maintaining closed-loop control performance throughout the operational phase, particularly in single-use scenarios where re-powering or variable power delivery is not an option.

Many modern high-performance aerial vehicles, designed for maximum maneuverability or reduced aerodynamic drag, possess inherent static or dynamic instability. Without active intervention, such platforms would be difficult or impossible to control effectively. A Stability Augmentation System (SAS) leverages precision GNC components like fiber optic gyroscopes (FOGs) and MEMS accelerometers to detect even subtle angular rates and accelerations. This high-fidelity sensory feedback is processed by a dedicated control loop that commands actuators to apply corrective forces, effectively increasing the vehicle's damping and improving its short-period stability. GNC Tech's high-bandwidth, low-noise sensors are critical for providing the real-time, accurate motion data necessary for these systems to operate effectively, transforming an otherwise uncontrollable design into a stable and precise platform.

Quadrant detectors are crucial for achieving the sub-arcsecond precision required in advanced optical guidance and laser tracking systems. By converting the spatial position of a light spot into electrical signals, they provide real-time, differential feedback on a laser beam's deviation from a desired target. This precise positional error signal allows GNC components, such as fast steering mirrors or gimbals, to continuously correct the beam's trajectory. This closed-loop feedback mechanism ensures exceptional pointing accuracy and dynamic stability, even in environments with vibrations or platform motion. This capability is vital for applications ranging from free-space optical communication to target designation and active beam stabilization.

Target tracking systems rely heavily on a stable measurement platform to accurately acquire, follow, and predict the movement of targets. GNC Tech's fiber optic gyroscopes (FOGs), MEMS sensors, and quartz accelerometers deliver the high-bandwidth, low-noise angular rate and acceleration data essential for precision platform stabilization. By continuously providing exact ego-motion information, these components enable control systems to counteract disturbances, vibration, and vehicle motion. This stability ensures that optical, radar, or IR tracking sensors mounted on the platform can obtain clean, undistorted measurements, significantly enhancing the accuracy and robustness of the target tracking algorithms, especially for long-range or high-dynamic targets.

In beam riding guidance, the munition must continuously sense its position relative to a precisely directed beam, which can be radar or laser. GNC Tech's precision components are essential for this closed-loop control. Fiber optic gyroscopes (FOGs) and MEMS gyroscopes provide highly accurate angular rate information, crucial for determining the munition's orientation and how it deviates from the beam's central axis. Quartz accelerometers measure linear accelerations, complementing gyroscope data to track the munition's translational movement. The integrated guidance system uses these precise inertial inputs, combined with signals from specialized beam detection sensors, to calculate real-time flight path corrections, ensuring the munition stays accurately centered on the beam towards its intended target.

Proportional Navigation (PN) is a widely adopted guidance law where an interceptor's turn rate is directly proportional to the rotation rate of the line-of-sight (LOS) to the target. To effectively implement PN, guidance systems require highly accurate, low-noise angular rate measurements to determine the LOS rate. GNC Tech's precision fiber optic gyroscopes (FOGs) and advanced MEMS gyroscopes provide the stability and accuracy needed for this. These sensors continuously measure the interceptor's own angular motion, which, when combined with seeker data, allows for real-time calculation of the LOS rate. This precise data ensures the guidance system can command the appropriate maneuver for an accurate intercept, especially critical in dynamic, high-speed scenarios where even small errors accumulate rapidly.

For high-precision navigation and control, the choice between FOG-based and MEMS-based Inertial Measurement Units (IMUs) hinges on accuracy requirements, drift stability, and operational environment. FOG-based IMUs, utilizing fiber optic gyroscopes, excel in applications demanding extremely low drift rates and high angular rate accuracy over extended periods, making them indispensable for strategic-grade navigation, aerospace platforms, and critical autonomous systems. Their performance is less susceptible to temperature fluctuations and vibration. Conversely, MEMS-based IMUs offer significant advantages in size, weight, power (SWaP), and cost. While their inherent drift and noise characteristics are generally higher than FOGs, advancements in MEMS technology make them suitable for tactical-grade applications, robotics, and commercial UAVs where a balance of performance and budget is crucial. GNC Tech offers both technologies to meet diverse precision GNC requirements.

