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High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI

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High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI

Name: High Accuracy Inertial Navigation System ThreeAxis MEMS Gyro GI300FA0DGI
Brand: AVIC
Price: 1 USD

Brand Name : AVIC

Model Number : GI300F-A0-DGI

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 : INS with GNSS

Gyro range : ±400°/s

Gyro Zero bias stability : ≤0.3°/h

Accelerometer range : ±20g

Accelerometer Zero bias stability : ≤100µg

Voltage : 9-36V DC

Interface : 2 RS 232,1-RS 422,1- PPS

Operating temperature : -40℃~+60℃

Storage temperature : -45℃~+70℃

Life span : > 15 years

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High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI

Product Description

The fiber optic integrated navigation system GI300F-A0-DGI consists of a cost-effective three-axis closed-loop fiber optic gyroscope, accelerometer, and navigation board card. It is implemented through multi-sensor fusion and navigation calculation algorithms, meeting the precise measurement requirements for attitude, heading, and position information in applications such as high-precision mobile measurement systems and medium to large unmanned aerial vehicles.

Main Function

The system has inertial/satellite integrated navigation mode and pure inertial mode.
In the inertial/satellite integrated navigation mode, the satellite positioning information received by the internal GNSS receiver can be used for integrated navigation, and the pitch, roll, course, position, speed, time and other information of the carrier can be output; After the signal is lost, the position, velocity and attitude of the inertial solution are output, in which the pitch and roll are required to be kept accurate, with a certain course keeping function in a short time and meter-level positioning accuracy in a short time.
After the pure inertial mode (that is, GPS fusion has never been performed after power-on, and if it loses lock again after fusion, it belongs to the integrated navigation mode) is started, it has accurate attitude measurement function, can output the pitch and roll heading, and the pure inertial mode can find the north statically.

Index Parameter

Project	Test conditions	Indicators
Positioning accuracy	GNSS Valid, Single Point	1.5m
	GNSS Valid, RT K	2cm+1ppm
	Pure inertial horizontal positioning holding	80m/5min(CEP)
		500m/10min(CEP)
		1.5nm/30min(CEP)
	Horizontal positioning holding accuracy	0.8nm/30min (CEP)
Heading accuracy	Single antenna (RMS)	0.1°
	Dual Antenna (RMS)	0.2 °/L (L = baseline length) (RMS)
	Course Keeping (RMS)	0.2°/30min(RMS),0.5°/h
	Self-north seeking accuracy (RMS)	0.2 ° SecL,15 min
	Self-north seeking accuracy (RMS)	1.0 ° SecL, 5-10 min
Attitude accuracy	GNSS is valid	0.02°(RMS)
Attitude accuracy	Attitude hold (GNSS failure)	0.2°/30min(RMS),0.5°/h(RMS)
Speed accuracy	GNSS valid, single point L1/L2	0.1m/s(RMS)
Gyroscope	Measuring range	±400°/s
Gyroscope	Zero bias stability	≤0.3°/h
Accelerometer	Measuring range	±20g
Accelerometer	Zero bias stability	≤100µg
Physical dimensions and electrical characteristics	Voltage	9-36V DC
	Power consumption	≤ 12W (steady state)
	Interface	2 RS 232,1-RS 422,1- PPS
	Dimension/LWH/mm	92.0 92.090.0
	Weight	≤1.0kg
Environmental characteristics	Operating temperature	-40℃~+60℃
	Storage temperature	-45℃~+70℃
	Vibration	5 ~ 2000Hz, 6.06 G
	Impact	30g, 11 ms (with shock)
	Life span	> 15 years
	Continuons operating hours	> 24 hours

Dimensions

High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI

L92.0mm x W92.0 mm x H90.0mm(L x W x H)

High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI

Product Tags:

GI300F-A0-DGI Inertial Navigation System

High Accuracy Inertial Navigation System

High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI Images

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