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Dubhe-A20 – RLG INS Inertial Integrated Navigation System | Vibration-Resistant Aerospace INS for Drones

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Dubhe-A20 – RLG INS Inertial Integrated Navigation System | Vibration-Resistant Aerospace INS for Drones

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

Wuhan Deep Pilot Technology Co.,Ltd.

Model Number

Dubhe-A20

Alignment Time:

≤30min

Position Accuracy/Pure Inertia:

≤1nm/20h,CEP

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed accuracy/Pure Inertia:

≤1.0m/s,RMS

Speed accuracy/INS/GNSS Combination:

≤0.2m/s,RMS

Heading Accuracy/Pure Inertia:

≤0.02°sec(L),RMS

Heading Accuracy/INS/GNSS Combination:

≤0.01°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.015°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.01°,RMS

Dimensions:

232×186×160mm

Weight:

＜8.2kg

Input Voltage:

DC24V(±25%)

Temperature:

-40℃~60℃

Shock:

15g，Half-sine Wave 11ms

Product Description

The Dubhe-A20 is a high-performance airborne optical inertial navigation system (INS) designed for modern UAVs and airborne platforms. It integrates FOG/RLG gyroscopes and quartz accelerometers in an optimized strapdown architecture. The system’s fusion engine combines GNSS, celestial, and other navigation data while maintaining pure inertial navigation capability, delivering accurate and reliable positioning and attitude information.

Applications

UAVs and drones
Modern airborne platforms
Aerospace navigation systems

Key Features

Vibration-resistant alignment for stable navigation in dynamic environments
Flexible alignment options to support various mission profiles
Expandable sensor integration for additional navigation sources
Built-in system diagnostics for reliable operation and maintenance

Series			Aerospace Inertial Navigation System(INS-A)
Type			Dubhe-A20
Accelerometer	Months Bias Repeatability(1σ)		≤10μg
	Months Scale Factor Accuracy(1σ)		≤10ppm
Gyro	Bias Repeatability(1σ)		≤0.008°/hr
	Scale Factor Accuracy(1σ)		≤10ppm
	Random walk(1σ)		≤0.003°/√hr
Features	Position Accuracy	Pure inertia	≤1nm/20h,CEP
		INS/GNSS combination	better than GNSS
	Speed Accuracy	Pure inertia	≤1.0 m/s,RMS
		INS/GNSS combination	≤0.2m/s,RMS
	Angular Rate		≥±400°/sec
	Angular Acceleration		100000°/sec2
	Acceleration		＞25g
	Angular Attitude		Any Orientation
	Alignment time		≤30min
	Input/output		3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time	Time		＜30min
AHRS Applications Performance	Heading Accuracy	Pure inertia	≤0.02°sec(L),RMS
		INS/GNSS combination	≤0.01°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.015°,RMS
		INS/GNSS combination	≤0.01°,RMS
Characteristics	Power consumption		＜40W
	Dimensions		232×186×160
	Weight		＜8.2kg
	Temperature		-40℃~60℃
	Shock		15g,Half-sine wave 11ms
	Input Voltage		DC24V(±25%)
	cooling		Conduction to mounting plate
	Vibration		20~2000Hz,6.06g
	MTBF		＞10000 hours

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PRODUCTS DETAILS

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

Wuhan Deep Pilot Technology Co.,Ltd.

Model Number

Dubhe-A20

Alignment Time:

≤30min

Position Accuracy/Pure Inertia:

≤1nm/20h,CEP

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed accuracy/Pure Inertia:

≤1.0m/s,RMS

Speed accuracy/INS/GNSS Combination:

≤0.2m/s,RMS

Heading Accuracy/Pure Inertia:

≤0.02°sec(L),RMS

Heading Accuracy/INS/GNSS Combination:

≤0.01°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.015°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.01°,RMS

Dimensions:

232×186×160mm

Weight:

＜8.2kg

Input Voltage:

DC24V(±25%)

Temperature:

-40℃~60℃

Shock:

15g，Half-sine Wave 11ms

Minimum Order Quantity:

1 set

Price:

$1000-$100000

Delivery Time:

30 work days

Payment Terms:

T/T

Supply Ability:

500 sets per year

Product Description

Applications

UAVs and drones
Modern airborne platforms
Aerospace navigation systems

Key Features

Vibration-resistant alignment for stable navigation in dynamic environments
Flexible alignment options to support various mission profiles
Expandable sensor integration for additional navigation sources
Built-in system diagnostics for reliable operation and maintenance

Series			Aerospace Inertial Navigation System(INS-A)
Type			Dubhe-A20
Accelerometer	Months Bias Repeatability(1σ)		≤10μg
	Months Scale Factor Accuracy(1σ)		≤10ppm
Gyro	Bias Repeatability(1σ)		≤0.008°/hr
	Scale Factor Accuracy(1σ)		≤10ppm
	Random walk(1σ)		≤0.003°/√hr
Features	Position Accuracy	Pure inertia	≤1nm/20h,CEP
		INS/GNSS combination	better than GNSS
	Speed Accuracy	Pure inertia	≤1.0 m/s,RMS
		INS/GNSS combination	≤0.2m/s,RMS
	Angular Rate		≥±400°/sec
	Angular Acceleration		100000°/sec2
	Acceleration		＞25g
	Angular Attitude		Any Orientation
	Alignment time		≤30min
	Input/output		3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time	Time		＜30min
AHRS Applications Performance	Heading Accuracy	Pure inertia	≤0.02°sec(L),RMS
		INS/GNSS combination	≤0.01°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.015°,RMS
		INS/GNSS combination	≤0.01°,RMS
Characteristics	Power consumption		＜40W
	Dimensions		232×186×160
	Weight		＜8.2kg
	Temperature		-40℃~60℃
	Shock		15g,Half-sine wave 11ms
	Input Voltage		DC24V(±25%)
	cooling		Conduction to mounting plate
	Vibration		20~2000Hz,6.06g
	MTBF		＞10000 hours

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