In integrated navigation systems, a precision Inertial Measurement Unit (IMU) featuring high-performance fiber optic gyroscopes and quartz accelerometers is crucial for achieving robust and continuous positioning, even in challenging environments. While Global Navigation Satellite Systems (GNSS) provide absolute position fixes, they are susceptible to signal loss in urban canyons, under dense foliage, or during jamming. The IMU autonomously tracks motion, providing continuous, high-rate attitude, velocity, and relative position data. When GNSS signals are present, the IMU data is continuously corrected and refined through sensor fusion algorithms, such as Kalman filters, significantly improving overall accuracy and robustness. During GNSS outages, the IMU "coasts" – maintaining navigation estimates based on its own measurements, thus providing a critical bridge until external aiding is restored. This synergistic approach ensures uninterrupted, high-fidelity navigation for demanding applications.

The performance of an Inertial Navigation System (INS) is fundamentally tied to the precision of its Inertial Measurement Unit (IMU) components. Key inherent characteristics contributing to long-term drift and accuracy degradation include: * **Gyroscope Bias and Noise:** Gyroscopes measure angular rate. Any constant or slowly varying error (bias) in this measurement, even minute, leads to accumulating angular position error over time. Noise further degrades the integration. * **Accelerometer Bias, Scale Factor, and Noise:** Accelerometers measure linear acceleration. Biases affect the perceived gravity vector, impacting attitude and position calculations. Scale factor errors distort the magnitude of acceleration, directly affecting velocity and position. * **Sensor Stability over Temperature and Time:** The consistency of these characteristics across varying temperatures and over operational lifespans is critical. High-precision components like GNC Tech's FOGs, MEMS, and quartz accelerometers are designed to exhibit superior bias stability and low noise, minimizing the accumulation of errors. This foundational precision is crucial for applications requiring high accuracy, especially during extended GPS-denied or degraded periods where INS must operate autonomously.

In embedded GPS/INS systems, the coupling architecture defines how the GPS receiver and Inertial Navigation System (INS) interact. A **loosely coupled** system processes GPS data separately to obtain position and velocity, which are then fed into the INS filter. While simpler to implement, it's less robust, especially in GPS-challenged environments, as it requires a valid GPS fix to aid the INS. Conversely, a **tightly coupled** system merges the raw GPS measurements (pseudorange, pseudorange rate) directly with the INS data within a single Kalman filter. This advanced approach allows the INS to aid the GPS receiver in tracking satellites, improving signal acquisition and reacquisition, and significantly extending navigation capabilities during GPS outages or in environments with limited satellite visibility (e.g., urban canyons, heavy foliage). This provides superior accuracy, integrity, and operational robustness, crucial for high-precision GNC applications.

A precision Inertial Measurement Unit (IMU) is comprised of a minimum of three gyroscopes and three accelerometers, strategically arranged to measure motion across all three spatial axes (X, Y, Z). The gyroscopes measure angular velocity, providing critical data for determining an object's real-time attitude and orientation changes. Simultaneously, the accelerometers detect linear acceleration, which is integrated to derive velocity and ultimately position. Together, these six independent sensor outputs (three angular rates and three linear accelerations) allow for the precise determination of an object's 6-degrees-of-freedom (6-DoF) motion relative to an inertial frame. GNC Tech utilizes high-performance fiber optic gyroscopes, MEMS sensors, and quartz accelerometers to provide the robust, accurate data necessary for demanding precision guidance and navigation applications where reliability and low noise are paramount.

High vibration and shock are critical environmental factors that can significantly degrade the performance of an Inertial Measurement Unit by introducing noise, bias shifts, and even physical damage. GNC Tech's precision IMUs are engineered to address these challenges through a combination of robust mechanical design, advanced sensor technology, and sophisticated signal processing. Mechanically, they feature ruggedized housing, specialized damping materials, and optimized sensor mounting to effectively isolate sensitive components from external forces. By integrating inherently robust sensor technologies such as fiber optic gyroscopes (FOGs) and quartz accelerometers, GNC Tech's IMUs offer superior resilience against mechanical stress and reduce susceptibility to vibration rectification errors. Furthermore, specialized filtering algorithms are applied to raw sensor data, enabling the intelligent distinction between actual motion and environmentally induced noise, ensuring sustained high-accuracy attitude and velocity data in the most demanding dynamic conditions.

