OUR STORY
OEM-IMU-HG4930
The OEM-IMU-HG4930 is a high performing Micro Electro Mechanical Systems (MEMS) Inertial Measurement Unit (IMU). This IMU is economical, robust, small and operates on low power allowing it to provide tactical grade performance. It's ideal for use in unmanned vehicles and commercial or military guidance applications. The IMU is comprised entirely of commercial components which will simplify the export process.
NovAtel’s Synchronous Position, Attitude and Navigation (SPAN) technology can be integrated with this IMU to provide accurate 3D position, velocity and attitude data in a compact package. This combination makes the IMU ideal to use in airborne, marine and ground applications.
Features
- Ideal for size and weight constrained applications
- 5 VDC power input
- 100 Hz data rate
- SPAN GNSS+INS functionality
- MEMS gyros and accelerometers
Attributes
| General Info | Width/Diametre (mm) | 64.8 |
| Height (mm) | 35.7 | |
| Weight (g) | 200 | |
| Typical Power Consumption (W) | 3 | |
| IMU Data Rate | 100 Hz | |
| Gyro Type | MEMS | |
| Performance | Gyro Range (±deg/s) | 200 |
| Accelerometer (±g) | 20 |
OEM7 Receivers
Multi-frequency GNSS receivers that use a 555-channel architecture and can track all current and upcoming constellations.
Antennas
GNSS receiver performance is dependent on your choice of antenna. We offer high-performance, compact, anti-jam antennas and ground reference station antennas.
SPAN CPT7
The SPAN CPT7 is an ultra-compact, light-weight, dual-antenna SPAN® enclosure that delivers 3D position, velocity and attitude.
OEM-HG1930
Small, affordable MEMS IMU pairs with SPAN® technology to deliver 3D position, velocity and attitude.
IMU-LN200
Tactical grade, low noise IMU combines with NovAtel’s GNSS technology to provide 3D position, velocity and attitude solution.
TerraStar Correction Services
Global and regional correction services ranging from 2 cm to 50 cm accuracy for land and airborne applications.
Inertial Explorer®
Expands on the powerful features of GrafNav by adding support for loosely coupled and tightly coupled GNSS+INS processing.
