INS inertial system INS-BU
IMUAHRSwith integrated GPS

INS inertial system
INS inertial system
INS inertial system
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Characteristics

Type
IMU, INS, AHRS
Options
GNSS, for drones, for avionics instruments, lightweight, ITAR-free, miniature, with integrated GPS
Temperature range

Min.: -40 °C (-40 °F)

Max.: 85 °C (185 °F)

Description

Low Cost Single Antenna GPS-Aided Inertial Navigation Systems Input signals • Marine application: DVL (Doppler Velocity Log) • Land application: Odometer, Wheel sensor, Encoder, DMI • Aerial application: Wind sensor, Air Speed Sensor, Doppler shift from locator (for long-term GPS denied) • External Stand-Alone Magnetic Compass (SAMC/AHRS) Output signals • Horizontal and Vertical Positions, Heading, Pitch & Roll, Velocity, Accelerations, Angular rates, Barometric data, PPS • Direct AT_ITINS message with Position, Heading, Pitch & Roll to COBHAM AVIATOR UAV 200 • Direct Navigation Support for Pixhawk Flight Controllers as NMEA messages Main features Low Cost, 1 cm RTK position Data rate (INS) Hz Up to 200 (user settable) Data rate (IMU) Hz Up to 2000 (user settable) Start-up time sec <1 Positions, Velocity and Timestamps Units Horizontal position accuracy (SP, L1), RMS meters 1.5 Horizontal position accuracy (SP, L1/L2), RMS meters 1.2 Horizontal position accuracy (post processing) (1) meters 0.005 Horizontal position accuracy (RTK), RMS meters 0.01 + 1 ppm CEP Vertical position accuracy (SP), RMS meters <2 Vertical position accuracy (RTK), RMS meters 0.02 + 1 ppm CEP Position Accuracy (Free Inertial Land Vehicle) (2) %, DT 1 (Tunnel Guide positional aiding references) Velocity accuracy, RMS meters/sec 0.05 PPS timestamps accuracy nano sec 20
*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.