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Chi tiết sản phẩm

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Con quay gia tốc kế IMU
Created with Pixso.

RS422 Output IMU Six Output Inertial Sensor Analog Of STIM300

RS422 Output IMU Six Output Inertial Sensor Analog Of STIM300

Tên thương hiệu: AVIC
Số mẫu: IMU300C
MOQ: 1
giá bán: Có thể đàm phán
Điều khoản thanh toán: T/T,L/C
Khả năng cung cấp: 500/tháng
Thông tin chi tiết
Nguồn gốc:
Trung Quốc
Chứng nhận:
CE ROHS
Tên sản phẩm:
Đơn vị đo quán tính
phạm vi đo con quay hồi chuyển:
±500º/giây
con quay hồi chuyển Độ ổn định không thiên vị:
0.3 độ/giờ
đi bộ ngẫu nhiên góc:
0.06 độ /√h
phạm vi gia tốc:
16G
acc sự ổn định thiên vị:
00,02 mg
Yếu tố quy mô:
0,02%FS
băng thông:
200HZ
Sản lượng:
RS422
chi tiết đóng gói:
miếng bọt biển/hộp
Khả năng cung cấp:
500/tháng
Mô tả sản phẩm

RS422 Output IMU Six Output Inertial Sensor Analog Of STIM300

 

RS422 Output IMU Six Output Inertial Sensor Analog Of STIM300 0

 

 

Electrical interface

The electrical connector of IMU300C-A0-IMU product is J30J-15 TJL, and the specific contact definition and allocation are shown in the following table:

Stitch number Name Type Remark
1 TxD- Output RS422
2 RxD- Input RS422
3 TST_1 Output  
4 TOV_1 Output  
5 RST Input  
6 GND Input  
7 Spare    
8 VCC_5V Power source +5v
9 TxD+ Output RS422
10 RxD+ Input RS422
11 ExtTrig Input Synchronous input 5V
12 GND Input  
13 GND Input  
14 Spare    
15 GND Power ground  
 

Product features

  1. Three-axis digital gyroscope:
    1. ± 500º/s dynamic measuring range;
    2. Zero-bias stability: 3 °/H (GJB, 10s), 0.3 °/H (ALLAN);
  2. Triaxial digital accelerometer:
    1. ± 16 G dynamic measuring range;
    2. Zero-bias stability: 0.1mg (GJB, 10S), 0.02mg (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-way RS422
  7. Compatible with STIM300

Field of application

  1. Tactical and Industrial UAV
  2. Smart Munitions
  3. Seeker

Product indicators

Parameter

Test conditions

Design accuracy

Unit

Gyro Dynamic measuring range - ±500 º/s
Bias stability Allan variance (500 °/s range, normal temperature) 0.3 º/h
10 s average (-40 ℃ ~ + 80 ℃, constant temperature), 3.0 º/h
Bias Zero-bias range 0.1 º/s
Zero-bias variation over full temperature range 0.01 º/s
Start repeatability 0.005 º/s
Effect of linear acceleration on bias 0.002 º/s/g
Influence of vibration on Bias, change before and after vibration 0.002 º/s/g
Influence of vibration on Bias, change before and during vibration 0.001 º/s/g
Scale factor Scale factor accuracy 0.1 %
Scale factor nonlinearity 0.01 %FS
Angular random walk - 0.06 °/√hr
Bandwidth - 200 Hz
Accelerometer Dynamic measuring range - 16 g
Bias stability Allan variance (16g range, normal temperature) 0.02 mg
10 s average (-40 ℃ ~ + 80 ℃, constant temperature) 0.03 mg
Bias Zero-bias range 1 mg
Zero-bias variation over full temperature range 1 mg
Start repeatability 0.2 mg
Scale factor Scale factor accuracy 0.3 %
Scale factor nonlinearity 0.02 %FS
Speed random walk - 0.08 m/s/√hr
Bandwidth - 200 Hz
Communication interface 1-way SR422 Baud rate 460.8 MHz
Sampling frequency UART 1000 Hz
Electrical characteristics Voltage - 5 V
Power consumption - 1.5 W
Ripple P-P 150 mV
Structural characteristics Size - 38.6×44.6×21.5 mm
Weight - 65±2 g
Use environment Operating temperature - -40~80
Storage temperature - -45~85
Vibration - 20~2000Hz,6.06g  
Impact - 6000g,0.5ms  
Reliability MTBF - 20000 h
Continuous working time - 120 h
 

Product overview

The IMU300C-A0-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.
IMU300C-A0-IMU features 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.

Size