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Merak-H01(40S) Fiber Optic AHRS

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A fiber-optic attitude and heading reference system (AHRS) (gyro bias repeatability ≤500μg) with fast startup, RS-422/Ethernet output and extended-temperature operation, suited to demanding navigation and stabilization applications.

Description

A fiber-optic attitude and heading reference system (AHRS) (gyro bias repeatability ≤500μg) with fast startup, RS-422/Ethernet output and extended-temperature operation, suited to demanding navigation and stabilization applications.

The Merak-H01(40S) 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) ≤500μg; Accelerometer Scale Factor Accuracy (monthly, 1σ) ≤500ppm; Gyro Bias Repeatability (1σ) ≤0.15°/hr; Gyro Scale Factor Accuracy (1σ) ≤300ppm; Gyro Accuracy (10 s, 1σ) ≤0.3°/hr; Angular Random Walk (1σ) ≤0.05°/√hr. A companion “Deep Pilot” variant (SD-GZ01) 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): ≤500μg; Accelerometer Scale Factor Accuracy (monthly, 1σ): ≤500ppm; Gyro Bias Repeatability (1σ): ≤0.15°/hr; Gyro Scale Factor Accuracy (1σ): ≤300ppm; Gyro Accuracy (10 s, 1σ): ≤0.3°/hr; Angular Random Walk (1σ): ≤0.05°/√hr.

Specifications

Parameter Value Unit
Accelerometer Bias Repeatability (monthly, 1σ) ≤500μg
Accelerometer Scale Factor Accuracy (monthly, 1σ) ≤500ppm
Gyro Bias Repeatability (1σ) ≤0.15°/hr
Gyro Scale Factor Accuracy (1σ) ≤300ppm
Gyro Accuracy (10 s, 1σ) ≤0.3°/hr
Angular Random Walk (1σ) ≤0.05°/√hr
Angular Rate Range ≥±400°/sec
Angular Acceleration 100000°/s²
Acceleration Range ≥40g
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) ≤1.5°secL+0.3°/h,RMS
ins/single-antenna gnss combination ≤0.5°,RMS
Heading Accuracy (INS/Dual-Antenna GNSS-aided) ≤0.1°,RMS
Pitch & Roll Accuracy (Pure Inertial) ≤0.15°,RMS
Pitch & Roll Accuracy (INS/GNSS-aided) ≤0.1°,RMS
Power Consumption ≤10W
Dimensions (L×W×H, mm) 70×70×53
Weight ≤500g
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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