Inertial Navigation Systems

Description: ROVINS is a survey-grade full featured inertial navigation system for water depths up to 3 000 m. Designed specifically for offshore survey and construction works, ROVINS, thanks to its advanced Kalman filter, improves the efficiency of all operations where accurate position,

• Angular Rate Range: 750 deg/sec
• Device Type: Optical
• Electrical Output: Pulse / Frequency, Serial / Digital
• Linear Acceleration Measurement: Fiber Optic

Description: ROVINS NANO merges the established high-grade iXBlue inertial navigation system with our competitive IMU. It is built on iXBlue's renowned FOG truly solid state technology and offshore instrumentation expertise. ROVINS NANO offers the unbeatable stability and accuracy of the

• Angular Rate Range: 250 deg/sec
• Device Type: Optical
• Electrical Output: Pulse / Frequency, Serial / Digital
• Linear Acceleration Measurement: Fiber Optic

Description: Ellipse-E is a small-sized high performance Inertial Navigation System. It provides Roll, Pitch, Heading, and Heave, and computes Navigation data when connected to an external GPS. It accepts Odometer aiding to maintain the best accuracy in challenging environments. This

• Accuracy: 0.2000 ±% Full Scale
• Angular Rate Range: 450 to 1000 deg/sec
• Bandwidth: 250 Hz
• Electrical Output: Serial / Digital, Network / Fieldbus Output

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

• Angular Rate Range: 750 deg/sec
• Device Type: Optical
• Electrical Output: Pulse / Frequency, Serial / Digital
• Features: GPS Aided

Description: The LN-120G is a Stellar-Inertial-GPS navigation system that provides precise navigation and sensor pointing with or without GPS. This system integrates stellar tracking and SAASM (Selective Availability Anti-Spoofing Module)-based GPS with a Zero-Lock™ Gyro

Description: ADVANS LYRA is an inertial navigation system which provides a continuous, instant-on position and orientation for tactical vehicles, observation and weapon turrets, radars, missile alignment, mortars and artillery launchers. ADVANS LYRA is accurate (1 mil), robust to GPS drop

• Angular Rate Range: 200 deg/sec
• Device Type: Optical
• Electrical Output: Serial / Digital
• Features: GPS Aided

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

• Accuracy: 0.2000 ±% Full Scale
• Angular Rate Range: 450 to 1000 deg/sec
• Bandwidth: 250 Hz
• Electrical Output: Serial / Digital, Network / Fieldbus Output

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

• Accuracy: 0.2000 ±% Full Scale
• Angular Rate Range: 450 to 1000 deg/sec
• Bandwidth: 250 Hz
• Electrical Output: Serial / Digital, Network / Fieldbus Output

Description: Apogee-N is a highly accurate Inertial Navigation System with embedded GNSS receiver for real-time and post-processing operations. The ITAR Free Apogee-N is the most accurate INS/GNSS based on the robust and cost-effective MEMS technology. High Accuracy

• Angular Rate Range: 100 deg/sec
• Electrical Output: Serial / Digital, Network / Fieldbus Output
• Features: Data Recorder, GPS Aided
• Linear Acceleration Measurement: MEMS

Description: algorithm produces highly accurate computed outputs under dynamic conditions. Computed outputs include pitch, roll, yaw, heading, position, velocity, and GNSS outputs- making it a complete GNSS/INS (GNSS Aided Inertial Navigation System) solution. The use of Micro-Electro-Mechan

• Additional Outputs: Magnetic Field (Magnetometer)
• Angular Rate Range: 300 deg/sec
• Bandwidth: 250 Hz
• Electrical Output: Serial / Digital

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

• Additional Outputs: Magnetic Field (Magnetometer)
• Angular Rate Range: 300 deg/sec
• Bandwidth: 500 Hz
• Electrical Output: Serial / Digital

Description: The 3DM-RQ1™ -45 Ruggedized Tactical Grade GPS-Aided Inertial Navigation System (GPS/INS) combines a MEMS inertial sensor core with a high sensitivity GPS receiver, and a sophisticated Extended Kalman Filter to generate optimal position, velocity, and attitude (PVA)

• Angular Rate Range: 75 to 900 deg/sec
• Bandwidth: 250 Hz
• Features: GPS Aided
• Linear Acceleration Measurement: MEMS

Description: Miniature GPS-Aided Inertial Navigation System Overview The 3DM-GX3® -45 high-performance, miniature GPS-Aided Inertial Navigation System (GPS/INS) combines MEMS inertial sensors, a highly-sensitive embedded GPS receiver, and a complex Extended Kalman

• Additional Outputs: Magnetic Field (Magnetometer)
• Angular Rate Range: 50 to 1200 deg/sec
• Bandwidth: 225 Hz
• Features: GPS Aided

Description: The LN-270 is a highly adaptable Inertial Navigation System/Global Positioning System (INS/GPS) that can be used for navigation or as a pointing/stabilizati on solution on land. Northrop Grumman's LN-270 is an integrated land navigator, used as a precision pointing

• Angular Rate Range: 1000 deg/sec
• Linear Acceleration Range: 13 +/-g
• Operating Temperature: -65.2 to 160 F

