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Dubhe-M1 – Marine RLG Inertial Navigation System Unit

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Dubhe-M1 – Marine RLG Inertial Navigation System Unit

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	100 set per year

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Model Number

Dubhe-M1

Alignment Time:

≤15min

Position Accuracy/Pure Inertia:

≤1nm/1h,CEP

Position Accuracy/INS/DVL Combination:

≤0.3%D,RMS

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed Accuracy/Pure Inertia:

≤1.5kn,RMS

Speed Accuracy/GNSS Combination:

≤0.4kn,RMS

Heading Accuracy/Pure Inertia:

≤0.05°sec(L),RMS

Heading Accuracy/INS/GNSS Combination:

≤0.02°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.02°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.01°,RMS

Dimensions(Lmm×Wmm×Hmm):

195×160×108mm

Weight:

＜3.9kg

Temperature:

-40℃~60℃

Input Voltage:

DC24V(±25%)

Product Description

RLG (Dubhe-90)

The Dubhe-90 Ring Laser Gyroscope (RLG) operates based on the Sagnac effect, measuring angular increments by detecting phase differences between counter-propagating laser beams in a closed glass cavity.

With high integration, excellent reliability, strong environmental adaptability, and stable performance, the Dubhe-90 has become a widely used sensor for high-precision inertial navigation systems (INS).

Applications

Spacecraft
Aircraft
Satellites
Vehicles
Ships
Submersibles
Used for navigation and attitude reference.

Key Features

Monolithic optical and electronic integration for easy installation
Compact and lightweight design with controlled power consumption
High reliability with strong shock and vibration resistance
Wide dynamic response bandwidth with digital output

Series		Inertial Navigation System(INS-M)
Type		Dubhe-M1
Accelerometer	Months Bias Repeatability(1σ)	≤30μg
Accelerometer	Months Scale Factor Accuracy(1σ)	≤30ppm
Gyro	Bias Repeatability(1σ)	≤0.01°/hr
	Scale Factor Accuracy(1σ)	≤10ppm
	Random walk(1σ)	≤0.003°/√hr
Features	Angular Rate	≥±400°/sec
	Angular Acceleration	100000°/sec2
	Acceleration	＞25g
	Angular Attitude	Any Orientation
	Speed accuracy/Pure inertia	≤1.5kn,RMS
	Speed accuracy/GNSS Combination	≤0.4kn,RMS
	Startup time	≤10sec
	Input/output	3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time		≤15min
Position accuracy	Pure inertia	≤1nm/1h,CEP
	INS/DVL Combination	≤0.3%D,RMS
	INS/GNSS Combination	better than GNSS
Heading Accuracy	Pure inertia	≤0.05°sec(L),RMS
Heading Accuracy	Inertia/GNSS Combination	≤0.02°,RMS
Pitch & Roll Accuracy	Pure inertia	≤0.02°,RMS
Pitch & Roll Accuracy	Inertia/GNSS Combination	≤0.01°,RMS
Characteristics	Power consumption	＜20W
	Dimensions(Lmm×Wmm×Hmm)	195×160×108mm
	Weight	＜3.9kg
	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

Products

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	100 set per year

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Model Number

Dubhe-M1

Alignment Time:

≤15min

Position Accuracy/Pure Inertia:

≤1nm/1h,CEP

Position Accuracy/INS/DVL Combination:

≤0.3%D,RMS

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed Accuracy/Pure Inertia:

≤1.5kn,RMS

Speed Accuracy/GNSS Combination:

≤0.4kn,RMS

Heading Accuracy/Pure Inertia:

≤0.05°sec(L),RMS

Heading Accuracy/INS/GNSS Combination:

≤0.02°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.02°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.01°,RMS

Dimensions(Lmm×Wmm×Hmm):

195×160×108mm

Weight:

＜3.9kg

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:

100 set per year

Product Description

RLG (Dubhe-90)

Applications

Spacecraft
Aircraft
Satellites
Vehicles
Ships
Submersibles
Used for navigation and attitude reference.

Key Features

Monolithic optical and electronic integration for easy installation
Compact and lightweight design with controlled power consumption
High reliability with strong shock and vibration resistance
Wide dynamic response bandwidth with digital output

Series		Inertial Navigation System(INS-M)
Type		Dubhe-M1
Accelerometer	Months Bias Repeatability(1σ)	≤30μg
Accelerometer	Months Scale Factor Accuracy(1σ)	≤30ppm
Gyro	Bias Repeatability(1σ)	≤0.01°/hr
	Scale Factor Accuracy(1σ)	≤10ppm
	Random walk(1σ)	≤0.003°/√hr
Features	Angular Rate	≥±400°/sec
	Angular Acceleration	100000°/sec2
	Acceleration	＞25g
	Angular Attitude	Any Orientation
	Speed accuracy/Pure inertia	≤1.5kn,RMS
	Speed accuracy/GNSS Combination	≤0.4kn,RMS
	Startup time	≤10sec
	Input/output	3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time		≤15min
Position accuracy	Pure inertia	≤1nm/1h,CEP
	INS/DVL Combination	≤0.3%D,RMS
	INS/GNSS Combination	better than GNSS
Heading Accuracy	Pure inertia	≤0.05°sec(L),RMS
Heading Accuracy	Inertia/GNSS Combination	≤0.02°,RMS
Pitch & Roll Accuracy	Pure inertia	≤0.02°,RMS
Pitch & Roll Accuracy	Inertia/GNSS Combination	≤0.01°,RMS
Characteristics	Power consumption	＜20W
	Dimensions(Lmm×Wmm×Hmm)	195×160×108mm
	Weight	＜3.9kg
	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

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