| MOQ: | 1 set |
| Price: | $1000-$100000 |
| Delivery Period: | 30 work days |
| Payment Method: | T/T |
| Supply Capacity: | 500 sets per year |
The Merak-A03 is a high-performance aircraft inertial navigation system (INS) designed for UAVs and aerospace platforms. It integrates FOG/RLG gyroscopes and quartz accelerometers in a strapdown configuration. Its real-time fusion center combines inertial data with GNSS, celestial, and other navigation sources, providing accurate and reliable navigation solutions.
Reliable ground and air alignment for precise initialization
Multiple alignment mode selection to support diverse operational requirements
Scalable navigation augmentation for integration with additional sensors
Continuous system monitoring to ensure operational reliability
UAVs and drones
Aerospace platforms
Aircraft navigation systems
| Series | Aerospace Inertial Navigation System(INS-A) | ||
| Type | Merak-A03 | ||
| Accelerometer | Months Bias Repeatability(1σ) | ≤50μg | |
| Months Scale Factor Accuracy(1σ) | ≤50ppm | ||
| Gyro | Bias Repeatability(1σ) | ≤0.02°/hr | |
| Scale Factor Accuracy(1σ) | ≤50ppm | ||
| Random walk(1σ) | ≤0.01°/√hr | ||
| Features | Position Accuracy | Pure inertia | ≤4nm/1h,CEP |
| INS/GNSS combination | better than GNSS | ||
| Speed Accuracy | Pure inertia | ≤3.0m/s,RMS | |
| INS/GNSS combination | ≤0.2m/s,RMS | ||
| Angular Rate | ≥±400°/sec | ||
| Angular Acceleration | 100000°/sec2 | ||
| Acceleration | >25g | ||
| Angular Attitude | Any Orientation | ||
| Input/output | 3 RS422 full-duplex serial ports, 1 100M Ethernet port | ||
| Alignment time | <5min | ||
| AHRS Applications Performance | Heading Accuracy | Pure inertia | ≤0.2°sec(L),RMS |
| INS/GNSS combination | ≤0.1°,RMS | ||
| Pitch & Roll Accuracy | Pure inertia | ≤0.05°,RMS | |
| INS/GNSS combination | ≤0.03°,RMS | ||
| Characteristics | Power consumption | <15W | |
| Dimensions | 110×110×100 | ||
| 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 | ||
| MOQ: | 1 set |
| Price: | $1000-$100000 |
| Delivery Period: | 30 work days |
| Payment Method: | T/T |
| Supply Capacity: | 500 sets per year |
The Merak-A03 is a high-performance aircraft inertial navigation system (INS) designed for UAVs and aerospace platforms. It integrates FOG/RLG gyroscopes and quartz accelerometers in a strapdown configuration. Its real-time fusion center combines inertial data with GNSS, celestial, and other navigation sources, providing accurate and reliable navigation solutions.
Reliable ground and air alignment for precise initialization
Multiple alignment mode selection to support diverse operational requirements
Scalable navigation augmentation for integration with additional sensors
Continuous system monitoring to ensure operational reliability
UAVs and drones
Aerospace platforms
Aircraft navigation systems
| Series | Aerospace Inertial Navigation System(INS-A) | ||
| Type | Merak-A03 | ||
| Accelerometer | Months Bias Repeatability(1σ) | ≤50μg | |
| Months Scale Factor Accuracy(1σ) | ≤50ppm | ||
| Gyro | Bias Repeatability(1σ) | ≤0.02°/hr | |
| Scale Factor Accuracy(1σ) | ≤50ppm | ||
| Random walk(1σ) | ≤0.01°/√hr | ||
| Features | Position Accuracy | Pure inertia | ≤4nm/1h,CEP |
| INS/GNSS combination | better than GNSS | ||
| Speed Accuracy | Pure inertia | ≤3.0m/s,RMS | |
| INS/GNSS combination | ≤0.2m/s,RMS | ||
| Angular Rate | ≥±400°/sec | ||
| Angular Acceleration | 100000°/sec2 | ||
| Acceleration | >25g | ||
| Angular Attitude | Any Orientation | ||
| Input/output | 3 RS422 full-duplex serial ports, 1 100M Ethernet port | ||
| Alignment time | <5min | ||
| AHRS Applications Performance | Heading Accuracy | Pure inertia | ≤0.2°sec(L),RMS |
| INS/GNSS combination | ≤0.1°,RMS | ||
| Pitch & Roll Accuracy | Pure inertia | ≤0.05°,RMS | |
| INS/GNSS combination | ≤0.03°,RMS | ||
| Characteristics | Power consumption | <15W | |
| Dimensions | 110×110×100 | ||
| 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 | ||