Inertial Navigation System High Performance North Seeking Mems Gyroscope

• Type: Inertial Navigation
• Output Signal Type: Digital Output
• Measuring Shaft Quantities: Three
• Accuracy Grade: 0.1deg
• IP Rating: IP67
• Certification: CE
• Model NO.: GI100E-A0-DGI
• Customized: Customized
• Heading Accuracy: 0.1deg
• Attitude Accuracy: 0.1deg (RMS)
• Gyro Range: ±500°/S
• Gyro Zero Bias Stability: 4°/H
• Horizontal Velocity Accuracy: 0.1m/S
• Acc Range: ±16g
• Accelerometer Zero Bias Stability: 0.2mg
• Communication Interface: RS-422/RS-232
• Voltage: 9~36V
• Mtbf: 30000h
• Power Consumption: ≤3W
• Vibration: 20~2000Hz
• Weight: ≤150g
• Transport Package: Sponge and Box
• Specification: 80mm*53mm*23mm
• Trademark: AVIC
• Origin: China
• Production Capacity: 500/Month

Product Description

Inertial navigation system High Performance North Seeking MEMS Gyroscope
 

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.

 

Product Parameters

  

Project		Metrics (RMS)	Remark
Heading accuracy	GNSS Valid	0.1°
	Course holding	0.2°/min	GNSS failure
Attitude accuracy	GNSS is valid	0.1°	Single-point L1/L2, RTK
	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
	Zero bias stability	4°/h	Allan variance
Accelerometer	Measuring range	±16g	Customizable 200 G
	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
	RS422	Route 1
Electrical characteristics	Voltage	9~36VDC
	Power consumption	≤3W
	Ripple	100 mV	P-P
Structural characteristics	Size	80 mm×53 mm×23mm
	Weight	≤150g
Use environment	Operating temperature	-40ºC~+60ºC
	Storage temperature	-45ºC~+65ºC
	Vibration	20~2000Hz,6.06g
	Impact	30g,11ms
	Degree of protection	IP65
Reliability	MTBF	30000h
	Life span	> 15 years
	Continuous working time	>24h

Product Structure

  

Product Display

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.

Main Application Fields

 

 

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