- Components - Spare Parts
- Flight and Cockpit Instrument
- INS inertial system
- Inertial Labs, Inc.
IMU inertial system INS-DAHRSINSMEMS
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Characteristics
- Type
- IMU, AHRS, INS, MEMS, motion control
- Options
- miniature, GNSS, with integrated GPS, for UAV, navigation, for avionics instruments, with integrated dual-antenna GPS, 3-axis, high-accuracy, lightweight, ITAR-free
- Temperature range
Max.: 85 °C
(185 °F)Min.: -50 °C
(-58 °F)
Description
INS-D
Dual Antenna
Dual GNSS Antenna Inertial Navigation System
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Heading Accuracy: 0.8° (2m baseline) / 0.15° (1m baseline).
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: All INS-B features + high-precision dual GNSS Heading (HDT).
Size (mm): 120.5 x 53.2 x 49.3
Applications: Heavy Vehicle Guidance; Land Vehicle Navigation; Fixed Wing Navigation.
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Other Inertial Labs, Inc. products
INS – GPS-Aided Inertial Navigation Systems
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