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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

Name: MerakA03 GNSS Strapdown Aircraft Inertial Navigation System FOG INS
Brand: Star & Inertia Technology
Price: 1000 USD

Brand Name : Star & Inertia Technology

Model Number : Merak-A03

Place of Origin : China

MOQ : 1 set

Supply Ability : 500 sets per year

Delivery Time : 30 work days

Payment Terms : T/T

Price : $1000-$100000

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%)

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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

Product Tags:

GNSS Aircraft Inertial Navigation System

strapdown Aircraft Inertial Navigation System

OEM ins system in aircraft

Merak-A03 GNSS Strapdown Aircraft Inertial Navigation System FOG INS Images

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