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Aerospace Fiber Optic Gyro INS– Miniature Airborne Inertial Navigation System for UAV & Special Aircraft

Aerospace Fiber Optic Gyro INS– Miniature Airborne Inertial Navigation System for UAV & Special Aircraft

MOQ: 1 set
Price: $1000-$100000
Delivery Period: 30 work days
Payment Method: T/T
Supply Capacity: 500 sets per year
Detail Information
Place of Origin
China
Brand Name
Star & Inertia Technology
Model Number
Merak-A01
Highlight:

INS Fiber Optic Inertial Navigation System

,

RS422 Fiber Optic Inertial Navigation System

,

Half sine wave fog ins

Product Description

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() ≤500μg
Months Scale Factor Accuracy() ≤500ppm
Gyro Bias Repeatability() ≤0.1°/hr
Scale Factor Accuracy() ≤300ppm
Random walk() ≤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


products
PRODUCTS DETAILS
Aerospace Fiber Optic Gyro INS– Miniature Airborne Inertial Navigation System for UAV & Special Aircraft
MOQ: 1 set
Price: $1000-$100000
Delivery Period: 30 work days
Payment Method: T/T
Supply Capacity: 500 sets per year
Detail Information
Place of Origin
China
Brand Name
Star & Inertia Technology
Model Number
Merak-A01
Minimum Order Quantity:
1 set
Price:
$1000-$100000
Delivery Time:
30 work days
Payment Terms:
T/T
Supply Ability:
500 sets per year
Highlight

INS Fiber Optic Inertial Navigation System

,

RS422 Fiber Optic Inertial Navigation System

,

Half sine wave fog ins

Product Description

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() ≤500μg
Months Scale Factor Accuracy() ≤500ppm
Gyro Bias Repeatability() ≤0.1°/hr
Scale Factor Accuracy() ≤300ppm
Random walk() ≤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


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