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Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving

Categories Inertial Navigation System
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
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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


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


ProjectIndicators
Heading accuracyDual GNSS (2m baseline)0.1°(RMS)
Single GNSS0.2°(RMS)
Post-processing0.03°(RMS)
Course keeping (GNSS failure)1°/min(RMS)
Attitude accuracyGNSS valid (single point L1/L2)0.1°(RMS)
Inertia/odometer combination (optional)0.1°(RMS)
Post-processing0.02°(RMS)
Hold (GNSS failure)1°/min(RMS)
Horizontal positioning accuracyGNSS valid, single point L1/L21.2m(RMS)
Inertia/odometer combination (optional)2 ‰ D (D represents mileage, CEP)
RTK2cm+1ppm(RMS)
Post-processing1cm+1ppm(RMS)
GNSS failure1m/10s,10m/30s,20m/60s(RMS)
Horizontal velocity accuracyGNSS valid, single point L1/L20.1m/s(RMS)
Inertia/odometer combination (optional)0.1m/s(RMS)
Inertial/DVL combination (optional)0.2m/s(RMS)
GyroscopeMeasuring range±450°/s
Zero bias stability2°/h
AccelerometerMeasuring range±16g
Zero bias stability30µg
Communication interfaceRS422 /RS232Route 7
CAN (optional)Route 1
Baud rate up to 1Mbps
Transmitting frequency up to 200Hz
Ethernet interface10M
Odometer differential input (optional)Route 2
PPSRoute 1
EVENTRoute 1
Electrical characteristicsVoltage9~36VDC
Power consumption≤10W
Built-in memory (optional)16G
Structural characteristicsSize117mm×96mm×39.8mm
Weight≤0.4kg
Use environmentOperating temperature-40℃~+60℃
Storage temperature-45℃~+65℃
Vibration5~2000Hz,2g
Impact30g,11ms
ReliabilityMTBF30000h
Life span> 15 years
Continuous working time>24h

Product structure



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



Cheap Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving for sale
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