Inertial Navigation Unit

Description: -weight sensor (49 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

• 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: 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

• Device Type: Optical
• Electrical Output: Serial / Digital
• Features: GPS Aided
• Linear Acceleration Measurement: Fiber Optic

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: 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

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

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: 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

• Electrical Output: Serial / Digital, Network / Fieldbus Output
• Features: Data Recorder, GPS Aided
• Linear Acceleration Measurement: MEMS
• Linear Acceleration Range: 2 +/-g

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: 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

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 multi

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

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

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 on

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 such as

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

Description: The 3DM-GX4-15™ is a miniature high end industrial Inertial Measurement Unit (IMU), utilizing the highest performance MEMS sensor technology. It combines a triaxial accelerometer, triaxial gyro, temperature sensors, pressure altimeter and dual on-board processors running a

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

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

• Additional Outputs: Magnetic Field (Magnetometer)
• Angular Rate Range: 50 to 1200 deg/sec
• Bandwidth: 225 Hz
• Electrical Output: Serial / Digital

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

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

Description: The MTi 10-series is available in three integration levels: an IMU, a VRU and an AHRS. The 10-IMU offers sensor data, also available as delta_q and delta_vel. It is an excellent unit for designing own fusion filter algorithms, using the MTi’s excellent signal processing pipeline. The 20

Description: The MTi 10-series is available in three integration levels: an IMU, a VRU and an AHRS. The 10-IMU offers sensor data, also available as delta_q and delta_vel. It is an excellent unit for designing own fusion filter algorithms, using the MTi’s excellent signal processing pipeline. The 20

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

• 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

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

Description: temperature. 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

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: embedded 12/24 channel, All-In-View, Selective Availability/Anti-Sp oofing Module (SAASM), P(Y) code or Standard Positioning Service (SPS) GPS. The LN-251 fully integrated, tightly coupled GPS inertial design provides superior navigation performance relative to other embedded INS/GPS

• Angular Rate Range: 1000 deg/sec
• Linear Acceleration Range: 28 +/-g
• Operating Temperature: -65.2 to 160 F

Description: mount and 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

• Angular Rate Range: 400 deg/sec
• Linear Acceleration Range: 16 +/-g

Description: The MTi 10-series is available in three integration levels: an IMU, a VRU and an AHRS. The 10-IMU offers sensor data, also available as delta_q and delta_vel. It is an excellent unit for designing own fusion filter algorithms, using the MTi’s excellent signal processing pipeline. The 20

Description: The MTi 10-series is available in three integration levels: an IMU, a VRU and an AHRS. The 10-IMU offers sensor data, also available as delta_q and delta_vel. It is an excellent unit for designing own fusion filter algorithms, using the MTi’s excellent signal processing pipeline. The 20

Description: 2,000 Pounds Standard Capacity Virtual Path? 'Tape-free/Target-fr ee' Navigation

• AGV Type: Unit Load AGV, Tugger AGV
• Conveyor Coupling: Yes
• Guidance Type: Inertially Guided
• Load Capacity: 2000 lbs

Description: 10,000 Pounds Standard Capacity Virtual Path? 'Tape-free/Target-fr ee' Navigation

• AGV Type: Unit Load AGV, Tugger AGV
• Conveyor Coupling: Yes
• Guidance Type: Inertially Guided
• Load Capacity: 10000 lbs

Description: 7,000 Pounds Standard Capacity Virtual Path? 'Tape-free/Target-fr ee' Navigation

• AGV Type: Unit Load AGV, Tugger AGV
• Conveyor Coupling: Yes
• Guidance Type: Inertially Guided
• Load Capacity: 7000 lbs

Description: highly reliable and 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,

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

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

• AGV Type: Unit Load AGV, Forklift AGV, Tugger AGV
• Guidance Type: Laser Guided, Inertially Guided, Wire Guided
• Lift Height: 26.25 ft
• Load Capacity: 3308 lbs

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

• AGV Type: Unit Load AGV, Forklift AGV, Tugger AGV
• Guidance Type: Laser Guided, Inertially Guided, Wire Guided
• Lift Height: 3.28 ft
• Load Capacity: 1102 lbs

Description: AGVE offers a unique range of automated guided vehicles (AGVs), ranging from standard models to over 100 tailor-made vehicles. AGVE provide the highest quality automated guided vehicles for the most demanding applications. Load capacity between 3kg and 65 ton Quad directional motion available All

• AGV Type: Unit Load AGV, Forklift AGV, Tugger AGV
• Guidance Type: Laser Guided, Inertially Guided, Wire Guided
• Lift Height: 32.81 ft
• Load Capacity: 130000 lbs

Description: This specification defines the requirements for a two-degree-of-freedo m 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

Description: verification of the sensor’s integrity and continuous in-operation functionality test. MEMS gyros for navigation of dynamic applications GYPRO®4300 is a high stability MEMS gyro tailored to GNSS-assisted inertial navigation and positioning of ground vehicles and trains,

• Angular / Rotary Axes: Uniaxial
• Angular Rate Range: 300 deg/sec
• Bandwidth: 200 Hz
• Bias Stability: 0.4000 deg/hr

Description: power consumption. With a 1 year composite bias repeatability of 1 mg under demanding temperature and vibrations conditions, it overpasses all commercially available MEMS accelerometers. AXO®315 is the perfect candidate for integration into high performance Inertial Measurement Units

• Acceleration: 14 g
• Device Type: Sensor / Transducer
• Features: Self Test / Diagnostics / Self Calibrating
• Frequency Range: 300 Hz

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

• Angular / Rotary Axes: Triaxial
• Angular Rate Range: 300 deg/sec
• Electrical Output: Pulse / Frequency
• Operating Temperature: -40 to 85 F

Description: commercial, space and military 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

• Composition: Pure Gas
• Concentration: 99.99 %
• Noble Gases: Neon
• Product Forms: Gas

Description: The unrivalled noise level and excellent bias stability make AXO®305 an industry-leading sensor solution to build IMU (Inertial Measurement Unit), MRU (Motion Reference Unit), GNSS-aided positioning, navigation, precision attitude, motion control and tilt measurements

• Acceleration: 5 g
• Device Type: Sensor / Transducer
• Features: Self Test / Diagnostics / Self Calibrating
• Frequency Range: 120 Hz

Description: The FMT1030 is an AHRS (Attitude and Heading Reference System) Motion Tracking Module with . output of Orientation, Inertial Motion Data and Magnetic Field. With data rates of up to 1 kHz and orientation accuracy of 3° RMS, industrial applications in control, stabilisation, and

• Package Type / Mounting: Other
• Sensor Type: Acceleration Sensor

Description: reference with an initial tolerance as low as ±0.05%. Applications A/D and D/A Converters Precision Regulators Digital Voltmeters Inertial Navigation Systems Precision Scales Portable Reference Standard

• IC Package Type: DIP / CDIP / PDIP, SOIC / SOP, Other
• Initial Accuracy: 0.0500 %
• Life Cycle Stage: Other
• Operating Temperature: 0.0 to 70 C

Description: ideal for orientation and navigation systems in unmanned aerial vehicles using Inertial Measurement Units (IMUs) and inclinometers. By providing repeatable tilt measurement under all conditions, the new accelerometers enable minimal tilt error without extensive calibration in

• Acceleration: 2 to 8 g
• Features: Wireless
• Operating Temperature: -40 to 257 F
• Sensor Inputs: Accelerometer