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Gyroscopes are critical rotation sensing elements used in navigation systems (inertial navigation systems (INS), attitude and heading reference systems (AHRS) or inertial ...
Honeywell | Safety and Productivity Solutions
The HGuide n580 inertial navigation system is a small, light-weight, self-contained, all-attitude inertial navigation system which can be used in a wide variety of industrial ...
Honeywell | Safety and Productivity Solutions
... gyro-based systems and simplifies system integration by offering many configurable features – such as data rate output and flight control filtering. External heat sinks and cooling are not required by ...
Honeywell | Safety and Productivity Solutions
Temperature range: -55 °C - 70 °C
KSG7200 Air Data Attitude Heading and Reference System The air data attitude heading reference system is a revolutionary, dual-channel system that combines attitude, altitude, airspeed, ...
HONEYWELL
... Reference System Provides primary flight instruments, including attitude, airspeed, altitude, magnetic heading, DG, VSI, AOA, G-meter, turn rate, slip/skid ball, OAT, and TAS. Add a secondary ADAHRS for redundancy ...
... of Litef LCR92 and LCR-93 Attitude Heading Reference Systems (AHRS). The CCU provides control of the following functions of the Litef AHRS; Selection between SLAVED and FREE mode of operation AHRS ...
DAC INTERNATIONAL
... small-sized high performance RTK Inertial Navigation System (INS) with integrated GNSS receiver. It provides Roll, Pitch, Heading, Heave, and Navigation data. This light-weight sensor ...
SBG SYSTEMS
Ellipse-D is a compact Inertial Navigation System with integrated dual-antenna RTK GNSS receiver for accurate Heading and Navigation. It provides Roll, Pitch, Heading, Heave, and Navigation ...
SBG SYSTEMS
... small-sized high performance Attitude and Heading Reference System (AHRS). It provides Roll, Pitch, Heading, and Heave data. This light-weight sensor (45 grams) includes a MEMS-based Inertial Measurement ...
SBG SYSTEMS
Temperature range: -40 °C - 85 °C
The Inertial Labs GPS-Aided Inertial Navigation System (INS-U) is an IP67 rated version of the new generation, fully integrated, combined Inertial Navigation System ...
Inertial Labs, Inc.
Temperature range: -40 °C - 85 °C
The Inertial Labs GPS-Aided Inertial Navigation System (INS-DH-OEM) is an OEM version of the new generation of dual GNSS antenna, fully integrated, combined GPS, GLONASS, ...
Inertial Labs, Inc.
Temperature range: -40 °C - 85 °C
... new INS-DU-OEM is a high performance strapdown system that determines position, velocity, and absolute orientation to any platform that it is mounted to. It utilizes a cost-effective, dual antenna uBlox GNSS ...
Inertial Labs, Inc.
A40 MEMS Single-Axis accel offers both low noise and excellent bias with a small light weight form factor and low power. Designed for commercial marine, train and aircraft applications that require high performance, the ...
Gladiator Technologies
... to AHRS or INS functionality. It is available in both OEM and enclosed packages. Performance - 0.03 ° Roll and Pitch - 0.05 ° Heading - 0.2 °/hr MEMS Gyroscope - 1000 Hz Update Rate Key Features - Hot Start ...
Advanced Navigation
Orientus is a ruggedised miniature sensor and AHRS that provides accurate orientation under the most demanding conditions. It combines temperature calibrated accelerometers, gyroscopes and magnetometers in a sophisticated ...
Advanced Navigation
CERTUS is a GNSS aided Inertial Navigation System (INS) that provides accurate position, velocity, acceleration and orientation. It offers reliable data and 8 mm RTK position accuracy. ...
Advanced Navigation
The KRG 331 was developed to provide a yaw stability to the BendixKing Flight Control Systems. The KRG 331 senses angular displacement, making it simple to mount anywhere on the aircraft centerline without impact to ...
Bendix/King by Honeywell
Temperature range: -40 °C - 85 °C
The VN-100 is a miniature, high-performance Inertial Measurement Unit (IMU) and Attitude Heading Reference System (AHRS). Incorporating the latest MEMS sensor technology, the VN-100 combines 3-axis accelerometers, ...
VectorNav Technologies
Temperature range: -40 °C - 85 °C
... supported by the UTC Aerospace Systems commitment to the technical through-life support necessary for major procurement programmes. UTC Aerospace Systems has a long and respected heritage in the design ...
Collins Aerospace - UTC Aerospace Systems
Temperature range: -40 °C - 85 °C
Inertial sensors First Sensor features a highly innovative technology platform for manufacturing high-precision inertial sensors for geoengineering, condition monitoring or navigation applications. The ...
... MOD2) Attitude Heading Reference System (AHRS) has an initialization time that is 3X faster and now comes with a selectable low- and high-speed ARINC 429 output which allows for additional interface option with radar ...
Sandel Avionics
LISA-4000 belongs to the family of Strap Down Inertial Reference and Navigation System. It provides necessary Navigation functions for mission success. LISA-4000 performs two distinct basic functions: ...
Temperature range: -20 °C - 50 °C
High-end gyroscoop sensor ARS-06 - Range: ± 200 radian/sec (± 11,500 degree/sec) - Non-linearity: < 0.1 % - Temperature – Operating: -20 to +50 ºC (-4 to +122 ºF) - Output Impedance: < 100 ? ARS-06 - MHD Angular Rate Sensor The ARS-06 ...
Althen Sensors & Controls
The Geo-iNAV® 1000 is a low-cost, rugged GPS-aided inertial navigation system. The Geo-iNAV 1000 tightly couples a single-frequency GPS sensor with a high-stability Quartz MEMS IMU to ...
Geodetics, Inc.
uAHRS Attitude Heading Reference System with EVB interface board, semi-rugged case, and cables for fast and convenient evaluation.The uAHRS Development Kit provides the necessary components for quick and easy evaluation ...
Inertial Sense
The SAGI series GNC (Micro Guidance Navigation Control System) isthe new generation of guidance navigation control system designed forcommercial UAV with high integration and reliability. ...
AheadX Tech (Beijing) Co. Ltd.
... Heading Reference System (ADAHRS) and Inertial Navigation System (INS). It is perfect for system integration in avionics packages or other attitude sensing applications, ...
Temperature range: -40 °C - 85 °C
... Dynamic Measurement System (DMS) was designed for monitoring the drive and handling characteristics of vehicles. The DMS may be used in almost any application where triaxial angular rate and acceleration data is required. ...
Watson Industries, Inc.
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