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Supplier: Northrop Grumman Corporation
Description: The LTN-101 FLAGSHIP™ is an integrated global navigation, air data, inertial reference unit (GNADIRU). Introduced in 1992, FLAGSHIP™ has established an exceptional reliability record of over 16,000 operating hours MTBF on such leading commercial aircraft as the Airbus wide and
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Supplier: Exail
Description: PHINS is an inertial navigation system providing position, true heading, attitude, speed, depth and heave. Its high accuracy inertial measurement unit is based on iXBlue's fiber-optic gyroscope technology coupled with an embedded digital signal processor that runs an
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Supplier: Exail
Description: PHINS 6000 is a subsea inertial navigation system (INS) providing position, true heading, attitude, speed, depth, and heave for deep water operations. Its high-accuracy inertial measurement unit is coupled with an embedded digital signal processor that runs an advanced
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Supplier: Exail
Description: AIRINS, engineered for optimal integration and ease-of use, utilizes iXBlue's expertise in fiber-optic gyroscopes (FOG), already in use in satellite control. AIRINS combines the latest motion sensing technology, electronics and embedded processing design in one single unit. This offers the
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Supplier: SBG Systems SAS
Description: grams) includes a MEMS-based Inertial Measurement Unit (IMU) and runs an enhanced Extended Kalman Filter (EKF) which fuses inertial and aiding information to provide accurate real time orientation and navigation data. High Accuracy for Such a Small Sensor: 0.1° Roll and
- Angular Rate Range: 450 to 1,000.000000000002 deg/sec
- Bandwidth: 133 Hz
- Linear Acceleration Range: 8 to 16 g
- Accuracy: 0.2 ±% Full Scale
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Supplier: SBG Systems SAS
Description: Ekinox-U is an ITAR Free Underwater Inertial Navigation System. Designed for Subsea applications, Ekinox-U is operational up to 6,000 m. It combines an Inertial Measurement Unit (IMU), runs an enhanced on-board Extended Kalman Filter (EKF), and can be connected to several
- Linear Acceleration Range: 2 g
- Maximum Dimension: 6.1 inch
- Weight: 5.2 lbs
- Operating Temperature: -4 to 140 F
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Supplier: LORD MicroStrain Sensing Systems
Description: The 3DM-GX4-45™ is a miniature, industrial-grade GPS Aided Inertial Navigation System (GPS/INS), utilizing the highest performance MEMS sensor technology. It combines a triaxial accelerometer, triaxial gyro, triaxial magnetometer, temperature sensors, pressure altimeter, and dual
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Supplier: LORD MicroStrain Sensing Systems
Description: The LORD Sensing 3DM-GX5® family of industrial grade inertial sensors provides a wide range of triaxial inertial measurements and computed attitude and navigation solutions. The 3DM-GX5-45 all-in-one navigation solution features a high performance integrated
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Supplier: SBG Systems SAS
Description: Ellipse-N is a small-sized high performance Inertial Navigation System (INS) with integrated GNSS receiver. It provides Roll, Pitch, Heading, Heave, and Navigation data. This light-weight sensor includes a MEMS-based Inertial Measurement Unit (IMU) integrating
- Angular Rate Range: 450 to 1,000.000000000002 deg/sec
- Bandwidth: 133 Hz
- Linear Acceleration Range: 8 to 16 g
- Accuracy: 0.2 ±% Full Scale
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Supplier: Memsense, LLC
Description: The MS-IMU3020 is a miniature low drift inertial measurement unit (IMU) that delivers market leading price and performance. The IMU contains triaxial gyros, accelerometers and magnetometers that are extensively tested and calibrated over the full operational temperature range to ensure
- TJ: -40 to 85 C
- Features: Other
- Technology: RS422, USB
- Device Type: Transmitter
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Supplier: SBG Systems SAS
Description: Ellipse-D is a compact Inertial Navigation System with integrated Dual-antenna GNSS receiver for accurate Heading. It provides Roll, Pitch, Heading, Heave, and Navigation data. Ellipse-D includes a MEMS-based Inertial Measurement Unit (IMU) and runs an enhanced
- Angular Rate Range: 450 to 1,000.000000000002 deg/sec
- Bandwidth: 133 Hz
- Linear Acceleration Range: 8 to 16 g
- Accuracy: 0.2 ±% Full Scale
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Supplier: Exail
Description: ASTRIX is made of four independant closed loop FOG 120 gyrosope channels offering one redundancy and a failure direction capability. Moreover, this configuration improves the nominal performances by using four channels ON at the beginning of the mission, then three ON after one failure.
