- Components - Spare Parts
- Flight and Cockpit Instrument
- INS inertial system
- Inertial Labs, Inc.
IMU inertial system INS-BAHRSINSMEMS
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Characteristics
- Type
- IMU, AHRS, INS, MEMS, motion control
- Options
- GNSS, with integrated GPS, for UAV, navigation, for avionics instruments, 3-axis, high-accuracy, lightweight, ITAR-free
- Temperature range
Min.: -50 °C
(-58 °F)Max.: 85 °C
(185 °F)
Description
INS-B
Single Antenna
Basic Single GNSS Antenna Inertial Navigation System.
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Heading Accuracy: 1° 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: External Magnetic Compass (optional).
Other Features: Tactical Grade IMU, Advanced, extendable, embedded Kalman Filter with sensor fusion algorithms.
Size (mm): 120.5 x 53.2 x 49.3
Applications: UGV; Land Vehicle Navigation; Lightweight AGV; Post Processed Imagery.
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Other Inertial Labs, Inc. products
INS – GPS-Aided Inertial Navigation Systems
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*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.