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Merak-A01 – Commercial RS422 FOG Inertial Navigation System (INS, Small) for Aircraft and Drones | Aerospace FOG INS

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Merak-A01 – Commercial RS422 FOG Inertial Navigation System (INS, Small) for Aircraft and Drones | Aerospace FOG INS

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

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Model Number

Merak-A01

Alignment Time:

≤5min

Position Accuracy/Pure Inertia:

20m/60s(Ref.),500m/300s(Ref.),CEP

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed accuracy/Pure Inertia:

Speed accuracy/INS/GNSS Combination:

≤0.2m/s

Heading Accuracy/Pure Inertia:

≤1.0°secL+0.2°/h,RMS

Heading Accuracy/INS/GNSS Combination:

≤0.5°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.2°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.1°,RMS

Dimensions:

70×70×53mm

Weight:

＜500g

Temperature:

-40℃~60℃

Input Voltage:

DC24V(±25%)

Product Description

The Merak-A01 is a compact, high-performance airborne inertial navigation system (INS) designed for UAVs and special aircraft. It integrates fiber optic gyroscopes (FOG/RLG) and quartz accelerometers with advanced navigation fusion algorithms, providing accurate and reliable real-time navigation solutions.

System Capabilities

Challenging environment alignment for precise initialization in difficult conditions
Mission-adaptive alignment methods to support diverse operational requirements
Multi-source navigation enhancement for integration of additional sensors and data
Operational reliability assurance for continuous, dependable navigation

Applications

UAVs and drones
Special aircraft
Aerospace navigation platforms

Series			Aerospace Inertial Navigation System(INS-A)
Type			Merak-A01
Accelerometer	Months Bias Repeatability(1σ)		≤500μg
	Months Scale Factor Accuracy(1σ)		≤500ppm
Gyro	Bias Repeatability(1σ)		≤0.1°/hr
	Scale Factor Accuracy(1σ)		≤300ppm
	Random walk(1σ)		≤0.03°/√hr
Features	Position Accuracy	Pure inertia	20m/60s(Ref.),500m/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		＞40g
	Angular Attitude		Any Orientation
	Input/output		2 RS422 serial ports
Alignment time			＜5min
AHRS Applications Performance	Heading Accuracy	Pure inertia	≤1.0°secL+0.2°/h,RMS
		INS/GNSS combination	≤0.5°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.2°,RMS
		INS/GNSS combination	≤0.1°,RMS
Characteristics	Power consumption		＜10W
	Dimensions		70×70×53
	Weight		＜500g
	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,L/C
Supply Capacity:	500 sets per year

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Model Number

Merak-A01

Alignment Time:

≤5min

Position Accuracy/Pure Inertia:

20m/60s(Ref.),500m/300s(Ref.),CEP

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed accuracy/Pure Inertia:

Speed accuracy/INS/GNSS Combination:

≤0.2m/s

Heading Accuracy/Pure Inertia:

≤1.0°secL+0.2°/h,RMS

Heading Accuracy/INS/GNSS Combination:

≤0.5°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.2°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.1°,RMS

Dimensions:

70×70×53mm

Weight:

＜500g

Temperature:

-40℃~60℃

Input Voltage:

DC24V(±25%)

Minimum Order Quantity:

1 set

Price:

$1000-$100000

Delivery Time:

30 work days

Payment Terms:

T/T,L/C

Supply Ability:

500 sets per year

Product Description

System Capabilities

Challenging environment alignment for precise initialization in difficult conditions
Mission-adaptive alignment methods to support diverse operational requirements
Multi-source navigation enhancement for integration of additional sensors and data
Operational reliability assurance for continuous, dependable navigation

Applications

UAVs and drones
Special aircraft
Aerospace navigation platforms

Series			Aerospace Inertial Navigation System(INS-A)
Type			Merak-A01
Accelerometer	Months Bias Repeatability(1σ)		≤500μg
	Months Scale Factor Accuracy(1σ)		≤500ppm
Gyro	Bias Repeatability(1σ)		≤0.1°/hr
	Scale Factor Accuracy(1σ)		≤300ppm
	Random walk(1σ)		≤0.03°/√hr
Features	Position Accuracy	Pure inertia	20m/60s(Ref.),500m/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		＞40g
	Angular Attitude		Any Orientation
	Input/output		2 RS422 serial ports
Alignment time			＜5min
AHRS Applications Performance	Heading Accuracy	Pure inertia	≤1.0°secL+0.2°/h,RMS
		INS/GNSS combination	≤0.5°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.2°,RMS
		INS/GNSS combination	≤0.1°,RMS
Characteristics	Power consumption		＜10W
	Dimensions		70×70×53
	Weight		＜500g
	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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