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Dubhe-L4 Tactical Ring Laser Gyro Based Inertial Navigation System Guidance Unit 24V

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Dubhe-L4 Tactical Ring Laser Gyro Based Inertial Navigation System Guidance Unit 24V

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	500 sets per year

Details Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Model Number

Dubhe-L4

Alignment Time:

≤8min

Position Accuracy/10min Zero Speed Correction:

Position Accuracy/INS/Odometer Combination:

≤0.1%D,RMS

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Heading Accuracy/North Finding/orientation Accuracy:

≤0.5mil,RMS

Heading Bearing Keeping Accuracy/2h:

≤0.5mil,RMS

Heading Accuracy/INS/GNSS Combination:

≤0.3mil,RMS

Pitch & Roll Accuracy:

≤0.2mil,RMS

Dimensions:

232×186×160mm

Weight:

Temperature:

-40℃~60℃

Input Voltage:

DC24V(±25%)

Highlight:

24V ring laser gyro based inertial navigation system

ring laser gyro based inertial navigation system

Tactical inertial guidance system

Product Description

Land RLG INS (Dubhe-L4)

This tactical-grade vehicular navigation system features RLG/FOG technology with quartz accelerometers in a ruggedized strapdown configuration. Providing continuous positioning through ZUPT and sensor fusion, it ensures operational capability in extreme conditions (-65° latitude to Arctic environments).

Deployment platforms include: Main battle tanks, self-propelled guns, IFVs, and unmanned systems.

Battlefield features:

1) Rapid alignment;

2) GNSS-denied navigation;

3) Extreme climate operation;

4) EMI-hardened reliability.

Series			Land Inertial Navigation System(INS-L)
Type			Dubhe-L4
Accelerometer	Months Bias Repeatability(1σ)		≤10μg
	Months Scale Factor Accuracy(1σ)		≤10ppm
Gyro	Bias Repeatability(1σ)		≤0.003°/h
	Scale Factor Accuracy(1σ)		≤5ppm
	Random walk(1σ)		≤0.001°/√hr
Features	Angular Rate		≥±400°/sec
	Angular Acceleration		100000°/sec2
	Acceleration		＞25g
	Angular Attitude		Any Orientation
	Input/output		3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time			≤8min
Position accuracy	10min zero speed correction		≤7m,CEP
	INS/Odometer combination		≤0.1%D,RMS
	INS/GNSS combination		better than GNSS
AHRS Applications Performance	Heading Accuracy	North finding/orientation accuracy	≤0.5mil,RMS
		Heading bearing keeping accuracy/2h	≤0.5mil,RMS
		INS/GNSS combination	≤0.3mil,RMS
	Pitch & Roll Accuracy		≤0.2mil,RMS
Characteristics	Power consumption		＜30W
	Dimensions		232×186×160mm
	Weight		＜8kg
	Temperature		-40℃~60℃
	Shock		15g,Half-sine wave 11ms
	Input Voltage		DC24V(±25%)
	cooling		Conduction to mounting plate
	Vibration		20~2000Hz,6.06g
	MTBF		＞20000 hours

Tags:

Products

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	500 sets per year

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Model Number

Dubhe-L4

Alignment Time:

≤8min

Position Accuracy/10min Zero Speed Correction:

≤7m

Position Accuracy/INS/Odometer Combination:

≤0.1%D,RMS

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Heading Accuracy/North Finding/orientation Accuracy:

≤0.5mil,RMS

Heading Bearing Keeping Accuracy/2h:

≤0.5mil,RMS

Heading Accuracy/INS/GNSS Combination:

≤0.3mil,RMS

Pitch & Roll Accuracy:

≤0.2mil,RMS

Dimensions:

232×186×160mm

Weight:

＜8kg

Temperature:

-40℃~60℃

Input Voltage:

DC24V(±25%)

Minimum Order Quantity:

1 set

Price:

$1000-$100000

Delivery Time:

30 work days

Payment Terms:

T/T

Supply Ability:

500 sets per year

Highlight

24V ring laser gyro based inertial navigation system

ring laser gyro based inertial navigation system

Tactical inertial guidance system

Product Description

Land RLG INS (Dubhe-L4)

Deployment platforms include: Main battle tanks, self-propelled guns, IFVs, and unmanned systems.

Battlefield features:

1) Rapid alignment;

2) GNSS-denied navigation;

3) Extreme climate operation;

4) EMI-hardened reliability.

Series			Land Inertial Navigation System(INS-L)
Type			Dubhe-L4
Accelerometer	Months Bias Repeatability(1σ)		≤10μg
	Months Scale Factor Accuracy(1σ)		≤10ppm
Gyro	Bias Repeatability(1σ)		≤0.003°/h
	Scale Factor Accuracy(1σ)		≤5ppm
	Random walk(1σ)		≤0.001°/√hr
Features	Angular Rate		≥±400°/sec
	Angular Acceleration		100000°/sec2
	Acceleration		＞25g
	Angular Attitude		Any Orientation
	Input/output		3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time			≤8min
Position accuracy	10min zero speed correction		≤7m,CEP
	INS/Odometer combination		≤0.1%D,RMS
	INS/GNSS combination		better than GNSS
AHRS Applications Performance	Heading Accuracy	North finding/orientation accuracy	≤0.5mil,RMS
		Heading bearing keeping accuracy/2h	≤0.5mil,RMS
		INS/GNSS combination	≤0.3mil,RMS
	Pitch & Roll Accuracy		≤0.2mil,RMS
Characteristics	Power consumption		＜30W
	Dimensions		232×186×160mm
	Weight		＜8kg
	Temperature		-40℃~60℃
	Shock		15g,Half-sine wave 11ms
	Input Voltage		DC24V(±25%)
	cooling		Conduction to mounting plate
	Vibration		20~2000Hz,6.06g
	MTBF		＞20000 hours

Tags:

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Ring Laser Gyroscope

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