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Inertial Navigation System

High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology

Name: High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: GI100E-A0-DGI
Price: 5,000.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	GI100E-A0-DGI
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 Accelerometer

Heading Accuracy:

0.1deg (rms)

Attitude Accuracy:

0.1deg (rms)

Horizontal Velocity Accuracy:

0.1m/s

Gyro Range:

±500°/s

Gyro Zero Bias Stability:

4°/h

Accelerometer Range:

±16g

Accelerometer Zero Bias Stability:

0.2mg

Communication Interface:

RS-422/RS-232

Weight:

≤150g

Packaging Details:

sponge+carton

Supply Ability:

500/month

Highlight:

High heading accuracy Integrated Navigation System

Satellite Navigation Integrated Navigation System

MEMS Integrated Navigation System

Product Description

High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology

Product Description

The GI100E-A0-DGI integrated navigation system has built-in high-performance MEMS gyroscope and accelerometer, which can receive internal GNSS data, realize multi-sensor fusion and integrated navigation solution algorithm, and have short-term inertial navigation capability when GNSS is invalid.

The product has high reliability and strong environmental adaptability. By matching different software, the products can be widely used in the fields of tactical and industrial unmanned aerial vehicles, unmanned vehicles, unmanned ships, aviation guided bombs, intelligent ammunition, rockets, mobile communication, mapping, seeker and stable platform.

Technical indicators

Project		Metrics (RMS)	Remark
Heading accuracy	GNSS Valid ^①	0.1°
Heading accuracy	Course holding	0.2°/min	GNSS failure
Attitude accuracy	GNSS is valid	0.1°	Single-point L1/L2, RTK
Attitude accuracy	Attitude maintenance	0.2°/min	GNSS failure
Positioning accuracy	Horizontal, GNSS valid; RTK	1.5m；1cm+1ppm	Single point L1/L2; Differential
	Elevation, GNSS valid; RTK	2.5m；2cm+1ppm	Single point L1/L2; Differential
	Position keeping, GNSS failure	20m	Unlocked for 60s
Horizontal velocity accuracy	GNSS is valid	0.1m/s	Single-point L1/L2, RTK
Gyroscope	Measuring range	±500°/s
Gyroscope	Zero bias stability	4°/h	Allan variance
Accelerometer	Measuring range	±16g	Customizable 200 G
Accelerometer	Zero bias stability	0.2mg	Allan variance
Satellite card	Cold start	< 30 seconds	Open environment
	Hot start	5 seconds	Open environment
	Type of receiver	BDS B1I/B2I/B3I
		GPS L1C/A/L2P (Y)/L2C/L5
		GLONASS G1/G2
		Galileo E1/E5a/E5b
		QZSS L1/L2/L5
Communication interface	RS232	Route 2
Communication interface	RS422	Route 1
Electrical characteristics	Voltage	9~36VDC
	Power consumption	≤3W
	Ripple	100 mV	P-P
Structural characteristics	Size	80 mm×53 mm×23mm
Structural characteristics	Weight	≤150g
Use environment	Operating temperature	-40℃~+60℃
	Storage temperature	-45℃~+65℃
	Vibration	20~2000Hz,6.06g
	Impact	30g,11ms
	Degree of protection	IP65
Reliability	MTBF	30000h
	Life span	> 15 years
	Continuous working time	>24h

Main Features

The integrated navigation system can carry out integrated navigation by using the satellite navigation information received internally, and output the pitch, roll, course, position, speed, time and other information of the carrier; After losing the satellite signal, it outputs the position, velocity and attitude information of inertial solution, and has a certain navigation accuracy maintenance function in a short time.

Product Dimensions

High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology 0

L80mm x W53mm x H23mm(L x W x H)

High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology 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

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High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology

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