• Fully Integrated Honeywell HG4930 IMU
• Commercial ECCN 7A994 (No License Required) Export Status
• Precision Real time (RTK) & Post Processing (PPK)
• High Precision NovAtel Dual Antenna GNSS Receiver
• Honeywell HG4930 Tactical-grade IMU
• Position accuracy = 60 cm SBAS / 40 cm DGPS / 1 cm RTK / 2.5 cm PPP / 0.5 cm PPK
• Heading accuracy = 0.05 deg RTK / 0.015 deg PPK
• Pitch & Roll accuracy = 0.015 deg RTK / 0.003 deg PPK
• Small Size, light weight
• Compatible with LIDAR, Optical camera
• Applications: flight control, remote sensing, photogrammetry
The Inertial Labs GPS-Aided Inertial Navigation System (INS-DH-OEM) is an OEM version of the new generation of dual GNSS antenna, fully-integrated, combined GPS, GLONASS,
GALILEO and BEIDOU GNSS and high-performance strapdown system, that determines position, velocity and absolute orientation (Heading, Pitch and Roll) for any device on which it
is mounted. Horizontal and Vertical Position, Velocity, Dual Antenna Heading, Pitch & Roll are determined with high accuracy for both motionless and dynamic applications with IMU input
from the Honeywell HG4930 aided by the NovAtel Dual Antenna Receiver.
The Inertial Labs INS-DH-OEM utilizes an advanced dual antenna GNSS receiver, a Honeywell HG4930 IMU which has 3-axes each of calibrated in full operational temperature range Advanced MEMS Accelerometers and new generation of tactical grade MEMS Gyroscopes to provide accurate Position, Velocity, Heading, Pitch and Roll of the device under measure. INS-DH-OEM contains Inertial Labs new on-board sensors fusion filter, state of the art navigation
and guidance algorithms and calibration software.