INS-U - GPS-Aided Inertial Navigation System

INS-U - GPS-Aided Inertial Navigation System

Inertial Labs INS Brochure and Datasheet

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 (INS) + Attitude & Heading Reference System (AHRS) + Air Data Computer (ADC) high-performance strapdown system, that determines position, velocity and absolute orientation (Heading, Pitch and Roll) for any device on which it is mounted. Horizontal and Vertical Position, Velocity and Orientation are determined with high accuracy for both motionless and dynamic applications.

KEY FEATURES, BENEFITS & FUNCTIONALITY
• 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
• GPS, GLONASS, GALILEO, BEIDOU, QZSS, RTK supported signals
• 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