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GPS-Aided Inertial Navigation Systems INS-U

The environmentally sealed IP67 version of InertialLabs GPS-aided inertial navigation system, INS-U is a new generation high-performance 3 in 1 strapdown system that determines position, velocity and absolute orientation of a device. This is fully-integrated and equipped with Inertial Navigation System (INS) + Attitude & Heading Reference System (AHRS) + Air Data Computer (ADC). The sensor fusion results in high accuracy measurement for both motionless and dynamic objects. The GPS-aided inertial navigation system, INS-U makes use of single antenna multi-constellation GNSS receiver, two barometers; miniature gyro-compensated Fluxgate compass along with 3-axes each of Advanced MEMS Accelerometers and Gyroscopes.  All of its sensing elements are temperature calibrated. It also comprises total and static pressure sensors for calculating indicated airspeed. The INS-U  device is specially designed for fixed-wing and multi-rotor Aerial Platforms. Its small size, light weight and low power consumption makes it ideal for a myriad of applications. Its advanced and leading-edge technology of sensor fusion algorithm, Kalman filter makes it noteworthy for different motions of Helicopters and UAV.
PARAMETERS GPS-aided inertial navigation system INS-U
Measurement Range: Gyroscope ±2000 deg/sec
Measurement Range: Accelerometer ±8 ; ±15 ; ±10 g
Measurement Range: Magnetometer ±8 gauss
Operating Temperature -40 to +85 deg C
Size 82mm x 40mm x 26mm
Weight < 200 gm
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