| MOQ: | 1 set |
| Price: | $1000-$100000 |
| Delivery Period: | 30 work days |
| Payment Method: | T/T |
| Supply Capacity: | 500 sets per year |
Product Description
The Merak-A05 is an airborne fiber-optic inertial navigation system (FOG-INS) designed for UAVs and special aircraft. It utilizes optical gyroscopes and quartz accelerometers as core inertial sensors and adopts a strapdown architecture.
The system runs high-speed internal navigation software to compute and output real-time inertial navigation data, including attitude, heading, velocity, and position.
According to user requirements, the Merak-A05 supports pure inertial navigation as well as multi-sensor integrated navigation, enabling fusion with GNSS, altimeters, radio navigation, vision, and other external aiding sources.
Key Advantages
Applications
✔ Unmanned Aerial Vehicles (UAVs)
✔ Special-purpose aircraft (e.g., survey, research, and tasks requiring stabilized navigation)
These platforms benefit from high-quality inertial data during flight where accurate position, attitude, and heading information is required.
| Series | Aerospace Inertial Navigation System(INS-A) | ||
| Type | Merak-A05 | ||
| Accelerometer | Months Bias Repeatability(1σ) | ≤30μg | |
| Months Scale Factor Accuracy(1σ) | ≤30ppm | ||
| Gyro | Bias Repeatability(1σ) | ≤0.01°/hr | |
| Scale Factor Accuracy(1σ) | ≤30ppm | ||
| Random walk(1σ) | ≤0.005°/√hr | ||
| Features | Position Accuracy | Pure inertia | ≤2nm/1h,CEP |
| INS/GNSS combination | better than satellite accuracy | ||
| Speed Accuracy | Pure inertia | ≤1.5m/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 | ≤0.1°sec(L),RMS |
| INS/GNSS combination | ≤0.05°,RMS | ||
| Pitch & Roll Accuracy | Pure inertia | ≤0.03°,RMS | |
| INS/GNSS combination | ≤0.02°,RMS | ||
| Characteristics | Power consumption | <15W | |
| Dimensions(Lmm×Wmm×Hmm) | 130×130×110 | ||
| Weight | <2.2kg | ||
| 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 |
Product Description
The Merak-A05 is an airborne fiber-optic inertial navigation system (FOG-INS) designed for UAVs and special aircraft. It utilizes optical gyroscopes and quartz accelerometers as core inertial sensors and adopts a strapdown architecture.
The system runs high-speed internal navigation software to compute and output real-time inertial navigation data, including attitude, heading, velocity, and position.
According to user requirements, the Merak-A05 supports pure inertial navigation as well as multi-sensor integrated navigation, enabling fusion with GNSS, altimeters, radio navigation, vision, and other external aiding sources.
Key Advantages
Applications
✔ Unmanned Aerial Vehicles (UAVs)
✔ Special-purpose aircraft (e.g., survey, research, and tasks requiring stabilized navigation)
These platforms benefit from high-quality inertial data during flight where accurate position, attitude, and heading information is required.
| Series | Aerospace Inertial Navigation System(INS-A) | ||
| Type | Merak-A05 | ||
| Accelerometer | Months Bias Repeatability(1σ) | ≤30μg | |
| Months Scale Factor Accuracy(1σ) | ≤30ppm | ||
| Gyro | Bias Repeatability(1σ) | ≤0.01°/hr | |
| Scale Factor Accuracy(1σ) | ≤30ppm | ||
| Random walk(1σ) | ≤0.005°/√hr | ||
| Features | Position Accuracy | Pure inertia | ≤2nm/1h,CEP |
| INS/GNSS combination | better than satellite accuracy | ||
| Speed Accuracy | Pure inertia | ≤1.5m/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 | ≤0.1°sec(L),RMS |
| INS/GNSS combination | ≤0.05°,RMS | ||
| Pitch & Roll Accuracy | Pure inertia | ≤0.03°,RMS | |
| INS/GNSS combination | ≤0.02°,RMS | ||
| Characteristics | Power consumption | <15W | |
| Dimensions(Lmm×Wmm×Hmm) | 130×130×110 | ||
| Weight | <2.2kg | ||
| 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 | ||