| 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-A01 Aerospace FOG INS is a compact and high-performance airborne inertial navigation system designed for UAV platforms and special-mission aircraft.
It integrates fiber-optic gyroscopes (FOG/RLG) and quartz accelerometers, supported by advanced navigation algorithms to deliver accurate attitude, velocity, and position outputs under demanding flight conditions.
The system supports multi-source sensor fusion with satellite navigation, barometric altimeters, radio and mission payload sensors, ensuring reliable navigation continuity—even in GNSS-denied or highly dynamic environments.
With rapid alignment capability and robust operational reliability, the Merak-A01 enables precise navigation for tactical, autonomous, and reconnaissance aviation platforms.
Advantages
✓ Miniature Aerospace Form Factor
Compact size supports UAV, eVTOL, and small airborne platforms without compromising accuracy.
✓ FOG + Quartz Accelerometer Architecture
Provides stable long-term bias performance and superior drift resistance.
✓ GNSS-Denied Mission Capability
Maintains inertial navigation continuity in jamming or signal-restricted environments.
✓ Multi-Source Fusion Algorithms
Supports GNSS, altimeter, radio navigation & mission sensors for enhanced total accuracy.
✓ Rapid & Adaptive Alignment
Ground/air alignment, dynamic alignment, and mission-adaptive navigation modes.
✓ High Reliability & Built-In Fault Detection
Ensures mission continuity for aerospace and defense-grade operations.
Application
Suitable for aerospace platforms requiring high-stability inertial navigation:
✔ UAV / UAS Fixed-Wing Platforms
✔ VTOL & eVTOL Aircraft
✔ Special-Mission Aircraft
✔ ISR (Intelligence / Surveillance / Reconnaissance) Systems
✔ Tactical Unmanned Systems
✔ Autonomous Flight & Guidance Control
✔ Payload Stabilization
✔ GNSS-Challenged / GNSS-Denied Flight Missions
| Series | Aerospace Inertial Navigation System(INS-A) | ||
| Type | Merak-A01 | ||
| Accelerometer | Months Bias Repeatability(1σ) | ≤500μg | |
| Months Scale Factor Accuracy(1σ) | ≤500ppm | ||
| Gyro | Bias Repeatability(1σ) | ≤0.1°/hr | |
| Scale Factor Accuracy(1σ) | ≤300ppm | ||
| Random walk(1σ) | ≤0.03°/√hr | ||
| Features | Position Accuracy | Pure inertia | 20m/60s(Ref.),500m/300s(Ref.),CEP |
| INS/GNSS combination | better than satellite accuracy | ||
| Speed Accuracy | Pure inertia | —— | |
| INS/GNSS combination | ≤0.2m/s,RMS | ||
| Angular Rate | ≥±400°/sec | ||
| Angular Acceleration | 100000°/sec2 | ||
| Acceleration | >40g | ||
| Angular Attitude | Any Orientation | ||
| Input/output | 2 RS422 serial ports | ||
| Alignment time | <5min | ||
| AHRS Applications Performance | Heading Accuracy | Pure inertia | ≤1.0°secL+0.2°/h,RMS |
| INS/GNSS combination | ≤0.5°,RMS | ||
| Pitch & Roll Accuracy | Pure inertia | ≤0.2°,RMS | |
| INS/GNSS combination | ≤0.1°,RMS | ||
| Characteristics | Power consumption | <10W | |
| Dimensions(Lmm×Wmm×Hmm) | 70×70×53 | ||
| Weight | <500g | ||
| 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-A01 Aerospace FOG INS is a compact and high-performance airborne inertial navigation system designed for UAV platforms and special-mission aircraft.
It integrates fiber-optic gyroscopes (FOG/RLG) and quartz accelerometers, supported by advanced navigation algorithms to deliver accurate attitude, velocity, and position outputs under demanding flight conditions.
The system supports multi-source sensor fusion with satellite navigation, barometric altimeters, radio and mission payload sensors, ensuring reliable navigation continuity—even in GNSS-denied or highly dynamic environments.
With rapid alignment capability and robust operational reliability, the Merak-A01 enables precise navigation for tactical, autonomous, and reconnaissance aviation platforms.
Advantages
✓ Miniature Aerospace Form Factor
Compact size supports UAV, eVTOL, and small airborne platforms without compromising accuracy.
✓ FOG + Quartz Accelerometer Architecture
Provides stable long-term bias performance and superior drift resistance.
✓ GNSS-Denied Mission Capability
Maintains inertial navigation continuity in jamming or signal-restricted environments.
✓ Multi-Source Fusion Algorithms
Supports GNSS, altimeter, radio navigation & mission sensors for enhanced total accuracy.
✓ Rapid & Adaptive Alignment
Ground/air alignment, dynamic alignment, and mission-adaptive navigation modes.
✓ High Reliability & Built-In Fault Detection
Ensures mission continuity for aerospace and defense-grade operations.
Application
Suitable for aerospace platforms requiring high-stability inertial navigation:
✔ UAV / UAS Fixed-Wing Platforms
✔ VTOL & eVTOL Aircraft
✔ Special-Mission Aircraft
✔ ISR (Intelligence / Surveillance / Reconnaissance) Systems
✔ Tactical Unmanned Systems
✔ Autonomous Flight & Guidance Control
✔ Payload Stabilization
✔ GNSS-Challenged / GNSS-Denied Flight Missions
| Series | Aerospace Inertial Navigation System(INS-A) | ||
| Type | Merak-A01 | ||
| Accelerometer | Months Bias Repeatability(1σ) | ≤500μg | |
| Months Scale Factor Accuracy(1σ) | ≤500ppm | ||
| Gyro | Bias Repeatability(1σ) | ≤0.1°/hr | |
| Scale Factor Accuracy(1σ) | ≤300ppm | ||
| Random walk(1σ) | ≤0.03°/√hr | ||
| Features | Position Accuracy | Pure inertia | 20m/60s(Ref.),500m/300s(Ref.),CEP |
| INS/GNSS combination | better than satellite accuracy | ||
| Speed Accuracy | Pure inertia | —— | |
| INS/GNSS combination | ≤0.2m/s,RMS | ||
| Angular Rate | ≥±400°/sec | ||
| Angular Acceleration | 100000°/sec2 | ||
| Acceleration | >40g | ||
| Angular Attitude | Any Orientation | ||
| Input/output | 2 RS422 serial ports | ||
| Alignment time | <5min | ||
| AHRS Applications Performance | Heading Accuracy | Pure inertia | ≤1.0°secL+0.2°/h,RMS |
| INS/GNSS combination | ≤0.5°,RMS | ||
| Pitch & Roll Accuracy | Pure inertia | ≤0.2°,RMS | |
| INS/GNSS combination | ≤0.1°,RMS | ||
| Characteristics | Power consumption | <10W | |
| Dimensions(Lmm×Wmm×Hmm) | 70×70×53 | ||
| Weight | <500g | ||
| 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 | ||