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Low Zero Stability Integrated Navigation System With Fiber Gyro And Mems Acceleroemter

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Low Zero Stability Integrated Navigation System With Fiber Gyro And Mems Acceleroemter

Brand Name : AVIC

Model Number : GI300A

Certification : CE ROHS

Place of Origin : CHINA

MOQ : 1

Price : negotiable

Payment Terms : T/T

Supply Ability : 50/month

Delivery Time : 20 days for sample

Packaging Details : sponge+carton

Product name : Integrated Navigation System

Heading accuracy : 0.1deg

Attitude accuracy : 0.02deg

Gyro range : ±400°/s

Gyro Zero bias stability : ≤0.3°/h

Accelerometer range : ±16g

Accelerometer Zero bias stability : ≤50µg

Horizontal Velocity Accuracy : 0.05m/s

Output frequency : 200Hz

Working Temperature : -40℃~+60℃

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Low zero stability Integrated Navigation System with Fiber Gyro and Mems Acceleroemter

Product Description

The fiber optic integrated navigation system GI300A is based on a cost-effective closed-loop fiber optic gyroscope, accelerometer, and high-end GNSS receiving board. It is implemented through multi-sensor fusion and navigation calculation algorithms, meeting the precise measurement requirements for attitude, heading, and position information in applications such as high-precision mobile measurement systems and large unmanned aerial vehicles.

Product features

  • The system has inertial/satellite integrated navigation mode and pure inertial mode.
  • In the inertial/satellite integrated navigation mode, the satellite positioning information received by the internal GNSS receiver can be used for integrated navigation, and the pitch, roll, course, position, speed, time and other information of the carrier can be output; After the signal is lost, the position, velocity and attitude of the inertial solution are output, in which the pitch and roll are required to be kept accurate, with a certain course keeping function in a short time and meter-level positioning accuracy in a short time.In combination navigation mode, it is possible to output post-processing information for NovAtel's IE post-processing software to process.
  • After the pure inertial mode (that is, GPS fusion has never been performed after power-on, and if it loses lock again after fusion, it belongs to the integrated navigation mode) is started, it has accurate attitude measurement function, can output the pitch and roll heading, and the pure inertial mode can find the north statically.

Technical parameter

Parameter Technical indicators
Position accuracy Single point (RMS) 1.2m
RTK(RMS) 2cm+1ppm
Post-processing (RMS) 1cm+1ppm
Lock-loss accuracy (CEP) 10 m, loss of lock for 30 s ①
Deep/swaying/surging 5cm or 5%
Heading (RMS) Single antenna 0.1°②
Dual antenna 0.1 ° (baseline ≥ 2 m)
Post-processing 0.02°
Lock-loss holding accuracy 0.5 °, out of lock for 30 min
Self-north seeking accuracy 1 ° SecL, alignment for 15 min ③
Attitude (RMS) Single antenna 0.02°
Dual antenna 0.02°
Post-processing 0.015°
Lock-loss holding accuracy 0.5 °, out of lock for 30 min
Horizontal Velocity Accuracy (RMS) 0.05m/s
Timing accuracy 20ns
Data output frequency 200Hz④
Gyroscope Range 400°/s
Zero bias stability 0.3°/h⑤
Scale factor 100ppm
Nonlinearity
Angular random walk 0.05°/√hr
Accelerometer Range 16g
Zero bias stability 50ug⑤
Scale factor 100ppm
Nonlinearity
Speed random walk 0.01m/s/√hr
Physical dimensions and electrical characteristics Overall dimensions 138.5 mm×136.5 mm×102mm
Weight < 2.7 kg (without cable)
Input voltage 12～36VDC
Power consumption < 24W (steady state)
Store Reserved
Environmental indicators Operating temperature -40℃~+60℃
Storage temperature -45℃～+70℃
Random vibration 6.06g,20Hz~2000Hz
MTBF 30000h
Interface characteristics PPS, EVENT, RS232, RS422, CAN (optional)
Network port (reserved)
Antenna interface
Wheel speed sensor interface

Noted:

① Alignment is valid; ② On-board condition and maneuvering is required; ③ Dual-position alignment, and the heading difference between the two positions is greater than 90 degrees; ④ Single-channel output is 200hz; ⑤ 10s average.

Dimensions

Low Zero Stability Integrated Navigation System With Fiber Gyro And Mems Acceleroemter

L138.5mm x W136.5mm x H102mm(L x W x H)

Low Zero Stability Integrated Navigation System With Fiber Gyro And Mems Acceleroemter

Low Zero Stability Integrated Navigation System With Fiber Gyro And Mems Acceleroemter


Product Tags:

Fiber Gyro Integrated Navigation System

      

Low zero stability Integrated Navigation System

      

Mems Acceleroemter Integrated Navigation System

      
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