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

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

Description: • BITE Capability • Power Factor Correction • Multiple PCB Design • High Reliability GENERAL SPECIFICATION ¨ 115 V AC Single Phase Input ( 28 V DC ) ¨ Multiple Outputs +5V @ 7.5A, +290V @ 45mA, ±15V @ 1.2A, -5V @ 0.5A, +31.5 V @ 45mA ¨ Operating Temperature Range -40°C to +71°C ¨ BITE Capability ¨

• AC Input Voltage: 115 volts
• DC Output Current: 0.0450 to 7.5 amps
• DC Output Voltage: -15 to 290 volts
• Phase: Three-Phase

Description: GLOBAL NAVIGATION SATELLITE SYSTEMS, INERTIAL NAVIGATION, AND INTEGRATION

Description: manufactured in its own wafer fab, assembly and calibration lines, all located in France. They are well suited for system manufacturers with strong requirements for high bias stability, high-performance inertial sensors with strong vibration rejection. They are used in applications

Description: provides an additional benefit of an accurate GPS position fix while the UUV remains submerged. This further extends the mission capabilities by providing a reference position fix to the inertial navigation without expending time and power to return to the surface. Funding source: US

Description: The AHRS-2G is a high-performance strapdownattitude and heading reference system that determines absolute orientation (heading, pitch and roll) for any device on which it is mounted. Orientation is determined with high accuracy for both motionless and dynamic applications. In order to

• Additional Outputs: Magnetic Field (Magnetometer)
• Angular Rate Range: 400 deg/sec
• Bandwidth: 50 Hz
• Electrical Output: Serial / Digital

Description: The AHRS-6G is a high-performance strapdownattitude and heading reference system that determines absolute orientation (heading, pitch and roll) for any device on which it is mounted. Orientation is determined with high accuracy for both motionless and dynamic applications. In order to

• Additional Outputs: Magnetic Field (Magnetometer)
• Angular Rate Range: 300 deg/sec
• Bandwidth: 50 Hz
• Electrical Output: Serial / Digital

Description: possibilities of the MTi, and the integration possibilities of the MT with your own 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

Description: Gaming Sensor represents a shift from Inertial Labs traditional embedded 3DOF orientation systems. OS3D-GS is designed to provide compensated sensor data to the PC where the sensor fusion algorithms are then processed and applied to the application. This allows for the potential to

• Additional Outputs: Magnetic Field (Magnetometer)
• Angular Rate Range: 1200 deg/sec
• Electrical Output: Serial / Digital
• Features: Data Recorder

Description: The OptoWOM optically enhanced weapon orientation module combines technologies of inertial sensors with optical image tracking resulting in a robust and reliable 3DOF orientation module capable of operation in virtually any environment. With the addition of optical image tracking the

• Additional Outputs: Magnetic Field (Magnetometer)
• Angular Rate Range: 400 to 1000 deg/sec
• Device Type: Optical
• Electrical Output: Serial / Digital

Description: ). IMT40 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/ac celeration and attitude/angularrate /angular acceleration. The time signal

• Angular Rate Range: 0.0 to 6000 deg/sec
• Bandwidth: 0.0 to 60 Hz
• Device Type: Vibrating
• Electrical Output: Serial / Digital

Description: ). IMT40 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/ac celeration and attitude/angularrate /angular acceleration. The time signal

• Angular Rate Range: 0.0 to 6000 deg/sec
• Bandwidth: 0.0 to 2000 Hz
• Device Type: Vibrating
• Electrical Output: Serial / Digital

Description: Terms and definitions relating to aided and unaided inertial systems for navigation, guidance, orientation, stabilization, and related applications are presented. Usage as understood by the inertial systems community is given preference over general technical usage

Description: systems. Supply voltage can be 5V or 8-16V and low current consumption of less than 25mA. With a bandwidth of zero to 1500Hz these sensors are useful for applications within component and full vehicle testing and development programs. Typical applications include: Aero Performance

• Angular Rate Range: 200 deg/sec
• Bandwidth: 10 Hz
• Electrical Output: Analog Voltage
• Linear Acceleration Range: 100 +/-g

Description: The G300D Gyro represents Gladiator's breakthrough gyro technology enabling an ultra low noise tri-axis MEMS gyro and bandwidth of 250Hz that has performance commensurate with much more expensive small Dynamically Tuned Gyros. It also features industry leading bias in-run and bias over temperature.

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 160 F

Description: stability theory for nonlinear control design; derivation of optimal control strategies via Pontryagin's maximum principle; and derivation of a local coordinate system. In navigation, the global positioning system (GPS) is described in detail, as are inertial

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 (microelectromechani cal

Description: Inertial Sensing and Technology; GNSS; Connected, Integrated, Alternative Sensing; Application to Automated, Semi-Autonomous and Fully Autonomous Systems

• Industry: Aerospace, Automation and Robotics, Electronics and Semiconductor, Networking and Computing
• Type: Conference

Description: -restricted areas Savant Virtual Path?: The DC-25i utilizes a highly reliable and accurate, navigation system employing an 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,

• AGV Type: Unit Load AGV, Tugger AGV
• Guidance Type: Inertially Guided
• Load Capacity: 25000 lbs
• Load Transfer: Automatic, Manual