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Merak-H03 Tactical Attitude Heading Reference Unit System AHRS Jamming Resistant

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Merak-H03 Tactical Attitude Heading Reference Unit System AHRS Jamming Resistant

Brand Name : Star & Inertia Technology

Model Number : Merak-H03

Place of Origin : China

MOQ : 1 set

Price : $1000-$100000

Payment Terms : T/T

Supply Ability : 500 sets per year

Delivery Time : 30 work days

Alignment time : ＜10min

Heading Accuracy/Pure inertia : ≤0.2°secL+0.04°/1h,RMS

Heading Accuracy/Single-antenna GNSS combination : ≤0.1°,RMS

Heading Accuracy/Dual-antenna GNSS combination : ≤0.1°,RMS

Pitch & Roll Accuracy/Pure inertia : ≤0.05°,RMS

Pitch & Roll Accuracy/INS/GNSS combination : ≤0.02°,RMS

Dimensions : 110×110×100mm

Weight : ＜1.7kg

Temperature : -40℃~60℃

Input Voltage : DC24V(±25%)

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AHRS System (Merak-H03)


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-H03
Accelerometer Months Bias Repeatability(1σ) ≤50μg
Months Scale Factor Accuracy(1σ) ≤50ppm
Gyro Bias Repeatability(1σ) ≤0.02°/hr,1σ
Scale Factor Accuracy(1σ) ≤50ppm
Random walk(1σ) ≤0.004°/√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 ≤0.2°secL+0.04°/h,RMS
Single-antenna GNSS combination ≤0.1°,RMS
Dual-antenna GNSS combination ≤0.1°,RMS
Pitch & Roll Accuracy Pure inertia ≤0.05°,RMS
INS/GNSS combination ≤0.02°,RMS
Characteristics Power consumption ＜15W
Dimensions 110×110×100mm
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:

Tactical aircraft inertial reference system

      

AHRS aircraft inertial reference system

      

AHRS inertial reference unit

      
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