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Inertial Navigation System

Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving

Name: Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: GI100C-B0
Price: 5,000.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	GI100C-B0
MOQ:	1
Price:	negotiable
Payment Terms:	T/T
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Certification:

CE ROHS

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

Packaging Details:

sponge+carton

Supply Ability:

500/month

Highlight:

Autonomous Driving MEMS INS

Low gyro bias Inertial navigation system

Low gyro bias MEMS INS

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

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 1

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

products details

Low Gyro Bias MEMS INS Inertial Navigation System For Autonomous Driving

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