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Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable
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solutions
contact us
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home
about us
Company Profile
factory tour
quality control
FAQ
products

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable
blogs
solutions
contact us
quote

products details

Created with Pixso. Home Created with Pixso. Products Created with Pixso.
Inertial Navigation System
Created with Pixso.

Closed Loop Optical Fiber Integrated Inertial Navigation System Mobile Measurement

Closed Loop Optical Fiber Integrated Inertial Navigation System Mobile Measurement

Closed Loop Optical Fiber Integrated Inertial Navigation System Mobile Measurement

Brand Name: Firepower
Model Number: GI300F
MOQ: 1
Price: negotiable
Payment Terms: T/T
Supply Ability: 500/month
Detail Information
Product Description
Detail Information
Place of Origin:
CHINA
Certification:
CE ROHS
Product:
FOG INS
Heading Accuracy:
0.1°
Attitude Accuracy:
0.02°（RMS）
Gyroscope Range:
±400°/s
Zero Bias Stability:
≤100µg
Accelerometer Range:
±20g
Packaging Details:
sponge+carton
Supply Ability:
500/month
Highlight:

Closed Loop Inertial Navigation System

,

FOG INS Inertial Navigation System

,

High Precision Inertial Navigation System

Product Description

Closed-Loop Optical Fiber Integrated Navigation System High Precision Mobile Measurement Systems

 

The fiber-optic integrated navigation system GI300F-INS is based on closed-loop fiber-optic gyroscope and accelerometer with high cost performance, and is realized through multi-sensor fusion and navigation calculation algorithm, which meets the requirements of precise measurement of attitude, heading and position information in the application fields of medium and high precision mobile measurement systems, medium and large UAVs, etc.

 

Project Test conditions Indicators
Positioning accuracy External GNSS Valid, Single Point Better than external satellite positioning accuracy
External GNSS Valid, RTK Better than external satellite positioning accuracy
Pure inertial horizontal position holding①

80m/5min(CEP)

500m/10min(CEP)

1.5nm/30min(CEP)
Airspeed combination horizontal position hold② 0.8nm/30min (CEP)
Heading accuracy Single antenna (RMS) 0.1°③
Dual Antenna (RMS) 0.2 °/L (L = baseline length) (RMS)
Course Keeping (RMS) 0.2°/30min(RMS),0.5°/h
Self-north seeking accuracy (RMS)

0.2 ° SecL, dual position alignment for 15 min

1.0 ° SecL, single position alignment 5-10 min
Attitude accuracy GNSS is valid 0.02°(RMS)
Attitude hold (GNSS failure) 0.2°/30min(RMS),0.5°/h(RMS)
Speed accuracy GNSS valid, single point L1/L2 0.1m/s(RMS)
Gyroscope Measuring range ±400°/s
Zero bias stability ≤0.3°/h
Accelerometer Measuring range ±20g
Zero bias stability ≤100µg
Physical dimensions and electrical characteristics Voltage 9-36V DC
Power consumption ≤ 12W (steady state)
Interface 2-channel RS232, 1-channel RS422, 1-channel PPS (LVTTL/422 level)
Size 92.0 mm × 92.0 mm × 81.0mm (L, W, H)
Weight ≤1.2kg
Environmental characteristics Operating temperature -40℃~+60℃
Storage temperature -45℃~+70℃
Vibration 5 ~ 2000Hz, 6.06 G (with shock absorber)
Impact 30g, 11 ms (with shock)
Life span > 15 years
Continuous working time >24h
Height limit ≤5000m
speed limit ≤500m/s

Note:

  • The alignment is valid;
  • For airborne use, there is a turning maneuver before the airspeed combination, and the test takes the flight speed of 150km/H as an example;
  • On-board conditions, need to be mobile;
 

 

Size:

Closed Loop Optical Fiber Integrated Inertial Navigation System Mobile Measurement 0

Tags: 

GPS Inertial Navigation Sensor  

INS570D Inertial Navigation System  

Inertial Navigation System RTK

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