Merak-H1(98S) Fiber Optic AHRS

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A fiber-optic attitude and heading reference system (AHRS) (gyro bias repeatability ≤30μg) with fast startup, RS-422/Ethernet output and extended-temperature operation, suited to demanding navigation and stabilization applications.

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A fiber-optic attitude and heading reference system (AHRS) (gyro bias repeatability ≤30μg) with fast startup, RS-422/Ethernet output and extended-temperature operation, suited to demanding navigation and stabilization applications.

The Merak-H1(98S) Fiber Optic AHRS is a fiber-optic attitude and heading reference system (AHRS) from the Merak civil AHRS series. It combines a high-precision fiber optic gyroscope triad with quartz flexible accelerometers in a strapdown architecture, and outputs attitude, heading and inertial data over serial and Ethernet interfaces. The unit delivers a dynamic range of at least ±400°/s with excellent bias stability and low angular random walk. Key performance figures include Accelerometer Bias Repeatability (monthly, 1σ) ≤30μg; Accelerometer Scale Factor Accuracy (monthly, 1σ) ≤30ppm; Gyro Bias Repeatability (1σ) ≤0.005°/hr; Gyro Scale Factor Accuracy (1σ) ≤20ppm; Gyro Accuracy (10 s, 1σ) ≤0.01°/hr; Angular Random Walk (1σ) ≤0.001°/√hr. A companion “Deep Pilot” variant (SD-GZ1) with the same specifications is also available. Electrical interfacing is provided through high-speed serial or Ethernet links with fast startup, and the unit operates over an extended industrial temperature range with high MTBF for long-endurance missions. Typical applications include guns, lasers, sonars, cannons and other military equipment platforms, as well as unmanned surface vessels and industrial attitude-measurement systems that require a continuous, GPS-independent attitude reference. All specifications below are taken directly from the manufacturer’s 2026 catalog and datasheet.

Key specifications: Accelerometer Bias Repeatability (monthly, 1σ): ≤30μg; Accelerometer Scale Factor Accuracy (monthly, 1σ): ≤30ppm; Gyro Bias Repeatability (1σ): ≤0.005°/hr; Gyro Scale Factor Accuracy (1σ): ≤20ppm; Gyro Accuracy (10 s, 1σ): ≤0.01°/hr; Angular Random Walk (1σ): ≤0.001°/√hr.

Specifications

Parameter Value Unit
Accelerometer Bias Repeatability (monthly, 1σ) ≤30μg
Accelerometer Scale Factor Accuracy (monthly, 1σ) ≤30ppm
Gyro Bias Repeatability (1σ) ≤0.005°/hr
Gyro Scale Factor Accuracy (1σ) ≤20ppm
Gyro Accuracy (10 s, 1σ) ≤0.01°/hr
Angular Random Walk (1σ) ≤0.001°/√hr
Angular Rate Range ≥±400°/sec
Angular Acceleration 100000°/s²
Acceleration Range ≥25g
Attitude Any Orientation
Startup Time 10 sec
Input/Output Interface 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment Time ≤10min
Heading Accuracy (Pure Inertial) ≤0.05°secL+0.01°/h,RMS
ins/single-antenna gnss combination ≤0.02°,RMS
Heading Accuracy (INS/Dual-Antenna GNSS-aided) ≤0.02°,RMS
Pitch & Roll Accuracy (Pure Inertial) ≤0.02°,RMS
Pitch & Roll Accuracy (INS/GNSS-aided) ≤0.01°,RMS
Power Consumption ≤15W
Dimensions (L×W×H, mm) 188×188×124
Weight ≤4.5kg
Operating Temperature -40°C~60°C
Shock 15g, Half-sine wave 11ms
Input Voltage DC24V(±25%)
Cooling Conduction to mounting plate
Vibration 20~2000Hz,6.06g
MTBF ≥20000 hours

All specifications are taken from the manufacturer’s current datasheet.

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