This light-weight MEMS-based
Inertial Navigation System (INS)
integrates three gyroscopes, three
accelerometers along with GPS
information for a low cost medium
accuracy navigation performance for
air and ground applications.
- MEMS gyro & accelerometers.
- Rate: ± 300°/sec.
- Acceleration: ± 10g.
- Accuracy (1σ): 10m.
- Hybridization with GPS.
- RS-422 interface.
- Velocity, Position, Attitude outputs.
- Fully indigenous system software.