10-Axis Inertial Measurement Unit Kt-Ex 9-1 Imu Adis16488 Alternative for Unmanned Aircraft

Product Details
Customization: Available
Output Signal Type: Digital Output
IP Rating: IP67
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Registered Capital
1000000 RMB
Plant Area
1001~2000 square meters
  • 10-Axis Inertial Measurement Unit Kt-Ex 9-1 Imu Adis16488 Alternative for Unmanned Aircraft
  • 10-Axis Inertial Measurement Unit Kt-Ex 9-1 Imu Adis16488 Alternative for Unmanned Aircraft
  • 10-Axis Inertial Measurement Unit Kt-Ex 9-1 Imu Adis16488 Alternative for Unmanned Aircraft
  • 10-Axis Inertial Measurement Unit Kt-Ex 9-1 Imu Adis16488 Alternative for Unmanned Aircraft
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  • Overview
  • Product Description
  • Product Parameters
  • Company Profile
Overview

Basic Info.

Model NO.
KT-EX 9-1
Certification
CE
Customized
Customized
Gyro Range
±500º/S
Zero Bias Stability
0.3 Deg/H
Acc Range
20g
Acc Bias Stability
2ug
Bandwidth (-3dB)
250Hz
Transport Package
Sponge and Box
Specification
47mm*44mm*15mm
Trademark
AVIC
Origin
China
HS Code
9031809090
Production Capacity
100/Month

Product Description

10-axis Inertial Measurement Unit KT-EX 9-1 IMU ADIS16488 Alternative for Unmanned Aircraft
 

Product Description


 The KT-EX 9-1 inertial measurement unit is a complete inertial system with a built-in three-axis gyroscope and a three-axis accelerometer, which is used to measure the three-axis angular rate, acceleration and other parameters of the carrier, and output the data after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) through SPI according to the communication protocol.
10-Axis Inertial Measurement Unit Kt-Ex 9-1 Imu Adis16488 Alternative for Unmanned Aircraft
10-Axis Inertial Measurement Unit Kt-Ex 9-1 Imu Adis16488 Alternative for Unmanned Aircraft


 

Product Parameters

Parameter Test conditions Minimum value Typical value Maximum value Unit
Gyro Dynamic measuring range     ±500   º/s
Bias instability Allan variance, better than   0.3   º/h
Bias stability 1s smooth, RMS, better than   10   º/h
Bias in full temperature range -40 ºC ~ 85 ºC, 10 s smoothing, RMS   0.005   º/s
Random walk   0.15   º/√h
Bias repeatability   10   º/h
Output noise No filtering, RMS   0.05   º/s
Scale factor repeatability   0.01   %
Scale factor nonlinearity   0.01   %
Scale factor FS=450 º/s, 32bits   2621440   LSB/°/sec
Bandwidth (-3dB)     250   Hz
Cross coupling     0.1   %
Acceleration sensitivity     1   °/h/g
Vibration rectification effect     0.5   °/h/g2
Resonant frequency     12k   Hz
Accelerometer Dynamic measuring range     ±20   g
Bias stability Allan variance   2   ug
Bias in full temperature range -40 ºC ~ 85 ºC, 10 s smoothing, RMS   1   mg
Random walk   0.029   m/s/√h
Bias repeatability   5   mg
Output noise No filtering, RMS   0.5   mg
Scale factor repeatability   0.1   %
Scale factor nonlinearity FS=20g   0.1   %FS
Scale factor ±20, 32bits   65536000   g/LSB
Bandwidth (-3dB)     250   Hz
Cross coupling     0.1   %
Temperature Scale factor     0.0125   °C/LSB
Communication interface 1-way SPI Enter the clock frequency   8 15 MHz
Electrical characteristics Voltage Direct current   3.3 ± 10%   V
Power consumption     1 1.5 W
Ripple P-P   48±2 100 mV
Use environment Operating temperature Scalable -40   85 ºC
Storage temperature   -55   85 ºC
Vibration     10~2000Hz,6.06g    
Impact     1000g,0.1ms    



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10-Axis Inertial Measurement Unit Kt-Ex 9-1 Imu Adis16488 Alternative for Unmanned Aircraft

Company Profile

10-Axis Inertial Measurement Unit Kt-Ex 9-1 Imu Adis16488 Alternative for Unmanned Aircraft10-Axis Inertial Measurement Unit Kt-Ex 9-1 Imu Adis16488 Alternative for Unmanned Aircraft







 
 
 

 

 

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