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EGIS-N400 (Compact EGI System)
Region
South Korea
Category
Aviation
Application - UAVs/Drone- Combat Tanks/Armored Vehicles- Light Combat Robots- Maneuvering Weapon System- Unmanned Autonomous Robots Characteristics - Continuous, Reliable 3D Navigation even in GNSS Unavailable Areas(Tunnels, Urban Canyon)- Extended Kalman Filter Technology to Combine Inertial Sensor, GNSS, VMS, etc.- Automatic Switchover to Optimal Navigation Mode in Accordance with Operation Environment (GNSS/INS/VMS/ZUPT)- Store Alignment/In-Motion Alignment Function to Minimize Initial Start-Up Time- Optional
Functions of DGPS/RTK- Post-Processing Solution for Improving Navigation Accuracy of Real-Time Trajectory- Flexible Configurations Support for Various Operation Environments- High Reliability to Meet the Operating Conditions of Severe Battlefields- Competitive Solution Considering Price/Performance Specifications Accuracy (With GNSS) Positioning 3m CEP(Horizontal) Velocity 0.5m/s RMS Attitude (Roll/Pitch/Yaw) 0.2 ° RMS/0.2 ° RMS/0.5 ° RMS GNSS Receiver Supported Frequency GPS L1/L2 GLONASS L1/L2 Galileo E1/E5 BeiDou B1/B2 Interface Output Data Position, Velocity, Attitude, Time etc Output Rate 100Hz Input/Output RS-232 or RS-422 VMS, 1PPS, AirData Power Input Voltage 9~36VDC(24VDC Nominal) Consumption 6W(Nominal) Size 75(W)x47(H)x90(L)mm Weight