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Merak-A03 GNSS Strapdown Aircraft Inertial Navigation System FOG INS

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Merak-A03 GNSS Strapdown Aircraft Inertial Navigation System FOG INS

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-A03

Alignment Time:

≤5min

Position Accuracy/Pure Inertia:

≤4nm/1h,CEP

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed accuracy/Pure Inertia:

≤3.0m/s,RMS

Speed accuracy/INS/GNSS Combination:

≤0.2m/s,RMS

Heading Accuracy/Pure Inertia:

≤0.2°sec(L),RMS

Heading Accuracy/INS/GNSS Combination:

≤0.1°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.05°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.03°,RMS

Dimensions:

110×110×100mm

Weight:

＜1.7kg

Temperature:

-40℃~60℃

Input Voltage:

DC24V(±25%)

Highlight:

FOG INS Fiber Optic Inertial Navigation System

GNSS Fiber Optic Inertial Navigation System

GNSS Aided fog inertial navigation system

Product Description

Aerospace FOG INS(Merak-A03)

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-A03
Accelerometer	Months Bias Repeatability(1σ)		≤50μg
	Months Scale Factor Accuracy(1σ)		≤50ppm
Gyro	Bias Repeatability(1σ)		≤0.02°/hr
	Scale Factor Accuracy(1σ)		≤50ppm
	Random walk(1σ)		≤0.01°/√hr
Features	Position Accuracy	Pure inertia	≤4nm/1h,CEP
		INS/GNSS combination	better than GNSS
	Speed Accuracy	Pure inertia	≤3.0m/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	≤0.2°sec(L),RMS
		INS/GNSS combination	≤0.1°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.05°,RMS
		INS/GNSS combination	≤0.03°,RMS
Characteristics	Power consumption		＜15W
	Dimensions		110×110×100
	Weight		＜1.7kg
	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-A03

Alignment Time:

≤5min

Position Accuracy/Pure Inertia:

≤4nm/1h,CEP

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed accuracy/Pure Inertia:

≤3.0m/s,RMS

Speed accuracy/INS/GNSS Combination:

≤0.2m/s,RMS

Heading Accuracy/Pure Inertia:

≤0.2°sec(L),RMS

Heading Accuracy/INS/GNSS Combination:

≤0.1°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.05°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.03°,RMS

Dimensions:

110×110×100mm

Weight:

＜1.7kg

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

FOG INS Fiber Optic Inertial Navigation System

GNSS Fiber Optic Inertial Navigation System

GNSS Aided fog inertial navigation system

Product Description

Aerospace FOG INS(Merak-A03)

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-A03
Accelerometer	Months Bias Repeatability(1σ)		≤50μg
	Months Scale Factor Accuracy(1σ)		≤50ppm
Gyro	Bias Repeatability(1σ)		≤0.02°/hr
	Scale Factor Accuracy(1σ)		≤50ppm
	Random walk(1σ)		≤0.01°/√hr
Features	Position Accuracy	Pure inertia	≤4nm/1h,CEP
		INS/GNSS combination	better than GNSS
	Speed Accuracy	Pure inertia	≤3.0m/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	≤0.2°sec(L),RMS
		INS/GNSS combination	≤0.1°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.05°,RMS
		INS/GNSS combination	≤0.03°,RMS
Characteristics	Power consumption		＜15W
	Dimensions		110×110×100
	Weight		＜1.7kg
	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:

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