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Supplier: Shenzhen Rion Technology Co., Ltd
Description: The AH/VG610B is a high reliable, vibration-rejecting solid state inertial measuring unit. It consists of three vibrating ring gyroscopes and three internal damping accelerometers mounted orthogonally in each axis of space. Each device is factory calibrated over the working temperature
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Supplier: LORD MicroStrain Sensing Systems
Description: Overview The 3DM-GX3® -15-OEM is a high-performance, miniature Inertial Measurement Unit and Vertical Gyro, utilizing MEMS sensor technology. It combines a triaxial accelerometer, triaxial gyro, temperature sensors, and an on-board processor running a sophisticated sensor fusion
- Angular Rate Range: 49.999999999999986 to 1,200 deg/sec
- Bandwidth: 440 Hz
- Linear Acceleration Range: -50 to 50 g
- Maximum Dimension: 1.4960638 inch
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Supplier: LORD MicroStrain Sensing Systems
Description: estimatesImproved position outputs with concurrent tracking of up to two GNSS constellations (GPS/QZSS, GLONASS, BeiDou... )The LORD MicroStrain® 3DM-GQ4-45™ tactical grade inertial sensor provides a wide range of triaxial inertial measurements and computed attitude and
- Angular Rate Range: 300 deg/sec
- Bandwidth: 160 Hz
- Maximum Dimension: 3.1102379 inch
- Weight: 0.231481481481481 lbs
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Supplier: Honeywell Sensing & IoT
Description: The Honeywell 6-D Motion Variant 6DF (six degrees of freedom) Inertial Measurement Unit (IMU) sensors are designed to provide motion, position, and navigational sensing from a durable single device over six degrees of freedom. This is achieved by using MEMS (microelectromechanical
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Supplier: Honeywell Sensing & IoT
Description: The Honeywell 6-D Motion Variant 6DF (six degrees of freedom) Inertial Measurement Unit (IMU) sensors are designed to provide motion, position, and navigational sensing from a durable single device over six degrees of freedom. This is achieved by using MEMS (microelectromechanical
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Supplier: Shenzhen Rion Technology Co., Ltd
Description: GI550 MEMS IMU is a tactical-level inertial and integrated navigation system built by the company, which is calibrated precisely in full temperature range to meet the performance requirements under different conditions. The data fusion is realized by the built-in navigation
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Supplier: Xsens Technologies BV
Description: system. With the Development Kit you have will have your measurement unit up and running in just a few minutes to start your first R&D. Highlights 3 products: MTi-10 IMU, MTi-20 VRU and MTi-30 AHRS MTi-10 IMU: inertial dynamic data (rate of turn/acc or delta_q/delta_vel) and magnetic
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Supplier: Northrop Grumman Corporation
Description: The Northrop Grumman LN-260 is a flight qualified operational form and fit replacement Inertial Navigation System/Global Positioning System (INS/GPS) that can be incorporated with numerous international and domestic Standard Navigation Unit platforms. In the news:
- Operating Temperature: -40 to 159.8 F
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Supplier: Northrop Grumman Corporation
Description: The LN-251 Inertial Navigation System/Global Positioning System (INS/GPS) is the smallest, lightest, lower power, and most reliable navigator with unsurpassed geo-location and velocity accuracy in its class. The LN-251 is a fully integrated, non-dithered navigation system with
- Angular Rate Range: 1,000.000000000002 deg/sec
- Linear Acceleration Range: 28 g
- Operating Temperature: -65.2 to 159.8 F
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Supplier: Northrop Grumman Corporation
Description: can be installed in place of older systems with virtually no aircraft modifications. The LN-100R is designed as a "Form, Fit, and Function" replacement for the commercial ARINC 561 inertial navigation systems. The unit is a specially packaged version of the highly successful
- Angular Rate Range: 400.0000000000002 deg/sec
- Linear Acceleration Range: 16 g
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Supplier: Imego
Description: consists of a small IMU (InertialMeasurement Unit), a communication unit (that also can store data), andPC software (for calculations and data display). The navigated datainclude position/velocity/acceleration and attitude/angularrate/angular acceleration. The time signal can be
- Angular Rate Range: 0 to 6,000 deg/sec
- Bandwidth: 1,000 Hz
- Linear Acceleration Range: -500 to 500 g
- Maximum Dimension: 1.28 inch
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Supplier: Gladiator Technologies, Inc.
Description: The unit is highly durable and can withstand environmental vibration and shock typically associated with commercial stabilization and aerospace requirements. The MEMS G300D gyro is offered at 100°/s or 300°/s rate range. The unit is temperature compensated for bias and offers
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Supplier: Savant Automation, Inc.
