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Fiber Optic GNSS Integrated Inertial Navigation System Gyroscope Sensors Attitude

Categories Inertial Navigation System
Brand Name: Firepower
Model Number: GI500-A0
Certification: CE ROHS
Place of Origin: CHINA
MOQ: 1
Price: negotiable
Supply Ability: 100/month
Delivery Time: 15 days for sample
Packaging Details: sponge+box
Payment Terms: T/T
Product name: INS Navigation System
Positioning accuracy: 1.5nm/h
Heading accuracy: 0.1°
Attitude accuracy: 0.03°
Speed accuracy: 0.1m/s(RMS)
Gyro scope: ±400°/s
Gyro Zero bias stability: ≤0.02°/h
Accelerometer range: ±20g
Accelerometer Zero bias stability: ≤50µg
Working temperature: -40℃~+60℃
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Fiber Optic GNSS Integrated Inertial Navigation System Gyroscope Sensors Attitude

Fiber optic GNSS integrated inertial navigation system gyroscope sensors Attitude


Product Description


The GI500-A0 fiber optic integrated navigation system is based on high-precision closed-loop fiber optic gyroscopes, accelerometers, and high-end GNSS receiving boards. It is implemented through multi-sensor fusion and navigation calculation algorithms, providing high-precision heading, velocity, and position information to the outside world, meeting the requirements of high-precision measurement and control.


Main application areas


Large scale unmanned aerial vehicle reference inertial navigation

Ship Compass

Self propelled artillery orientation

Vehicle positioning and orientation

High precision mobile measurement

High precision stable platform


Product features


The system has inertial/satellite integrated navigation mode and pure inertial mode.

Inertial navigation has a built-in GNSS board. When GNSS is effective, inertial navigation can combine with GNSS for navigation and provide users with combined navigation parameters such as position, altitude, velocity, attitude, heading, acceleration, angular velocity, etc. At the same time, it outputs GNSS position, altitude, velocity, and other information.

When GNSS is ineffective, it can enter pure inertial mode (i.e. GPS fusion has never been performed after power on, and if the fusion is lost again, it belongs to integrated navigation mode). After activation, it has precise attitude measurement function, can output pitch and roll heading, and pure inertial can static seek north.


Technical indicators

ItemsTest ConditionsA0-IndicatorsB0-Indicators
Positioning accuracyGNSSValid, single point1.2m(RMS)1.2m(RMS)
GNSSValid,RTK2cm+1ppm(RMS)2cm+1ppm(RMS)
Position holding (GNSS failure)1.5nm/h(50%CEP),5nm/2h(50%CEP)0.8nm/h(CEP),3.0nm/3h(CEP)
Heading accuracyNorth-seekingit self

0.1°×sec(Lati),

*Lati:latitude (RMS),10min

0.06°×sec(Lati),Static base 5min alignment;

0.03°×sec(Lati),Static base 5min alignment;*Lati:latitude (RMS)

Course keeping (GNSS failure)0.05°/h(RMS),0.1°/2h(RMS)0.02°/h(RMS),0.05°/3h(RMS)
Attitude accuracyGNSS Valid0.03°(RMS)0.01°(RMS)
Attitude holding (GNSS failure)0.02°/h(RMS),0.06°/2h(RMS)0.01°/h(RMS),0.03°/3h(RMS)
Speed accuracyGNSS Valid, single pointL1/L20.1m/s(RMS)0.1m/s(RMS)
Speed retention (GNSS failure)2m/s/h(RMS),5m/s/2h(RMS)0.8m/s/h(RMS),3m/s/3h(RMS)
Fiber optical gyroMeasuring range±400°/s±400°/s
Bias stability≤0.02°/h≤0.01°/h
Quartz flexibleaccelerometerMeasuring range±20g±20g
Bias stability≤50µg(10s Average)≤20µg(10s平均)
Communication interfaceRS4226waysThe baud rate ranges from 9.6 KBPS to 921.6 KBPS. The default baud rate is 115.2 KBPSThe maximum frequency is 1000Hz(raw data), and the default frequency is 200Hz
RS2321 wayThe baud rate ranges from 9.6 KBPS to 921.6 KBPS. The default baud rate is 115.2 KBPSThe maximum frequency is 1000Hz(raw data), and the default frequency is 200Hz
Electrical characteristicsVoltage24~36VDC
Power consumption≤30W
Structural characteristicsDimension199mm×180mm×219.5mm
Weight6.5kg≤7.5kg(non-aviation)≤6.5kg (aviation optional)
EnvironmentWorking temperature-40℃~+60℃
Storage temperature-45℃~+65℃
Vibration (with damping)5~2000Hz,6.06g
Impact (with shock absorption)30g,11ms
ReliabilityLifetime>15years
Continuous working time>24

Size

L199mm x W180mm x H219.5mm(L x W x H)



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