Inertial Labs INS-U

Horizontal and Vertical Position, Velocity and Orientation are determined with high accuracy for both motionless and dynamic applications.

The Inertial Labs INS-U utilizes advanced single antenna multi constellation (GPS, GLONASS, GALILEO, QZSS and BEIDOU GNSS) receiver; two Honeywell TruStability® Board Mount Pressure Sensors; a miniature gyro-compensated Fluxgate compass; 3-axes each of calibrated in full operational temperature range Advanced MEMS Accelerometers and Gyroscopes to provide accurate Position, Velocity, Heading, Pitch and Roll of the device under measure.

INS-U contains Inertial Labs new on-board sensor fusion filter, state-of-the-art navigation and guidance algorithms and calibration software.

KEY FEATURES, BENEFITS & FUNCTIONALITY

• Commercially exportable GPS-Aided Inertial Navigation System

• 3-in-1 strapdown system: INS + AHRS + ADC (Air Data Computer)

• Embeddedin-flightcalibration

• 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