-
Digital Inclinometer Sensor
-
Analog Inclinometer Sensor
-
Dynamic Inclinometer
-
Wireless Inclinometer
-
Electronic Compass Sensor
-
Attitude And Heading Reference System
-
IMU Inertial Measurement Unit
-
Accelerometer Vibration Sensor
-
GNSS INS Integration
-
Tilt Switch Sensor
-
Fiber Optical Gyroscope
-
Gyroscope Sensor Chip
-
Accelerometer Chip
GI520 High-Precision Fiber Optic Integrated Navigation System INS GNSS
Contact me for free samples and coupons.
Whatsapp:0086 18588475571
Wechat: 0086 18588475571
Skype: sales10@aixton.com
If you have any concern, we provide 24-hour online help.
xAcceleration | ±4 G | Operating Temperature | -40°C ~ +60°C |
---|---|---|---|
Speed Accuracy | 0.1m/s | Data Update Rate | 100 Hz @ 115,200 Baud Rate |
Orientation Accuracy | 0.1deg,(2m Base Line) | Dimension | Φ89mm× 118 Mm(Designable) |
Angular Velocity | ±300 Deg/s | Weight | ≤810 G |
High Light | 0.1m/s GNSS INS Integration,GNSS INS Integration accuracy 0.1 deg,2m line aviation gps navigation |
GI520 High-precision FIber Optic Integrated Navigation System
Introduction
The BW-GI520 integrated navigation system uses tight coupling technology to closely combine the high-precision, professional-grade, multi-channel, dual-antenna single-frequency carrier phase and pseudo-range GPS receiver with a high-precision optical fiber inertial measurement unit. It has a small size, light weight, Features such as high performance.
Perfomance index
Azimuth accuracy | (2m base line) | 0.1 deg |
Satellite signal loss |
0.06deg /5min 0.6deg /1h |
|
Roll attitude accuracy | ≤0.2 deg | |
Pitch attitude accuracy | ≤0.2 deg | |
Combined external GPS | Speed accuracy | 0.1m/s |
Single point positioning accuracy | DGPS 0.5m /RTK 2cm | |
Orientation accuracy | 0.1deg,(2m base line) | |
Measuring range | Azimuth | ±180 deg |
Roll angle | ±90 deg | |
Pitch angle | ±90 deg | |
Angular velocity | ±300 deg/s | |
Acceleration | ±4 g | |
Interface characteristics | Power supply | +9~+36 Vdc, ≤8 W @ 24Vdc |
Electrical Interface | RS422 | |
Data update rate | 100 Hz @ 115,200 baud rate | |
Use environment | Operating temperature | -40°C ~ +60°C |
Storage temperature | -55°C ~ +85°C | |
Physical characteristics | Dimension | Φ89mm× 118 mm(Designable) |
Weight | ≤810 g | |
Connector | Y11P-1210ZK10 |
Application:
● Space stable platform, the stability of the antenna system
● Attitude/azimuth reference system, multi-beam attitude sensing
● Navigation and control of unmanned vehicles, unmanned aerial vehicles, and unmanned ships
Company introduction
Wuxi Bewis Sensing Technology LLC(BWSENSING) is an innovative fast growing company established in 2010. The company was born in The Institute of Microelectronics (IME) of Peking University. We have achieved the top spot in the middle and high-end industry applications in the Chinese market.
From 2019, BWSENSING ® is approved as our global brand.With 10 years experience in the research-design-development and manufacture of a range of Inertial sensor technology, BWSENSING posses the skills, knowledge and experience to provide fully integrated OEM/ODM design and manufacturing services for Inclinometer, Electronic Compass, IMU, AHRS, GNSS/INS and Fiber Optic Gyroscope. As the company co-founder Dr. Guangyi Shi said, we will use the Accurate and Cost-effective sensors to make a greater contribution to the global society for a better IoT world.
FAQ
Q1: Accuracy definition of products
A: RMS accuracy, the accuracy of each product can be traced.Accuracy test report can be provided if required.
Q2: How to select suitable model?
A: Users should check the following points:
a. Single or dual axis?
b. Commom protocol, Modbus or CAN?
c. Dynamic or static Application scenarios?
d. Horizontal or vertical installation?
Q3: How to purchase?
A: If you want sample, please purchase on BWSENSING online shop. We accept Paypal/TT/CC.If you purchase in bulk, it is recommended to consult the sales for the best price.
Q4: How long is the warranty period?
A: One year.
Q5: Fiber optic gyroscope test method
The military standard for the current fiber optic gyroscope test method is: GJB2426A-2004