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Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving

Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving
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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
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Autonomous Driving MEMS INS


Low gyro bias Inertial navigation system


Low gyro bias MEMS INS

Basic Infomation
Place of Origin: CHINA
Brand Name: AVIC
Certification: CE ROHS
Model Number: GI100C-B0
Payment & Shipping Terms
Packaging Details: sponge+carton
Delivery Time: 10 days
Payment Terms: T/T
Supply Ability: 500/month
Product Description

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


Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving 0


                     L117mm x W96mm x H39.8mm(L x W x H)


Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving 1Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving 2


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