A 6-axis IMU, comprising three-axis gyroscopes and three-axis accelerometers, measures angular velocity and linear acceleration. While 9-axis IMUs incorporate magnetometers to provide an absolute heading reference, these sensors are highly susceptible to disturbances from ferrous materials, electrical currents, and localized magnetic field variations found in many operational environments. In precision GNC applications such as indoor robotics, autonomous underwater vehicles (AUVs), spacecraft operating near metallic structures, or within industrial settings, these magnetic disturbances can render magnetometer data unreliable or even detrimental to navigation accuracy. In such cases, a 6-axis IMU is often preferred. Its data is integrated, typically with advanced estimation algorithms like an Extended Kalman Filter, to maintain attitude and dead reckoning, relying on the IMU's inherent drift characteristics rather than corrupt external magnetic references. This choice prioritizes consistent, albeit drifting, attitude information over potentially erratic absolute heading data.

A 9-axis IMU integrates a 3-axis accelerometer, a 3-axis gyroscope, and a 3-axis magnetometer. While accelerometers provide gravity-referenced pitch and roll, and gyroscopes measure angular rates, gyroscopes are susceptible to drift over time, particularly in the yaw axis. The magnetometer's ability to sense the Earth's magnetic field offers an independent, absolute heading reference. By fusing this magnetic data with the gyro and accelerometer inputs, a 9-axis IMU can effectively compensate for gyro drift in yaw, providing a more stable and accurate attitude and heading reference system (AHRS). This capability is critical for precision GNC applications requiring prolonged, accurate orientation tracking, especially in environments where satellite navigation signals may be compromised or unavailable, ensuring reliable platform stabilization, guidance, and control.

A purely inertial guidance system operates autonomously, relying solely on its internal accelerometers and gyroscopes to continuously calculate position, velocity, and orientation from an initial known state. This self-contained nature makes it indispensable in environments where external navigation aids, such as GPS, are unavailable, unreliable, or compromised. Key scenarios include GPS-denied or jammed combat zones, subterranean or underwater operations where signals cannot penetrate, and deep-space missions. Its primary advantages are immunity to external interference, jamming, and spoofing, providing uninterrupted navigation. While pure inertial systems accumulate drift over time, GNC Tech's high-precision FOGs, MEMS sensors, and quartz accelerometers are designed to minimize this, enabling reliable performance for critical missions where absolute autonomy and resistance to external disruption are paramount.

A precision Inertial Navigation System (INS) operates by continuously integrating raw angular rate (from gyroscopes) and specific force (from accelerometers) measurements provided by its Inertial Measurement Unit (IMU). The core computational cycle involves three primary steps, iterated at high frequencies (e.g., hundreds to thousands of Hz): 1. **Attitude Update:** Gyroscope data is integrated to update the system's orientation (attitude) in space, typically using quaternion-based algorithms for robust numerical stability. 2. **Velocity Update:** The specific force measured by accelerometers, once rotated into the navigation frame using the updated attitude, is integrated to determine the system's velocity, accounting for local gravity and Coriolis effects. 3. **Position Update:** The calculated velocity is then integrated to derive the system's current position. This iterative process provides autonomous, real-time navigation states. To manage inherent drift and achieve higher long-term accuracy, precision INS often incorporate Kalman filters or similar optimal estimation techniques to fuse IMU data with external aiding sensors like GPS or magnetometers.

Achieving robust autonomous navigation for unmanned systems in diverse environments presents significant challenges, including maintaining accuracy in GNSS-denied or spoofed conditions, mitigating drift over extended missions, and ensuring reliable operation despite vibration, shock, or temperature variations. Precision GNC components, such as high-performance FOGs, MEMS IMUs, and quartz accelerometers, are critical. They provide accurate, low-drift inertial data for continuous dead reckoning, which is essential when GNSS signals are unavailable. Furthermore, their high-bandwidth and low-noise characteristics enable precise control for dynamic maneuvers, while robust designs ensure performance in harsh operational settings, thereby enhancing overall system reliability and mission success.

In closed-loop fiber optic gyroscopes, the multifunction integrated optical chip's (MIOC) polarization extinction ratio (PER) is critical for achieving high bias stability. A high PER ensures that only the desired polarization mode propagates through the interferometer, effectively minimizing spurious signals and reducing errors that can manifest as bias drift. This directly contributes to a stable and precise angular rate measurement. While MIOCs with a chip polarization extinction ratio of ≥55 dB are suitable for many demanding applications, ultra-high extinction ratios of ≥80 dB are essential for achieving the lowest possible bias drift in the most demanding precision FOG designs. These higher specifications are particularly vital for FOGs requiring superior long-term navigation accuracy. For less sensitive systems, a standard extinction ratio may be sufficient. GNC Tech supplies various MIOCs to meet these requirements.