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Merak-A05 – Optical Gyroscope Aircraft Inertial Navigation System (FOG INS)
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Merak-A05 – Optical Gyroscope Aircraft Inertial Navigation System (FOG INS)
  • name

Merak-A05 – Optical Gyroscope Aircraft Inertial Navigation System (FOG INS)

MOQ: 1 set
Price: $1000-$100000
Delivery Period: 30 work days
Payment Method: T/T
Supply Capacity: 500 sets per year
Detail Information
Product Description
Detail Information
Place of Origin
China
Brand Name
Wuhan Deep Pilot Technology Co.,Ltd.
Model Number
Merak-A05
Alignment Time:
≤5min
Position Accuracy/Pure Inertia:
≤2nm/1h,CEP
Position Accuracy/INS/GNSS Combination:
Better Than GNSS
Speed ​​accuracy/Pure Inertia:
≤1.5m/s,RMS
Speed ​​accuracy/INS/GNSS Combination:
≤0.2m/s,RMS
Heading Accuracy/Pure Inertia:
≤0.1°sec(L),RMS
Heading Accuracy/INS/GNSS Combination:
≤0.05°,RMS
Pitch & Roll Accuracy/Pure Inertia:
≤0.03°,RMS
Pitch & Roll Accuracy/INS/GNSS Combination:
≤0.02°,RMS
Dimensions:
130×130×110mm
Weight:
＜2.2kg
Temperature:
-40℃~60℃
Input Voltage:
DC24V(±25%)
Product Description

The Merak-A05 Optical Gyroscope Inertial Navigation System is an airborne INS designed for aircraft, drones, and UAV applications. It uses optical gyroscopes and quartz accelerometers as core sensors and adopts strapdown or modulation technology architectures to provide stable and reliable inertial navigation performance.

An internal high-speed navigation computer runs advanced navigation software to process sensor data and output real-time navigation information. According to user requirements, the system can integrate navigation information from satellites, astronomy, altimeters, radio, and vision, supporting both pure inertial operation and multi-source information fusion modes. This enables the system to deliver comprehensive navigation information for airborne platforms.

Applications

  • UAVs

  • Special aircraft

Capabilities

  • Ground and air alignment

  • Alignment mode switching

  • Sensor fusion

  • Fault detection

The Merak-A05 Aerospace FOG INS provides reliable real-time navigation data and flexible working modes, meeting the operational needs of modern airborne and unmanned platforms.

 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 GNSS
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 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


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products
PRODUCTS DETAILS
Products

Ring Laser Gyroscope

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Portable UUV

Laser
Merak-A05 – Optical Gyroscope Aircraft Inertial Navigation System (FOG INS)
  • name
Merak-A05 – Optical Gyroscope Aircraft Inertial Navigation System (FOG INS)
MOQ: 1 set
Price: $1000-$100000
Delivery Period: 30 work days
Payment Method: T/T
Supply Capacity: 500 sets per year
Detail Information
Product Description
Detail Information
Place of Origin
China
Brand Name
Wuhan Deep Pilot Technology Co.,Ltd.
Model Number
Merak-A05
Alignment Time:
≤5min
Position Accuracy/Pure Inertia:
≤2nm/1h,CEP
Position Accuracy/INS/GNSS Combination:
Better Than GNSS
Speed ​​accuracy/Pure Inertia:
≤1.5m/s,RMS
Speed ​​accuracy/INS/GNSS Combination:
≤0.2m/s,RMS
Heading Accuracy/Pure Inertia:
≤0.1°sec(L),RMS
Heading Accuracy/INS/GNSS Combination:
≤0.05°,RMS
Pitch & Roll Accuracy/Pure Inertia:
≤0.03°,RMS
Pitch & Roll Accuracy/INS/GNSS Combination:
≤0.02°,RMS
Dimensions:
130×130×110mm
Weight:
＜2.2kg
Temperature:
-40℃~60℃
Input Voltage:
DC24V(±25%)
Minimum Order Quantity:
1 set
Price:
$1000-$100000
Delivery Time:
30 work days
Payment Terms:
T/T
Supply Ability:
500 sets per year
Product Description

The Merak-A05 Optical Gyroscope Inertial Navigation System is an airborne INS designed for aircraft, drones, and UAV applications. It uses optical gyroscopes and quartz accelerometers as core sensors and adopts strapdown or modulation technology architectures to provide stable and reliable inertial navigation performance.

An internal high-speed navigation computer runs advanced navigation software to process sensor data and output real-time navigation information. According to user requirements, the system can integrate navigation information from satellites, astronomy, altimeters, radio, and vision, supporting both pure inertial operation and multi-source information fusion modes. This enables the system to deliver comprehensive navigation information for airborne platforms.

Applications

  • UAVs

  • Special aircraft

Capabilities

  • Ground and air alignment

  • Alignment mode switching

  • Sensor fusion

  • Fault detection

The Merak-A05 Aerospace FOG INS provides reliable real-time navigation data and flexible working modes, meeting the operational needs of modern airborne and unmanned platforms.

 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 GNSS
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 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


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15827090628
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