Inertial Labs INS-U GPS Aided INS with Air Data Computer

GPS Aided INS with Air Data Computer

Fixed Wing UAV Flight Control and Navigation in longterm GNSS Denied Environments

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Inertial Labs INS-U a GPS Aided Inertial Navigation System (INS) with air data computer.

Inertial Labs INS-U GPS Aided INS Features:
Commercially exportable GPS-Aided Inertial Navigation System
3-in-1 strapdown system: INS + AHRS + ADC (Air Data Computer)
Embedded in-flight calibration
Designed for UAV application algorithm
UBlox ZED-F9P F9 High Precision GNSS Module
Small size, lightweight & low power: 82 x 40.0 x 26.0 mm, <200-grams, <1 watt
Total and Static Pressure Sensors for calculating Indicated Airspeed
Embedded Gyro-compensated Mini-Fluxgate magnetometers (compass)
GNSS measurements and IMU raw data for post processing
Advanced, extendable, embedded Kalman Filter based sensor fusion algorithms
State-of-the-art algorithms for different dynamic motions of Helicopters, and UAV
Full temperature calibration of all sensing elements
Environmentally sealed (IP67)
Aiding data: Wind sensor, Air Speed Sensor, Doppler shift from locator (for long-term GPS denied), External position and External Heading




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