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Merak-A05 Optical Gyroscope Aircraft Inertial Navigation System | Drone & UAV FOG INS 2000Hz

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Merak-A05 Optical Gyroscope Aircraft Inertial Navigation System | Drone & UAV FOG INS 2000Hz

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-A05

Alignment Time:

≤5min

Position Accuracy/Pure Inertia:

≤2nm/1h,CEP

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed accuracy/Pure Inertia:

≤1.5m/s,RMS

Speed accuracy/INS/GNSS Combination:

≤0.2m/s,RMS

Heading Accuracy/Pure Inertia:

≤0.1°sec(L),RMS

Heading Accuracy/INS/GNSS Combination:

≤0.05°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.03°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.02°,RMS

Dimensions:

130×130×110mm

Weight:

＜2.2kg

Temperature:

-40℃~60℃

Input Voltage:

DC24V(±25%)

Product Description

The Merak-A05 Optical Gyroscope Inertial Navigation System (INS) is designed for aircraft and UAV applications, providing precise and reliable navigation performance. Using optical gyroscopes and quartz accelerometers as core sensors, the system employs advanced strapdown and modulation technology. It processes navigation data internally at high speeds, delivering real-time navigation information to the carrier.

This INS series supports integration with multiple navigation sources, including satellite, astronomical, altimeter, radio, and visual data, offering both pure inertial and multi-source information fusion modes. Users can access comprehensive and accurate navigation information tailored to their operational needs.

Applications:

Unmanned Aerial Vehicles (UAVs)
Special-purpose aircraft

Key Capabilities:

Ground and air alignment
Alignment mode switching
Multi-sensor fusion
Fault detection

Series			Aerospace Inertial Navigation System(INS-A)
Type			Merak-A05
Accelerometer	Months Bias Repeatability(1σ)		≤30μg
	Months Scale Factor Accuracy(1σ)		≤30ppm
Gyro	Bias Repeatability(1σ)		≤0.01°/hr
	Scale Factor Accuracy(1σ)		≤30ppm
	Random walk(1σ)		≤0.005°/√hr
Features	Position Accuracy	Pure inertia	≤2nm/1h,CEP
		INS/GNSS combination	better than GNSS
	Speed Accuracy	Pure inertia	≤1.5m/s,RMS
		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	≤0.1°sec(L),RMS
		INS/GNSS combination	≤0.05°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.03°,RMS
		INS/GNSS combination	≤0.02°,RMS
Characteristics	Power consumption		＜15W
	Dimensions		130×130×110
	Weight		＜2.2kg
	Temperature		-40℃~60℃
	Shock		15g,Half-sine wave 11ms
	Input Voltage		DC24V(±25%)
	cooling		Conduction to mounting plate
	Vibration		20~2000Hz,6.06g
	MTBF		＞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-A05

Alignment Time:

≤5min

Position Accuracy/Pure Inertia:

≤2nm/1h,CEP

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed accuracy/Pure Inertia:

≤1.5m/s,RMS

Speed accuracy/INS/GNSS Combination:

≤0.2m/s,RMS

Heading Accuracy/Pure Inertia:

≤0.1°sec(L),RMS

Heading Accuracy/INS/GNSS Combination:

≤0.05°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.03°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.02°,RMS

Dimensions:

130×130×110mm

Weight:

＜2.2kg

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

Applications:

Unmanned Aerial Vehicles (UAVs)
Special-purpose aircraft

Key Capabilities:

Ground and air alignment
Alignment mode switching
Multi-sensor fusion
Fault detection

Series			Aerospace Inertial Navigation System(INS-A)
Type			Merak-A05
Accelerometer	Months Bias Repeatability(1σ)		≤30μg
	Months Scale Factor Accuracy(1σ)		≤30ppm
Gyro	Bias Repeatability(1σ)		≤0.01°/hr
	Scale Factor Accuracy(1σ)		≤30ppm
	Random walk(1σ)		≤0.005°/√hr
Features	Position Accuracy	Pure inertia	≤2nm/1h,CEP
		INS/GNSS combination	better than GNSS
	Speed Accuracy	Pure inertia	≤1.5m/s,RMS
		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	≤0.1°sec(L),RMS
		INS/GNSS combination	≤0.05°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.03°,RMS
		INS/GNSS combination	≤0.02°,RMS
Characteristics	Power consumption		＜15W
	Dimensions		130×130×110
	Weight		＜2.2kg
	Temperature		-40℃~60℃
	Shock		15g,Half-sine wave 11ms
	Input Voltage		DC24V(±25%)
	cooling		Conduction to mounting plate
	Vibration		20~2000Hz,6.06g
	MTBF		＞20000 hours

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