INT

INT-A12(50T) Celestial RLG Inertial Positioning System Inertial Navigation System For Drones




INT-A12(50T) Celestial RLG Inertial Positioning System Inertial Navigation System For Drones

Detail Information
Place of Origin
China
Brand Name
INT
Model Number:                                   INT-A12(50T)
Alignment Time:
≤5min
Position Accuracy/Pure Inertia:
≤1.0nm/1h,CEP
Position Accuracy/INS/GNSS Combination:
Better Than GNSS
Speed ​​accuracy/Pure Inertia:
≤1.2m/s,RMS
Speed ​​accuracy/INS/GNSS Combination:
≤0.2m/s,RMS
Heading Accuracy/Pure Inertia:
≤0.05°sec(L),RMS
Heading Accuracy/INS/GNSS Combination:
≤0.03°,RMS
Pitch & Roll Accuracy/Pure Inertia:
≤0.03°,RMS
Pitch & Roll Accuracy/INS/GNSS Combination:
≤0.015°,RMS
Dimensions:
185×156×136mm
Weight:
<7kg
Temperature:
-40℃~60℃
Input Voltage:
DC24V(±25%)
Highlight:

Celestial inertial positioning system

,

RLG inertial positioning system

,

RLG inertial navigation system for drones

Product Description

    Aerospace RLG INS(INT-A12(50T)


The airborne optical gyro INS utilizes FOG/RLG gyroscopes and quartz accelerometers as core sensors, adopting strapdown or modulated architecture. Its high-speed navigation computer runs advanced algorithms to provide real-time navigation solutions. The system supports multiple operational modes including pure inertial and multi-source fusion (GNSS, celestial, altimeter, radio, and vision), delivering complete navigation parameters.


    Applications include fixed-wing UAVs, rotary-wing UAVs, and special aircraft.

    Key features:

    1) Ground sway base/airborne alignment capability;

    2) Switchable alignment modes (self/transfer/moving base);

    3) Multi-source navigation fusion;

    4) Fault detection and alarm functions.

 SeriesAerospace Inertial Navigation System(INS-A)
TypeINT-A12(50T)
AccelerometerMonths Bias Repeatability()30μg
Months Scale Factor Accuracy()30ppm
GyroBias Repeatability()≤0.008°/hr
Scale Factor Accuracy()10ppm
Random walk()≤0.003°/√hr
FeaturesPosition AccuracyPure inertia1.0nm/1h,CEP
INS/GNSS combinationbetter than GNSS
Speed AccuracyPure inertia1.2m/s,RMS
INS/GNSS combination0.2m/s,RMS
Angular Rate≥±400°/sec
Angular Acceleration100000°/sec2
Acceleration>25g
Angular Attitude Any Orientation
Input/output3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time5min
AHRS Applications PerformanceHeading AccuracyPure inertia0.05°sec(L),RMS
INS/GNSS combination0.03°,RMS
Pitch & Roll AccuracyPure inertia0.03°,RMS
INS/GNSS combination0.015°,RMS
CharacteristicsPower consumption<20W
Dimensions185×156×136
Weight<7kg
Temperature -40℃~60℃
Shock15g,Half-sine wave 11ms
Input VoltageDC24V(±25%)
coolingConduction to mounting plate
Vibration 20~2000Hz,6.06g
MTBF>20000 hours
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