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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
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: -45 °C - 75 °C
SiIMU02® MEMS Inertial Measurement Unit (IMU) The UTC Aerospace Systems SiIMU02® is an all-digital, second generation, MEMS inertial measurement unit (IMU). It delivers excellent ...
Collins Aerospace - UTC Aerospace Systems
Temperature range: -55 °C - 85 °C
... ight control systems, anti-tank weapons, small UAVs and troop navigation units. UTC Aerospace Systems has a long and respected heritage in the design and development of inertial ...
Collins Aerospace - UTC Aerospace Systems
Temperature range: -40 °C - 85 °C
Single Antenna RTK GNSS Ellipse-N is a small-sized high-performance RTK Inertial Navigation System (INS) with an integrated Dual band, Quad Constellations GNSS receiver. It ...
SBG SYSTEMS
Temperature range: -40 °C - 85 °C
Ellipse-D is the smallest Inertial Navigation System integrating a Dual-antenna, multi-band GNSS receiver, capable of delivering precise heading as well as centimeter level position accuracy ...
SBG SYSTEMS
Temperature range: -40 °C - 85 °C
... provide efficient vibration rejection. Robust RTK Position during GNSS Outages For the INS models (E, N, D), the internal Extended Kalman Filter fuses in real-time inertial and RTK GNSS ...
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-U-OEM) is OEM version of new generation, fully-integrated, combined GPS, GLONASS, GALILEO, QZSS and BEIDOU GNSS ...
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.
... is ideal for commercial applications requiring high inertial performance approaching “FOG-Class”, yet available at much lower cost. Other key advantages include low power consumption, small size, light ...
Gladiator Technologies
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 - 75 °C
Bias stability: ≤ 0.05°/h Measurement range: ±500°/s Accelerometer range: ±30g Wide temperature range: ﹣40℃~+75℃ Power Supply：10~30V Small size: L97.3*W90*H70mm Weight: 1000g
Wuxi Bewis Sensing Tecnology LLC
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
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
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
... 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
... 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 ...
... 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
... 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.
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.
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
... 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 ...
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