| MOQ: | 1 set |
| Price: | $1000-$100000 |
| Delivery Period: | 30 work days |
| Payment Method: | T/T |
| Supply Capacity: | 500 sets per year |
The Merak-A02 is a high-performance, compact airborne inertial navigation system (INS) designed for UAVs and specialized aircraft. It integrates FOG/RLG gyroscopes and quartz accelerometers in a strapdown configuration. The system’s real-time fusion center combines inertial data with GNSS, celestial navigation, and other data sources, providing accurate and reliable navigation solutions.
Reliable ground and air alignment for precise initialization
Multiple alignment mode selection to meet diverse operational requirements
Scalable navigation augmentation for integrating additional sensors or data sources
Continuous system monitoring to ensure operational reliability
The Merak-A02 FOG INS delivers high-precision, real-time navigation data in a compact form factor, making it ideal for UAVs, drones, and small aircraft platforms.
| Series | Aerospace Inertial Navigation System(INS-A) | ||
| Type | Merak-A02 | ||
| Accelerometer | Months Bias Repeatability(1σ) | ≤100μg | |
| Months Scale Factor Accuracy(1σ) | ≤100ppm | ||
| Gyro | Bias Repeatability(1σ) | ≤0.05°/hr | |
| Scale Factor Accuracy(1σ) | ≤100ppm | ||
| Random walk(1σ) | ≤0.02°/√hr | ||
| Features | Position Accuracy | Pure inertia | 5m/60s(Ref.),150m/300s(Ref.),CEP |
| INS/GNSS combination | better than GNSS | ||
| Speed Accuracy | Pure inertia | —— | |
| 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 | ≤0.5°secL+0.1°/h,RMS |
| INS/GNSS combination | ≤0.3°,RMS | ||
| Pitch & Roll Accuracy | Pure inertia | ≤0.1°,RMS | |
| INS/GNSS combination | ≤0.05°,RMS | ||
| Characteristics | Power consumption | <15W | |
| Dimensions | 100×100×90 | ||
| Weight | <1.35kg | ||
| 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-A02 is a high-performance, compact airborne inertial navigation system (INS) designed for UAVs and specialized aircraft. It integrates FOG/RLG gyroscopes and quartz accelerometers in a strapdown configuration. The system’s real-time fusion center combines inertial data with GNSS, celestial navigation, and other data sources, providing accurate and reliable navigation solutions.
Reliable ground and air alignment for precise initialization
Multiple alignment mode selection to meet diverse operational requirements
Scalable navigation augmentation for integrating additional sensors or data sources
Continuous system monitoring to ensure operational reliability
The Merak-A02 FOG INS delivers high-precision, real-time navigation data in a compact form factor, making it ideal for UAVs, drones, and small aircraft platforms.
| Series | Aerospace Inertial Navigation System(INS-A) | ||
| Type | Merak-A02 | ||
| Accelerometer | Months Bias Repeatability(1σ) | ≤100μg | |
| Months Scale Factor Accuracy(1σ) | ≤100ppm | ||
| Gyro | Bias Repeatability(1σ) | ≤0.05°/hr | |
| Scale Factor Accuracy(1σ) | ≤100ppm | ||
| Random walk(1σ) | ≤0.02°/√hr | ||
| Features | Position Accuracy | Pure inertia | 5m/60s(Ref.),150m/300s(Ref.),CEP |
| INS/GNSS combination | better than GNSS | ||
| Speed Accuracy | Pure inertia | —— | |
| 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 | ≤0.5°secL+0.1°/h,RMS |
| INS/GNSS combination | ≤0.3°,RMS | ||
| Pitch & Roll Accuracy | Pure inertia | ≤0.1°,RMS | |
| INS/GNSS combination | ≤0.05°,RMS | ||
| Characteristics | Power consumption | <15W | |
| Dimensions | 100×100×90 | ||
| Weight | <1.35kg | ||
| 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 | ||