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IMU inertial system INS-P
AHRSINSMEMS

IMU inertial system - INS-P - Inertial Labs, Inc. - AHRS / INS / MEMS
IMU inertial system - INS-P - Inertial Labs, Inc. - AHRS / INS / MEMS
IMU inertial system - INS-P - Inertial Labs, Inc. - AHRS / INS / MEMS - image - 2
IMU inertial system - INS-P - Inertial Labs, Inc. - AHRS / INS / MEMS - image - 3
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Characteristics

Type
IMU, AHRS, INS, MEMS, motion control
Options
GNSS, with integrated GPS, for UAV, miniature, navigation, for avionics instruments, 3-axis, high-accuracy, lightweight, ITAR-free
Temperature range

Max.: 85 °C
(185 °F)

Min.: -50 °C
(-58 °F)

Description

INS-P Single Antenna Professional Single GNSS Antenna - - - - - - - - - - Heading Accuracy: 0.4° static / 0.1° dynamic Position Accuracy: 1cm (RTK), 2.5cm (PPP), 60cm (SBAS) Pitch & Roll Accuracy: 0.03° dynamic, 0.05° static GNSS Constellations: BDS, GAL, GLO, GPS, QZSS. Corrections: DGPS, PPK, PPP, RTK, SBAS. Type of IMU: MEMS, Tactical-grade. Magnetometer: Embedded Fluxgate Magnetic Compass. Other Features: All INS-B features + Fluxgate Gyro-Compensated Compass (Magnetometer) – high performance in longterm GPS-Denied environment. Size (mm): 120.5 x 53.2 x 49.3 Applications: Extended GNSS-Denied Navigation; UAS; North Finding & Keeping. - - - - - - - - - -

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