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HGuide n380 Inertial Navigation System
The HGuide n380 is an incredibly small, light-weight, self-contained, all-attitude Inertial Navigation System designed for applications where robust, continuous position and attitude navigation data is required.
The HGuide n380 is an incredibly small, light-weight, self-contained, all-attitude Inertial Navigation System designed for applications where robust, continuous position and attitude navigation data is required.
The HGuide n380 contains Honeywell’s leading edge i300 inertial measurement unit (IMU) and provides a powerful dual-antenna, multi-frequency, multi-constellation RTK capability.
Honeywell’s integration expertise blends the IMU and GNSS data to provide an accurate, robust navigation service to your application with all the functionalities that you need.
The HGuide n380 output data includes time stamped position, velocity, angular rate, linear acceleration, roll, pitch and heading information. In dual-antenna mode, the device supports GNSS-based heading measurements and initialization.
Key Honeywell Advantages:
- Honeywell proven navigation algorithms for air, land and sea.
- World-class inertial sensor development, calibration, and compensation.
- Proven reliability, dependability, and ruggedness.
- Accepts RTCM3 GNSS corrections.
- Highest performing Inertial Navigation System of its size, weight and price.
- Configuration flexibility. Only purchase the features you need.
- Multiple configurable communication ports.
- The HGuide n380 is not ITAR controlled. Its Export Control Classification Number (ECCN) is 7A994.
An inertial navigation system (INS) is comprised of an IMU, a global navigation satellite system (GNSS) receiver and sensor fusion software. These components work together to calculate position, orientation, and velocity to deliver critical navigation information in GNSS-denied areas like urban canyons, bridges, tunnels, mountains, parking garages and dense forests.
The heart of an INS system is its inertial measurement unit (IMU). This mechanism is composed of three orthogonal gyros and three orthogonal accelerometers.
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