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Merak-A02 GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL

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Merak-A02 GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL

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

Details Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

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%)

Highlight:

GNSS ins inertial navigation system

SMALL ins inertial navigation system

SMALL inertial navigation unit

Product Description

Aerospace FOG INS(Merak-A02)

Delivering exceptional navigation performance, this optical INS employs FOG/RLG gyros and quartz accelerometers in strapdown configuration. The real-time fusion center combines inertial data with GNSS, celestial and other sources.

Key advantages for UAV applications:

1) Reliable ground/air alignment;

2) Multiple alignment mode selection;

3) Scalable navigation augmentation;

4) Continuous system monitoring.

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

Tags:

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

Star & Inertia Technology

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

Highlight

GNSS ins inertial navigation system

SMALL ins inertial navigation system

SMALL inertial navigation unit

Product Description

Aerospace FOG INS(Merak-A02)

Key advantages for UAV applications:

1) Reliable ground/air alignment;

2) Multiple alignment mode selection;

3) Scalable navigation augmentation;

4) Continuous system monitoring.

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

Tags:

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Ring Laser Gyroscope

Merak-A02 GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL

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