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Merak-L04(70SR2) FOG Orientation and Positioning System (INS-L)

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A vehicle-mounted FOG orientation and positioning system (gyro bias repeatability ≤30μg) with fast startup, RS-422/Ethernet output and extended-temperature operation, suited to demanding navigation and stabilization applications.

Description

A vehicle-mounted FOG orientation and positioning system (gyro bias repeatability ≤30μg) with fast startup, RS-422/Ethernet output and extended-temperature operation, suited to demanding navigation and stabilization applications.

The Merak-L04(70SR2) FOG Orientation and Positioning System (INS-L) is a fiber optic gyroscope (FOG) orientation and positioning system (INS-L) from the Merak series, designed for vehicle-mounted north-finding, orientation and positioning. It combines a fiber optic gyroscope triad with quartz flexible accelerometers and supports both static and moving-base alignment. 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) ≤0.02°/hr; Gyro Scale Factor Accuracy (1σ) ≤30ppm; Gyro Accuracy (10 s, 1σ) ≤0.05°/hr; Angular Random Walk (1σ) ≤0.005°/√hr. A companion “Deep Pilot” variant (SD-GL04) 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 ground vehicles, tanks, self-propelled artillery and other vehicle-mounted platforms that require rapid orientation, heading keeping and positioning, optionally aided by GNSS or an odometer. 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): ≤0.02°/hr; Gyro Scale Factor Accuracy (1σ): ≤30ppm; Gyro Accuracy (10 s, 1σ): ≤0.05°/hr; Angular Random Walk (1σ): ≤0.005°/√hr.

Specifications

Parameter Value Unit
Accelerometer Bias Repeatability (monthly, 1σ) ≤30μg
Accelerometer Scale Factor Accuracy (monthly, 1σ) ≤30ppm
Gyro Bias Repeatability (1σ) ≤0.02°/hr
Gyro Scale Factor Accuracy (1σ) ≤30ppm
Gyro Accuracy (10 s, 1σ) ≤0.05°/hr
Angular Random Walk (1σ) ≤0.005°/√hr
Angular Rate Range ≥±400°/sec
Angular Acceleration 100000°/s²
Acceleration Range ≥25g
Attitude Any Orientation
Input/Output Interface 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment Time ≤5min
Position Error (10 min zero-speed correction / 2 h) ≤40m,CEP
Position Accuracy (INS/Odometer-aided) ≤1.0%D,RMS
Position Accuracy (INS/GNSS-aided) better than satellite accuracy
North-Finding / Orientation Accuracy ≤5.0mil,RMS
Heading Keeping Accuracy (2 h) ≤3.0mil,RMS
Heading Accuracy (INS/GNSS-aided) ≤3.0mil,RMS
Pitch & Roll Accuracy ≤1.0mil,RMS
Power Consumption ≤15W
Dimensions (L×W×H, mm) 130×130×100
Weight ≤2.2kg
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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