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AHRS System (Merak-H1)
The Attitude and Heading Reference System (AHRS) employs fiber optic gyros (FOG) or ring laser gyros (RLG) coupled with quartz or MEMS accelerometers in a strapdown inertial architecture. Incorporating advanced navigation algorithms for real-time processing, the system delivers high-precision attitude and heading information through multiple operational modes including GNSS-aided and standalone inertial navigation. Applications include military platforms (radar, optical, acoustic, artillery), robotics, land/sea vehicles, submersibles, and industrial equipment. Key features:
1) Autonomous operation in GNSS-denied environments;
2) Output of both processed navigation data and raw inertial measurements;
3) Worldwide deployment capability;
4) High reliability design.
Series | Attitude and Heading Reference Systems(AHRS) | ||
Type | Merak-H1 | ||
Accelerometer | Months Bias Repeatability(1σ) | ≤30μg | |
Months Scale Factor Accuracy(1σ) | ≤30ppm | ||
Gyro | Bias Repeatability(1σ) | ≤0.005°/hr,1σ | |
Scale Factor Accuracy(1σ) | ≤20ppm | ||
Random walk(1σ) | ≤0.002°/√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 | ≤0.05°secL+0.01°/h,RMS |
Single-antenna GNSS combination | ≤0.02°,RMS | ||
Dual-antenna GNSS combination | ≤0.02°,RMS | ||
Pitch & Roll Accuracy | Pure inertia | ≤0.02°,RMS | |
INS/GNSS combination | ≤0.01°,RMS | ||
Characteristics | Power consumption | <15W | |
Dimensions | 161×153×123mm | ||
Weight | <3.5kg | ||
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 |