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Merak-A02 – GNSS Strapdown Aircraft Inertial Navigation System (FOG INS, Small) | Aerospace FOG INS

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Merak-A02 – GNSS Strapdown Aircraft Inertial Navigation System (FOG INS, Small) | Aerospace FOG INS

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

Merak-A02

Alignment Time:

≤5min

Position Accuracy/Pure Inertia:

5m/60s(Ref.),150m/300s(Ref.),CEP

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed accuracy/Pure Inertia:

Speed accuracy/INS/GNSS Combination:

≤0.2m/s,RMS

Heading Accuracy/Pure Inertia:

≤0.5°secL+0.1°/h,RMS

Heading Accuracy/INS/GNSS Combination:

≤0.3°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.1°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.05°,RMS

Dimensions:

100×100×90mm

Weight:

＜1.35kg

Temperature:

-40℃~60℃

Input Voltage:

DC24V(±25%)

Product Description

The Merak-A02 is a compact, high-performance aircraft inertial navigation system (INS) designed for UAVs and small aircraft platforms. It integrates FOG/RLG gyroscopes and quartz accelerometers in a strapdown configuration. The system’s real-time fusion center combines inertial data with GNSS, celestial, and other navigation sources, delivering accurate and reliable navigation solutions.

Key Advantages for UAV Applications

Reliable ground and air alignment for precise initialization
Multiple alignment mode selection to support diverse mission requirements
Scalable navigation augmentation for integration with additional sensors
Continuous system monitoring to ensure operational reliability

Applications

UAVs and drones
Small aircraft platforms
Aerospace navigation systems

Series			Aerospace Inertial Navigation System(INS-A)
Type			Merak-A02
Accelerometer	Months Bias Repeatability(1σ)		≤100μg
	Months Scale Factor Accuracy(1σ)		≤100ppm
Gyro	Bias Repeatability(1σ)		≤0.05°/hr
	Scale Factor Accuracy(1σ)		≤100ppm
	Random walk(1σ)		≤0.02°/√hr
Features	Position Accuracy	Pure inertia	5m/60s(Ref.),150m/300s(Ref.),CEP
		INS/GNSS combination	better than GNSS
	Speed Accuracy	Pure inertia	——
		INS/GNSS combination	≤0.2m/s,RMS
	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			＜5min
AHRS Applications Performance	Heading Accuracy	Pure inertia	≤0.5°secL+0.1°/h,RMS
		INS/GNSS combination	≤0.3°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.1°,RMS
		INS/GNSS combination	≤0.05°,RMS
Characteristics	Power consumption		＜15W
	Dimensions		100×100×90
	Weight		＜1.35kg
	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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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

Merak-A02

Alignment Time:

≤5min

Position Accuracy/Pure Inertia:

5m/60s(Ref.),150m/300s(Ref.),CEP

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed accuracy/Pure Inertia:

——

Speed accuracy/INS/GNSS Combination:

≤0.2m/s,RMS

Heading Accuracy/Pure Inertia:

≤0.5°secL+0.1°/h,RMS

Heading Accuracy/INS/GNSS Combination:

≤0.3°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.1°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.05°,RMS

Dimensions:

100×100×90mm

Weight:

＜1.35kg

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

Product Description

Key Advantages for UAV Applications

Reliable ground and air alignment for precise initialization
Multiple alignment mode selection to support diverse mission requirements
Scalable navigation augmentation for integration with additional sensors
Continuous system monitoring to ensure operational reliability

Applications

UAVs and drones
Small aircraft platforms
Aerospace navigation systems

Series			Aerospace Inertial Navigation System(INS-A)
Type			Merak-A02
Accelerometer	Months Bias Repeatability(1σ)		≤100μg
	Months Scale Factor Accuracy(1σ)		≤100ppm
Gyro	Bias Repeatability(1σ)		≤0.05°/hr
	Scale Factor Accuracy(1σ)		≤100ppm
	Random walk(1σ)		≤0.02°/√hr
Features	Position Accuracy	Pure inertia	5m/60s(Ref.),150m/300s(Ref.),CEP
		INS/GNSS combination	better than GNSS
	Speed Accuracy	Pure inertia	——
		INS/GNSS combination	≤0.2m/s,RMS
	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			＜5min
AHRS Applications Performance	Heading Accuracy	Pure inertia	≤0.5°secL+0.1°/h,RMS
		INS/GNSS combination	≤0.3°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.1°,RMS
		INS/GNSS combination	≤0.05°,RMS
Characteristics	Power consumption		＜15W
	Dimensions		100×100×90
	Weight		＜1.35kg
	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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Key Advantages for UAV Applications

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