Robust Imu Module Imu Navigation System for Unmanned Aircraft

Product Details
Customization: Available
Type: Inertial Navigation
Output Signal Type: Digital Output
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Registered Capital
1000000 RMB
Plant Area
1001~2000 square meters
  • Robust Imu Module Imu Navigation System for Unmanned Aircraft
  • Robust Imu Module Imu Navigation System for Unmanned Aircraft
  • Robust Imu Module Imu Navigation System for Unmanned Aircraft
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  • Overview
  • Product Description
  • Features
  • Product Parameters
  • Outline drawing
  • Company Profile
Overview

Basic Info.

Model NO.
16488H-B
Measuring Shaft Quantities
9 Axis
Accuracy Grade
0.8 Deg/H
IP Rating
IP67
Certification
CE
Customized
Customized
Gyro Range
-450deg/S-+450deg/S
Zero Bias Stability
0.8 Deg/H
Acc Range
16g
Acc Zero Bias Stability
0.015mg
High Reliability
>20000h
Transport Package
Sponge and Box
Specification
47mm*44mm*15mm
HS Code
9031809090
Production Capacity
100/Month

Product Description

Robust Imu Module IMU navigation System for Unmanned Aircraft
 

Product Description

The 16488-H-B is an inertial measurement unit (IMU) based on micromachining technology (MEMS), which contains high-performance MEMS gyroscope and MEMS accelerometer, and outputs three angular velocities and three accelerations.

16488-H features high reliability and strong environmental adaptability. By matching different software, the product can be widely used in intelligent driving, tactical and industrial UAV, intelligent ammunition, seeker, mobile communication, mapping, stable platform and other fields.
 

Features

  1. Three-axis digital gyroscope:
    1. ± 450º/s dynamic measuring range;
    2. Zero-bias stability: 3 °/H (GJB, 10s, Z-axis), 0.8 °/H (ALLAN, Z-axis);
  2. Triaxial digital accelerometer:
    1. ± 16 G dynamic measuring range;
    2. Zero-bias stability: 0.2mg (GJB, 10s), 0.03mg (ALLAN);
  3. High reliability: MTBF > 20000h;
  4. Guaranteed accuracy within the full temperature range (-40 ºC ~ 70 ºC): built-in high-performance temperature calibration and compensation algorithm;
  5. Suitable for working under strong vibration conditions;
  6. Interface 1 channel UART, 1 channel SPI, 1 channel CAN

Product Parameters

 
Parameter Test conditions Minimum value Typical value Maximum value Unit
Peg-top Dynamic measuring range       450 º/s
Zero bias stability Allan variance, Z-axis   0.8   º/h
Allan variance, X and Y axis   1   º/h
10 s average (-40 ºC ~ + 70 ºC, constant temperature), Z-axis   3   º/h
10 s average (-40 ºC ~ + 70 ºC, constant temperature), X axis and Y axis   4   º/h
Zero bias Zero-bias range, Z-axis   ±0.07   º/s
Zero-bias range, X-axis and Y-axis   ±0.2   º/s
Zero bias change over full temperature range, Z-axis1   ±0.02   º/s
Zero bias change over full temperature range, X and Y axis1   ±0.06   º/s
Successive Start Repeatability, Z-axis   0.002   º/s
Successive Start Repeatability, X-Axis and Y-Axis   0.006   º/s
Day-by-day start repeatability, Z-axis   0.003   º/s
Start repetition day by day, X axis and Y axis   0.009   º/s
Ffect of linear acceleration on bias   0.002   º/s/g
Influence of vibration on zero bias, change before and after vibration2   0.002   º/s/g
Influence of vibration on zero bias, change before and during vibration2   0.002   º/s/g
Scale factor Scale factor accuracy, Z-axis   0.3   %
Scale Factor Accuracy, X and Y Axis   0.6   %
Scale factor nonlinearity, Z-axis   0.01   %FS
Scale Factor Nonlinearity, X and Y Axis   0.02   %FS
Resolution     3.052×107   º/s/LSB
Bandwidth     200   Hz
Accelerometer Dynamic measuring range     16   g
Zero bias stability Allan variance   0.015   mg
10 s average (-40 ºC ~ + 70 ºC, constant temperature)   0.05   mg
Zero bias Zero-bias range   8 15 mg
Zero bias change in full temperature range, peak-to-peak value1   5 10 mg
Repeatability of successive starts     0.5 mg
Repeatability is initiated on a daily basis       mg
Zero-bias temperature coefficient   0.05 0.1 mg/ºC
Scale factor Scale factor accuracy     2 %
Scale factor nonlinearity     0.1 %FS
Resolution     1.221×108   g/LSB
Bandwidth     200   Hz
Communication interface 1-way SPI Baud rate     15 MHz
1-way UART Baud rate   230.4   Kbps
1-way CAN Baud rate     1 MHz
Sampling frequency SPI   200 1000 Hz
UART   200   Hz
CAN   200    
Electrical characteristics Voltage   3.0 3.3 3.6 V
Power consumption       1.5 W
Ripple P-P     100 mV
Structural characteristics Size     47×44×14   mm
Weight     50   g
Use environment Operating temperature   -40   70 ºC
Storage temperature   -45   75 ºC
Vibration     20~2000Hz,6.06g    
Impact     1000g,0.5ms    
Reliability MTBF     20000   h
Continuous working time     120   h
1: Calculate the zero deviation of the whole temperature change process, the temperature change rate is ≤ 1 ºC/min, and the temperature range is -40 ºC ~ + 70 ºC;
2: Vibration condition is 6.06 G, 20Hz ~ 2000Hz
 

Outline drawing


Robust Imu Module Imu Navigation System for Unmanned Aircraft

Company Profile


Robust Imu Module Imu Navigation System for Unmanned AircraftRobust Imu Module Imu Navigation System for Unmanned Aircraft





 
 
 

 

 

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