Description: 7,000 Pounds Standard Capacity Virtual Path™ 'Tape-free/Target-free' Navigation
- Load Capacity: 7,000 lbs
- Travel Speed: 200 ft/min
- Load Transfer: Automatic
- Features: Conveyor Coupling, Remote Control
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Supplier: AGVE AB
Description: AGVE offers a unique range of automated guided vehicles (AGVs), ranging from standard models to over 100 tailor-made vehicles. Models use a wide range of navigation technologies such as laser/vision/ contour/wire/magnet . AGVE provide the highest quality automated guided vehicles for the most
- Load Capacity: 3,307.5 lbs
- Lift Height: 26.246733333333335 ft
- AGV Type: Forklift AGV, Tugger AGV, Unit Load AGV
- Guidance Type: Inertially Guided, Laser Guided, Wire Guided
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Supplier: Tronics Microsystems
Description: repeatability of 1 mg, all within a significantly reduced Size, Weight, and Power (SWaP) footprint. Its superior bias instability of 3 µg makes it the ideal choice for demanding applications including high-performance Inertial Measurement Units (IMUs), GNSS-fused Inertial
- Acceleration: 5 g
- Frequency Range: 120 Hz
- Maximum Shock: 50 g
- Maximum Vibration: 4.12 g
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Supplier: Tronics Microsystems
Description: significantly smaller, lighter, and more power-efficient package. Key features include an industry-leading 1 mg 1-year composite bias repeatability and a minimal 20 µg/g² Vibration Rectification Error (VRE), making AXO314 ideal for high-performance Inertial Measurement Units (IMUs) and
- Acceleration: 14 g
- Frequency Range: 300 Hz
- Maximum Shock: 50 g
- Maximum Vibration: 4.12 g
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Supplier: AGVE AB
Description: types of navigation available No limitations in design
- Load Capacity: 130,000 lbs
- Lift Height: 32.808416666666666 ft
- AGV Type: Forklift AGV, Tugger AGV, Unit Load AGV
- Guidance Type: Inertially Guided, Laser Guided, Wire Guided
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Supplier: Savant Automation, Inc.
Description: accurate, navigation system employing a solid state inertial sensor chip to compare AGV heading and positional data to a virtual route CAD map in the vehicle’s memory. It is ideal for all environments, especially where damage vulnerable magnetic/optic floor tape, floor cut slots or
- Load Capacity: 25,000 lbs
- Travel Speed: 200 ft/min
- Load Transfer: Automatic, Manual
- Guidance Type: Inertially Guided
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Description: This specification defines the requirements for a two-degree-of-freedom dynamically tuned gyro to be used as a sensor in a strapdown, gimballed inertial navigation system (attitude reference units) for use in an aircraft, a missile, a spacecraft or similar applications. The
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Supplier: Xsens Technologies BV
Description: system. With the Development Kit you have will have your measurement unit up and running in just a few minutes to start your first R&D. Highlights 3 products: MTi-10 IMU, MTi-20 VRU and MTi-30 AHRS MTi-10 IMU: inertial dynamic data (rate of turn/acc or delta_q/delta_vel) and magnetic
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Supplier: Tronics Microsystems
Description: Bill of Materials (BOM) costs. An integrated self-test function provides continuous assurance of sensor integrity and operational functionality.Applications:•GNSS-Assisted Navigation: Ideal for ground vehicles, trains, and other dynamic platforms requiring precise positioning.•Motion Control
- Angular Rate Range: 300 deg/sec
- Linearity: 60 ±% Full Scale
- Bandwidth: 200 Hz
- Bias Stability: 0.4 deg/hr
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Supplier: Linde North America, Inc.
Description: guidance, navigation and control systems. The Ring Laser Gyros (RLG) can be used as the stable elements (for one degree of freedom each) in an inertial guidance system. The advantage of using a RLG is that there are no moving parts. Compared to the conventional spinning gyro, this
- Concentration: 99.99 %
- Product Form: Gas
- Supply Options: Gas Cylinder
- Industrial Gases: Neon
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Supplier: Shenzhen Rion Technology Co., Ltd
Description: TL766D is RION company newly developed three axis angle instrument based on latest MEMS inertial measurement platform , it can simultaneously output Moving carrier’s horizontal angle, vertical angle and horizontal azimuth. The internal integration of the triaxial accelerometer and triaxial
- Angular Rate Range: 300 deg/sec
- Weight: 1.25661375661376 lbs
- Operating Temperature: -40 to 85 F
- Output Options: Pulse / Frequency
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packaging, and proven manufacturing expertise to deliver custom inertial MEMS with tunable Q-factors. Ideal for navigation-grade systems, our foundry service supports scalable production with over 1 million units delivered. Learn more about Inertial MEMS Foundry. (read more)
Browse MEMS Foundry Datasheets for Tronics Microsystems -
GYPRO®4300 is a high stability MEMS gyro tailored to GNSS-assisted inertial navigation and positioning of ground vehicles and trains, MRU (Motion Control Unit) for ship motion control and positioning, as well as AHRS for small aircrafts, helicopters, and drones, but (read more)
Browse Gyroscopes Datasheets for Tronics Microsystems -
