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Merak-A05 Optical Gyroscope Aircraft Inertial Navigation System Drone UAVs 2000Hz

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Merak-A05 Optical Gyroscope Aircraft Inertial Navigation System Drone UAVs 2000Hz

Brand Name : Star & Inertia Technology

Model Number : Merak-A05

Place of Origin : China

MOQ : 1 set

Price : $1000-$100000

Payment Terms : T/T

Supply Ability : 500 sets per year

Delivery Time : 30 work days

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%)

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Aerospace FOG INS(Merak-A05)

The airborne optical gyro inertial navigation system uses optical gyroscopes and quartz accelerometers as core sensors, employing strapdown or modulation technology systems. It operates advanced navigation software at high speeds internally, calculating and outputting navigation information in real-time. This series of products can integrate navigation information from satellites, astronomy, altimeters, radio, vision, etc., according to user needs, supporting pure inertial and multi-source information fusion working modes, providing users with comprehensive navigation information for the carrier.

Applications: UAVs and special aircraft.

Capabilities:

1) Ground/air alignment;

2) Alignment mode switching;

3) Sensor fusion;

4) Fault detection.

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


Product Tags:

RS422 fog inertial navigation system

      

strapdown fog inertial navigation system

      

FOG strapdown inertial system

      
China Merak-A05 Optical Gyroscope Aircraft Inertial Navigation System Drone UAVs 2000Hz factory

Merak-A05 Optical Gyroscope Aircraft Inertial Navigation System Drone UAVs 2000Hz Images

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