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KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h
KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h
KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h
KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h
Specifications
Brand Name :
Firepower
Model Number :
KT-EX 9-1
Certification :
CE
Place of Origin :
CHINA
MOQ :
1
Price :
negotiable
Payment Terms :
L/C, T/T
Supply Ability :
500/Month
Delivery Time :
1 week for sample
Packaging Details :
Sponge/Box
Gyro Range :
±500°/s
Gyro Zero Bias Stability :
0.3°/h
Acc Range :
±20g
Acc Zero Bias Stability :
2ug
Random walk :
0.15°/√h
Communication Interface :
1 channel SPI
Bandwidth :
250Hz
Weight :
50g
Description

Cost Effective Mems lnertial Navigation Sensor for Aerospace and Aviation

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.

Main 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 1б 0.15 º/√h
Bias repeatability 1б 10 º/h
Output noise No filtering, RMS 0.05 º/s
Scale factor repeatability 1б 0.01 %
Scale factor nonlinearity 1б 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 1б 0.029 m/s/√h
Bias repeatability 1б 5 mg
Output noise No filtering, RMS 0.5 mg
Scale factor repeatability 1б 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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KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h

Production Environment

KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h

Packing& Shipping

KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h

KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h

KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h

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KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h

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Product Detail
Brand Name :
Firepower
Model Number :
KT-EX 9-1
Certification :
CE
Place of Origin :
CHINA
MOQ :
1
Price :
negotiable
Contact Supplier
KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h
KT-EX 9-1 Mems Inertial Navigation Sensor for Aerospace and Aviation Random Walk 0.15°/√h

Shenzhen Fire Power Control Technology Co., LTD

Verified Supplier
4 Years
guangdong, shenzhen
Since 2001
Business Type :
Manufacturer, Exporter, Trading Company, Seller
Main Products :
Accelerometer Gyro Sensor, IMU Accelerometer Gyro, Quartz Flexure Accelerometer
Total Annual :
10000000-15000000
Employee Number :
60~100
Certification Level :
Verified Supplier
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