. Its bias Instability of 4 μg and bias over temperature of ±0.5 mg enable precise GNSS-aided navigation of manned and unmanned ground vehicles when integrated into an Inertial Navigation System (INS). In subsea environments where satellite-based positioning is not available (read more)
Browse Accelerometers Datasheets for Tronics Microsystems -
Engineers designing industrial control and autonomous systems often struggle with accurate motion tracking, high vibration environments, and GPS-denied conditions. Inconsistent inertial data can degrade system (read more)
Browse Inertial Measurement Units (IMU) Datasheets for Win Source Electronics -
Build compact and high-performance inertial systems with GYPRO4300, a tactical grade ± 300 °/s MEMS rate gyro able to demonstrate high stability and low drift for precise attitude determination, positioning and navigation in harsh (read more)
Browse Gyroscopes Datasheets for Tronics Microsystems -
-performance IMU (Inertial Measurement Units) and INS (Inertial Navigation Systems). Click here to learn more and contact us about your next marine or subsea project. (read more)
Browse Accelerometers Datasheets for Tronics Microsystems -
features advanced etching and tunable Q-factor processes, enabling best-in-class inertial navigation performance. With over 1 million units produced, our foundry service ensures reliability, scalability, and precision. Explore the Accelero MEMS Foundry. (read more)
Browse MEMS Foundry Datasheets for Tronics Microsystems -
While compass was the first navigation instrument used by sailors to keep their course, today’s vessels, subsea vehicles and AUV (Autonomous Underwater Vehicles) are equipped with IMU (Inertial Measurement Units) or MRU (Motion Reference Unit) for high (read more)
Browse Datasheets for Tronics Microsystems -
integration into INS (Inertial Navigation Systems), IMU (Inertial Measurement Units) as well as AHRS (Attitude and Heading Reference Systems). To minimize mechanical cross-coupling in multi-axis applications, GYPRO4300 is available in 3 frequency ranges (read more)
Browse Gyroscopes Datasheets for Tronics Microsystems -
μg with a ±0.5 mg bias over its temperature range, thus enabling precise GNSS-aided navigation of manned and unmanned ground vehicles and trains when integrated into Inertial Navigation System (INS). AXO305 is a perfect candidate for Motion Reference Units (MRU) used (read more)
Browse Accelerometers Datasheets for Tronics Microsystems
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The Role of Inertial Measurement Unit (IMU) in 3D Time-of-Flight Cameras
An Inertial Measurement Unit (IMU) detects movements and rotations across six degrees of freedom, representing the types of motion a system can experience. When paired with ToF cameras, it ensures accurate spatial understanding and enhances robotic navigation systems. Get expert insights into how
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INS600 RTK INTEGRATED NAVIGATION SYSTEM
? INTRODUCTION The INS600 series is a dual-antenna GPS/INS integrated navigation system built by RION. The dual-antenna differential positioning measurement unit (IMU) is precisely calibrated in the full temperature to meet the performance requirements in different environments. The multi-data
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https://uwspace.uwaterloo.ca/bitstream/handle/10012/2991/thesis.pdf?sequence=1
5 Inertial Navigation Unit (INU .
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Geolocation Techniques
222 8.2.2 Inertial Navigation Unit (INU) Orientation Estimation. . .
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Industrial Instrumentation and Control Systems II
Initial calibration and alignment of low cost inertial navigation units for land vehicle applications Journal of Robotics Systems, 16 (2) (1999), pp. 81–92 .
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Avionics Navigation Systems 2nd Edition Complete Document
I shows typical characteristics of a strapdown inertial navigation unit .
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http://dspace.mit.edu/bitstream/handle/1721.1/71860/16-358j-spring-2005/contents/assignments/titan_1999_rpt.pdf
• The lack of focus and understanding of Inertial Measurement System software operations and Inertial Navigation Unit testing contributes to the poorly defined process for generation and test of the I1 rate filter constants.
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Aided Inertial LAnd NAvigation system (ILANA) with a minimum set of inertial sensors
Depending on the required system performance a GPS receiver can either be mounted externally or integrated within the Inertial Navigation Unit .
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Advanced Materials and Technologies for Micro/Nano-Devices, Sensors and Actuators
One example is related to Inertial Measurement Unit (IMU) or Inertial Navigation Unit (INU) where accelerometer and gyroscopes are each other comple- mentary to detect linear and angular motion in several applications including image stabilization, enhanced user interface for mobile phones, games …
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Laser Scanning for the Environmental Sciences
Position for any x,y,z point on the Earth’s surface is generated from three sources: (i) the LiDAR sensor, (ii) the Inertial Navigation Unit (INU) of the aircraft and (iii) GPS.
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Military Avionics Systems
Accordingly, mainly advanced EO packages have a dedicated strapdown inertial navigation unit (INU) directly fitted on to the head assembly to improve pointing and positional accuracy and reduce data latency.
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