Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving

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Shenzhen Fire Power Control Technology Co., LTD

City: shenzhen

Province/State:guangdong

Country/Region:china

Tel:86-755-23097872

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Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving

Brand Name	Firepower
Model Number	GI100C-B0
Certification	CE ROHS
Place of Origin	CHINA
Minimum Order Quantity	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

Detailed 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
Gyroscope	Zero bias stability	2°/h
Accelerometer	Measuring range	±16g
Accelerometer	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
Structural characteristics	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)

Product Tags: Autonomous Driving MEMS INS Low gyro bias Inertial navigation system Low gyro bias MEMS INS

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