Sign In | Join Free | My fnxradio.com
China Shenzhen Avionics Technology Co.,Ltd logo
Shenzhen Avionics Technology Co.,Ltd
Through the efforts of several generations, 450,000 aviators have been united together, inspiring each aviator to forge ahead and provide professional avionics products and services in the military
Verified Supplier

3 Years

Home > IMU Accelerometer Gyro >

Compact and Low Weight IMU Inertial Sensor Inertial Navigation System in UAV

Shenzhen Avionics Technology Co.,Ltd
Trust Seal
Verified Supplier
Credit Check
Supplier Assessment

Compact and Low Weight IMU Inertial Sensor Inertial Navigation System in UAV

Brand Name : AVIC

Model Number : GI200G-B0

Certification : CE

Place of Origin : CHINA

MOQ : 1

Price : negotiable

Payment Terms : T/T

Supply Ability : 500/month

Delivery Time : 1 weeks

Packaging Details : sponge + box

Product Name : IMU Gyro for UAV

Gyro Zero Bias Stability : 10 °/h (GJB, 10s), 2.0 °/h (ALLAN)

Gyro Range : ±500º/s

Accelerometer Zero Bias Atability : 0.5mg

Accelerometer Range : ±16g

Operating temperature : -40~+80℃

Vibration : 20~2000Hz

Bandwidth : 200Hz

Contact Now

Compact and Low Weight IMU Inertial Sensor Inertial Navigation System in UAV

Product Description

The GI200G-B0-IMU is an inertial measurement unit (IMU) based on micromachining technology (MEMS), with built-in high-performance MEMS gyroscope and MEMS accelerometer, outputting 3 angular velocities and 3 accelerations.

GI200G-B0-IMU has high reliability and strong environmental adaptability. By matching different software, the product can be widely used in tactical and industrial UAV, smart ammunition, seeker and other fields.

Main Application Field

  1. Tactical and Industrial UAV
  2. Smart Munitions
  3. Seeker
  4. Automatic driving
  5. Stabilize the platform

Main Functions

  1. Three-axis digital gyroscope:
    1. ±500º/s (MAX:±2000 °/s) dynamic measurement range;
    2. Zero bias stability: 10 °/h (GJB, 10s), 2.0 °/h (ALLAN);
  2. Triaxial digital accelerometer:
    1. ±16g (MAX:±200g) dynamic measuring range;
    2. Zero-bias stability: 0.5mg (GJB, 10s), 0.1mg (ALLAN);
  3. High reliability: MTBF > 20000h;
  4. Guaranteed accuracy within the full temperature range (-40 ℃ ~ 80 ℃): built-in high-performance temperature calibration and compensation algorithm;
  5. Suitable for working under strong vibration conditions
  6. Interface 1-channel UART

Technical Indicators

Parameter Test conditions Typical value Unit
Angular velocity Range Turntable 50,010,002,000 °/s
Zero bias Stability 10 s average, + 70 ℃, + 20 ℃, -40 ℃ 10 °/h
Allan variance, + 20 ℃ 2 °/h
Zero-bias total temperature variation -40 ℃ ~ + 70 ℃, 1 ℃/min, 10 s average, 1σ ±0.05 °/s
Zero bias Zero bias range ±0.1 °/s
Scale factor Non-linearity +20℃ 0.01 %FS
Scale factor accuracy Life-cycle change, accelerated testing 0.2 %FS
Acceleration sensitive term   8 °/h/g
Bandwidth 3dB 200 Hz
Data delay Excluding transmission time <5 ms
Acceleration Range   16,200 g
Zero bias Stability 10 s average, + 70 ℃, + 20 ℃, -40 ℃ 0.5 mg
Allan variance, + 20 ℃ 0.1 mg
Zero-bias total temperature variation -40 ℃ ~ + 70 ℃, 1 ℃/min variation 1 mg
Zero bias Zero bias range 5 mg
Scale factor Repeatability of successive starts +70℃,+20℃,-40℃ 100 ppm
Non-linearity +20℃ 0.02 %FS
Scale factor accuracy Life-cycle change, accelerated test instead 0.3 %FS
Bandwidth 3dB 200 Hz
Start time Time from power-on to output valid data 500 ms
3 gyro axes and 3 acceleration axes +70℃,+20℃,-40℃ 0.05 °
The degree of nonorthogonality between any two ax
Overall dimensions LxWxH 22.4×24×9 mm
Weight   10 g
Power supply   5±0.5 V
Ripple P-p 100 mV
Power consumption   0.5 W
Use environment Operating temperature- -40~+80
Storage temperature -45~+85
Impact 1000g,0.5ms  
Vibration 20~2000Hz,  
6.06g
Communication update rate 1-channel UART 500 (default) Hz
1000 (Max)
Communication baud rate 1-channel UART 460.8 (default) kbps
921.6 (Max)
Reliability MTBF 20000 h
Continuous working time 120 h

Electrical interface

GI200G-B0-IMU adopts 6PIN domestic connector with locking function for interconnection.

Interface model: A1008 WR-S-6P, the recommended mating terminal is A1008H-6P + A1008-T/G or 5013300600 (6p) + 5013340000.

Compact and Low Weight IMU Inertial Sensor Inertial Navigation System in UAV

Product Dimension

Compact and Low Weight IMU Inertial Sensor Inertial Navigation System in UAV

L22.4mm x W24mm x H9mm(L x W x H)


Product Tags:

Compact IMU Inertial Sensor

      

UAV IMU Inertial Sensor

      

Low Weight IMU Inertial Sensor

      
Wholesale Compact and Low Weight IMU Inertial Sensor Inertial Navigation System in UAV from china suppliers

Compact and Low Weight IMU Inertial Sensor Inertial Navigation System in UAV Images

Inquiry Cart 0
Send your message to this supplier
 
*From:
*To: Shenzhen Avionics Technology Co.,Ltd
*Subject:
*Message:
Characters Remaining: (0/3000)