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Inertial systems
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Temperature range: -40 °C - 85 °C
... 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

Temperature range: -40 °C - 85 °C
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

Temperature range: -40 °C - 85 °C
... Heading Reference System (AHRS). It embeds a best in class magnetic calibration procedure for optimal heading, and It is suitable for low to medium dynamic applications. Factory calibrated from -40 to 85°C, this ...
SBG Systems

Temperature range: -55 °C - 70 °C
... attitude heading reference system is a revolutionary, dual-channel system that combines attitude, altitude, airspeed, air temperature and heading information into a single box. The air data attitude ...

... , VSI, AOA, G-meter, turn rate, slip/skid ball, OAT, and TAS. Add a secondary ADAHRS for redundancy and SkyView and AFS EFIS systems automatically cross-check your instruments for you. For aircraft where ...

Temperature range: -40 °C - 85 °C
STIM277H is a small, tactical grade, affordable, robust and reliable, ultra high performance (Bias Stability 0.3°/h, ARW 0.15°/√h) 3 axis MEMS gyro module built into a hermetic package. The package is a hermetic aluminum enclosure with ...
MC MURDO GROUP

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 performance. The ...
Bendix/King by Honeywell

Temperature range: -55 °C - 70 °C
... 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

... affordable, reliable inertial data for both fixed- and rotary-wing platforms. Both of these products have been proven as excellent replacements of legacy DGVG sets or antiquated AHRS/ADAHRS to modernize your aircraft. The ...
Archangel Systems, Inc.

Temperature range: -40 °C - 85 °C
This AHRS is equipped with our most accurate gyros and a precision magnetometer to provide you with attitude and heading reference data in applications where GPS data could be lost or is not available. Features: Solid ...
Watson Industries, Inc.

Orientus is a miniature IMU and AHRS that provides accurate orientation under the most demanding conditions. Roll & Pitch 0.2 ° Heading (Magnetic) 0.8 ° Bias Instability 3 °/hr Update Rate 1000 Hz Orientus ...
Advanced Navigation

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

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

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: ...

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.

Temperature range: -40 °C - 65 °C
... such as GNSS / odometer / DVL / barometric altimeter and has excellent scalability. It combines inertial measurement with satellite navigation and odometer information through multi-sensor data fusion ...
Wuxi Bewis Sensing Tecnology LLC

... 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
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

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.

... cost NON-ITAR MEMS Inertial Measurement Unit (IMU) provides internally temperature compensated RS422/RS485 output at up to 5000Hz data rate of delta velocity and delta theta. This Inertial Measurement ...
Gladiator Technologies
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