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Shenzhen Fire Power Control Technology Co., LTD

  • China,Shenzhen ,Guangdong
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China High Performance Inertial Satellite Integrated Navigation System for Unmanned
China High Performance Inertial Satellite Integrated Navigation System for Unmanned

  1. China High Performance Inertial Satellite Integrated Navigation System for Unmanned

High Performance Inertial Satellite Integrated Navigation System for Unmanned

  1. MOQ: 1
  2. Price: Negotiable
  3. Get Latest Price
Payment Terms T/T
Supply Ability 500/month
Delivery Time 10 days
Packaging Details sponge and carton
Position accuracy 1.8nm/h
Heading accuracy 0.1°/h
Attitude accuracy 0.05°/h
Horizontal Velocity Accuracy 0.1m/s
Navigation data frequency(Single point L1/L2) 200Hz
Gyroscope Range 400°/s
Gyroscope Zero bias stability 0.3°/h
Accelerometer Range 16g
Accelerometer Zero bias stability 50ug
Dimension 138.5 mm× 136.5 mm×102mm
Weight 2.0 kg (without cable)
Operating temperature -40℃~+60℃
Brand Name Firepower
Model Number INS500D
Certification CE
Place of Origin China

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  1. Product Details
  2. Company Details

Product Specification

Payment Terms T/T Supply Ability 500/month
Delivery Time 10 days Packaging Details sponge and carton
Position accuracy 1.8nm/h Heading accuracy 0.1°/h
Attitude accuracy 0.05°/h Horizontal Velocity Accuracy 0.1m/s
Navigation data frequency(Single point L1/L2) 200Hz Gyroscope Range 400°/s
Gyroscope Zero bias stability 0.3°/h Accelerometer Range 16g
Accelerometer Zero bias stability 50ug Dimension 138.5 mm× 136.5 mm×102mm
Weight 2.0 kg (without cable) Operating temperature -40℃~+60℃
Brand Name Firepower Model Number INS500D
Certification CE Place of Origin China
High Light Inertial Satellite Integrated Navigation SystemHigh Performance Inertial Navigation SystemUnmanned Ships Inertial Navigation System
Product Description

      The fiber-optic integrated navigation system INS500D is based on closed-loop fiber-optic gyroscope, accelerometer and high-end GNSS receiving board with high cost performance, and is realized through multi-sensor fusion and navigation calculation algorithm, which meets the requirements of accurate measurement of attitude, heading and position information in the application fields of medium and high precision mobile measurement system and large UAV.

 

 

Main Function

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 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 calculated by inertia are output, in which the pitch and roll are required to be accurate, the course keeping function is available in a short time, and the meter-level positioning accuracy is available in a short time. In the integrated navigation mode, post-processing information can be output for post-processing software to process.

     After the pure inertial mode (i.e., 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.

 

 
Performance Index
Parameter Technical indicators

 

 

 

 

 

Position accuracy

Single point (RMS) 1.2m
RTK(RMS) 2cm+1ppm

 

Lock-loss accuracy (CEP)

1.8nm/h

2 ‰ D, where D is the distance travelled (optional, DVL or odometer combination)

 

 

Heading (RMS)

 

Self-north seeking accuracy

0.1 ° × sec (Lati), 10 min alignment of stationary base; Where Lati denotes the latitude.
Lock-loss holding accuracy 0.1°/h

 

Attitude (RMS)

GNSS is valid 0.02°
Lock-loss holding accuracy 0.05°/h
Horizontal Velocity Accuracy (RMS) Single point L1/L2 0.1m/s
GNSS is invalid 2m/s/h
Navigation data frequency 200Hz

 

 

 

 

 

Gyroscope

Range 400°/s
Zero bias stability 0.3°/h
Scale factor nonlinearity

 

50ppm

Angular random walk 0.02°/ √hr
   

 

 

 

 

 

Accelerometer

Range 16g
Zero bias stability 50ug⑤
Scale factor nonlinearity

 

100ppm

Speed random walk 0.01m/s/ √hr

 

 

 

 

Physical dimensions and electrical characteristics

Overall dimensions 138.5 mm× 136.5 mm×102mm
Weight 2.0 kg (without cable)
Input voltage 12~36VDC
Power consumption < 24W (steady state)
Store 16G

 

 

 

 

Environmental indicators

Operating temperature -40℃~+60℃
Storage temperature -45℃~+70℃
Random vibration 6.06g,20Hz~2000Hz
MTBF 3000h

 

 

 

 

Interface characteristics

PPS, EVENT, RS232, RS422, CAN (optional)
100m network port
Antenna Connector (TNC)
Wheel speed sensor interface

 

 

Outline Drawing


Company Details

Bronze Gleitlager

,

Bronze Sleeve Bushings

 and 

Graphite Plugged Bushings

 from Quality China Factory
  • Business Type:

    Manufacturer,Exporter,Trading Company,Seller

  • Year Established:

    2001

  • Total Annual:

    10000000-15000000

  • Employee Number:

    60~100

  • Ecer Certification:

    Verified Supplier

Shenzhen Fire Power Control Technology Co., Ltd. is a professional manufacturer specializing in the production of  electronic products and inertial devices, and providing technical consultation and export services. The company has a strong independent  team. The technical team is comp... Shenzhen Fire Power Control Technology Co., Ltd. is a professional manufacturer specializing in the production of  electronic products and inertial devices, and providing technical consultation and export services. The company has a strong independent  team. The technical team is comp...

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  • Shenzhen Fire Power Control Technology Co., LTD
  • 429, Building A10, Fuhai Information Port, Xinhe Community, Fuhai Street, Shenzhen, Guangdong, China
  • https://www.accelerometergyro.com/

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