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Brand Name : Firepower
Model Number : GI100C-B0
Certification : CE ROHS
Place of Origin : CHINA
MOQ : 1
Price : negotiable
Payment Terms : T/T
Supply Ability : 500/month
Delivery Time : 10 days
Packaging Details : sponge+carton
Product name : Integrated Navigation System with GNSS
Heading precision : 0.1deg (rms)
Attitude accuracy : 0.1deg (rms)
Horizontal velocity accuracy : 0.1m/s(RMS)
Gyro range : ±450°/s
Gyro zero bias stability : 2°/h
Accelerometer range : ±16g
Accelerometer zero bias stability : 30µg
Operating temperature : -40℃~+60℃
Vibration : 5~2000Hz
Low gyro bias MEMS INS Inertial navigation system for Autonomous Driving
Product Description
The GI100C-B0 integrated navigation system consists of MEMS sensors and a high-end GNSS receiver board (NovAtel-718D), which is implemented through multi-sensor fusion and navigation solving algorithms. This product has high reliability and strong environmental adaptability. By matching different software, the product can be widely used in fields such as drones, unmanned vehicles, surveying and mapping, marine compasses, stable platforms, and underwater vehicles.
Main functions
The integrated navigation system utilizes GNSS receiver to receive satellite navigation information for combined navigation, outputting carrier's pitch, roll, heading, position, velocity, time, etc.After losing the signal, it outputs the position, velocity and attitude information of inertial solution, and has a certain navigation accuracy maintenance function in a short time. When combined with navigation, it can output the raw information that can be used for post-processing to be processed by the IE post-processing software of NovAtel.
Performance index
Project | Indicators | |
Heading accuracy | Dual GNSS (2m baseline) | 0.1°(RMS) |
Single GNSS | 0.2°(RMS) | |
Post-processing | 0.03°(RMS) | |
Course keeping (GNSS failure) | 1°/min(RMS) | |
Attitude accuracy | GNSS valid (single point L1/L2) | 0.1°(RMS) |
Inertia/odometer combination (optional) | 0.1°(RMS) | |
Post-processing | 0.02°(RMS) | |
Hold (GNSS failure) | 1°/min(RMS) | |
Horizontal positioning accuracy | GNSS valid, single point L1/L2 | 1.2m(RMS) |
Inertia/odometer combination (optional) | 2 ‰ D (D represents mileage, CEP) | |
RTK | 2cm+1ppm(RMS) | |
Post-processing | 1cm+1ppm(RMS) | |
GNSS failure | 1m/10s,10m/30s,20m/60s(RMS) | |
Horizontal velocity accuracy | GNSS valid, single point L1/L2 | 0.1m/s(RMS) |
Inertia/odometer combination (optional) | 0.1m/s(RMS) | |
Inertial/DVL combination (optional) | 0.2m/s(RMS) | |
Gyroscope | Measuring range | ±450°/s |
Zero bias stability | 2°/h | |
Accelerometer | Measuring range | ±16g |
Zero bias stability | 30µg | |
Communication interface | RS422 /RS232 | Route 7 |
CAN (optional) | Route 1 | |
Baud rate up to 1Mbps | ||
Transmitting frequency up to 200Hz | ||
Ethernet interface | 10M | |
Odometer differential input (optional) | Route 2 | |
PPS | Route 1 | |
EVENT | Route 1 | |
Electrical characteristics | Voltage | 9~36VDC |
Power consumption | ≤10W | |
Built-in memory (optional) | 16G | |
Structural characteristics | Size | 117mm×96mm×39.8mm |
Weight | ≤0.4kg | |
Use environment | Operating temperature | -40℃~+60℃ |
Storage temperature | -45℃~+65℃ | |
Vibration | 5~2000Hz,2g | |
Impact | 30g,11ms | |
Reliability | MTBF | 30000h |
Life span | > 15 years | |
Continuous working time | >24h |
Product structure
L117mm x W96mm x H39.8mm(L x W x H)
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Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving Images |