PRODUCTS DETAILS

Home > Products >

Merak-H02 Tactical Attitude Heading Reference Unit System AHRS Jamming Resistant

Products

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

Ring Laser Gyroscope

Mr. Sales

18071128027@163.com

+86-18071128027

Contact Now

Merak-H02 Tactical Attitude Heading Reference Unit System AHRS Jamming Resistant

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-H02

Alignment Time:

＜10min

Heading Accuracy/Pure Inertia:

≤0.5°secL+0.1°/1h,RMS

Heading Accuracy/Single-antenna GNSS Combination:

≤0.3°,RMS

Heading Accuracy/Dual-antenna GNSS Combination:

≤0.1°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.1°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.03°,RMS

Dimensions:

100×100×90mm

Weight:

＜1.35kg

Temperature:

-40℃~60℃

Input Voltage:

DC24V(±25%)

Highlight:

Tactical attitude heading reference unit

AHRS attitude heading reference unit

Tactical system ahrs

Product Description

AHRS System (Merak-H02)

This tactical AHRS solution integrates high-performance FOG/RLG technology with precision accelerometers (quartz/MEMS) in a ruggedized strapdown configuration. Engineered for mission-critical applications, the system maintains continuous attitude reference during GNSS outages while providing both processed solutions and raw sensor data. Deployment platforms include: • Combat systems (fire control, EO/IR) • Autonomous vehicles (UGV/USV/UUV) • Naval/maritime systems • Specialized industrial equipment.

Battle-proven characteristics: 1) Jamming-resistant operation; 2) Dual data output modes; 3) Global operability; 4) MIL-SPEC reliability.

Series			Attitude and Heading Reference Systems(AHRS)
Type			Merak-H02
02Accelerometer	Months Bias Repeatability(1σ)		≤100μg
	Months Scale Factor Accuracy(1σ)		≤100ppm
Gyro	Bias Repeatability(1σ)		≤0.03°/hr,1σ
	Scale Factor Accuracy(1σ)		≤100ppm
	Random walk(1σ)		≤0.005°/√hr
Features	Angular Rate		≥±400°/sec
	Angular Acceleration		100000°/sec2
	Acceleration		＞25g
	Angular Attitude		Any Orientation
	Startup time		10 sec
	Input/output		3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time			＜10min
AHRS Applications Performance	Heading Accuracy	Pure inertia	≤0.5°secL+0.1°/h,RMS
		Single-antenna GNSS combination	≤0.3°,RMS
		Dual-antenna GNSS combination	≤0.1°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.1°,RMS
		INS/GNSS combination	≤0.03°,RMS
Characteristics	Power consumption		＜15W
	Dimensions		100×100×90mm
	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-H02

Alignment Time:

＜10min

Heading Accuracy/Pure Inertia:

≤0.5°secL+0.1°/1h,RMS

Heading Accuracy/Single-antenna GNSS Combination:

≤0.3°,RMS

Heading Accuracy/Dual-antenna GNSS Combination:

≤0.1°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.1°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.03°,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

Tactical attitude heading reference unit

AHRS attitude heading reference unit

Tactical system ahrs

Product Description

AHRS System (Merak-H02)

Battle-proven characteristics: 1) Jamming-resistant operation; 2) Dual data output modes; 3) Global operability; 4) MIL-SPEC reliability.

Series			Attitude and Heading Reference Systems(AHRS)
Type			Merak-H02
02Accelerometer	Months Bias Repeatability(1σ)		≤100μg
	Months Scale Factor Accuracy(1σ)		≤100ppm
Gyro	Bias Repeatability(1σ)		≤0.03°/hr,1σ
	Scale Factor Accuracy(1σ)		≤100ppm
	Random walk(1σ)		≤0.005°/√hr
Features	Angular Rate		≥±400°/sec
	Angular Acceleration		100000°/sec2
	Acceleration		＞25g
	Angular Attitude		Any Orientation
	Startup time		10 sec
	Input/output		3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time			＜10min
AHRS Applications Performance	Heading Accuracy	Pure inertia	≤0.5°secL+0.1°/h,RMS
		Single-antenna GNSS combination	≤0.3°,RMS
		Dual-antenna GNSS combination	≤0.1°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.1°,RMS
		INS/GNSS combination	≤0.03°,RMS
Characteristics	Power consumption		＜15W
	Dimensions		100×100×90mm
	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-H02 Tactical Attitude Heading Reference Unit System AHRS Jamming Resistant

Tactical attitude heading reference unit

AHRS attitude heading reference unit

Tactical system ahrs

attitude heading reference system,

system ahrs,

ahrs mems