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Aerospace FOG INS (Merak-A05) for UAV and Aircraft Navigation

Aerospace FOG INS (Merak-A05) for UAV and Aircraft Navigation

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-A05
Highlight:

RS422 fog inertial navigation system

,

strapdown fog inertial navigation system

,

FOG strapdown inertial system

Product Description

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

  • Airborne-grade optical gyroscope for stable inertial measurement
  • Strapdown configuration reduces weight and improves integration efficiency
  • Supports pure inertial and integrated navigation
  • Real-time computation and data output
  • Compatible with multi-source aiding sensors
  • Suitable for UAV platforms with space/power constraints

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() 30μg
Months Scale Factor Accuracy() 30ppm
Gyro Bias Repeatability() ≤0.01°/hr
Scale Factor Accuracy() 30ppm
Random walk() ≤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

 

products
PRODUCTS DETAILS
Aerospace FOG INS (Merak-A05) for UAV and Aircraft Navigation
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-A05
Minimum Order Quantity:
1 set
Price:
$1000-$100000
Delivery Time:
30 work days
Payment Terms:
T/T
Supply Ability:
500 sets per year
Highlight

RS422 fog inertial navigation system

,

strapdown fog inertial navigation system

,

FOG strapdown inertial system

Product Description

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

  • Airborne-grade optical gyroscope for stable inertial measurement
  • Strapdown configuration reduces weight and improves integration efficiency
  • Supports pure inertial and integrated navigation
  • Real-time computation and data output
  • Compatible with multi-source aiding sensors
  • Suitable for UAV platforms with space/power constraints

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() 30μg
Months Scale Factor Accuracy() 30ppm
Gyro Bias Repeatability() ≤0.01°/hr
Scale Factor Accuracy() 30ppm
Random walk() ≤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

 

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