Inertial Labs INS-DM Ruggedised Dual Antenna GPS Aided Inertial Navigation System (INS).
Inertial Labs INS-DM GPS Aided Ruggedised INS Features:
Commercially exportable GPS-Aided Inertial Navigation System
3-in-1 strapdown system: INS + AHRS + ADC (Air Data Computer)
Embedded Honeywell or Inertial Labs MEMS Inertial Measurement Unit (IMU)
NovAtel OEM7, u-blox ZED-F9P, or Septentrio mosaic-H High Precision GNSS receiver
GPS, GLONASS, GALILEO, BEIDOU, QZSS, RTK supported signals
Total and Static Pressure Sensors for calculating Indicated Airspeed
SP, SBAS, DGPS, RTK and PPP for real time operation
GNSS measurements and IMU raw data for post processing
Advanced, extendable, embedded Kalman Filter based sensor fusion algorithms
State-of-the-art algorithms for different dynamic motions of Helicopters, and UAV
Full temperature calibration of all sensing elements
EMC, EMI, and ERD protection
Environmentally sealed (IP68)
Aiding data: Wind sensor, Air Speed Sensor, Doppler shift from locator (for long-term GPS denied), External position and External Heading
Inertial Labs GPS-Aided Inertial Navigation System (INS-DM) is the latest version of Inertial Navigation System, developed by Inertial Labs.
INS-DM, is an IP68 rated version of an all new generation of super ruggedised, shielded from the EMC/EMI, fully-integrated, combined Inertial Navigation System (INS) + Attitude & Heading Reference System (AHRS) + Air Data Computer (ADC) high-performance strapdown system, that determines position, velocity and absolute orientation (Heading, Pitch and Roll) for any device on which it is mounted.