Home > IMU Accelerometer Gyro >

High Precision Navigation Mems Imu KT-EX9-1 for Inertial Navigation with Built-in 3 Axis Gyro

Product Categories

Shenzhen Avionics Technology Co.,Ltd

Trust Seal

Verified Supplier

Credit Check

Supplier Assessment

Contact Now

High Precision Navigation Mems Imu KT-EX9-1 for Inertial Navigation with Built-in 3 Axis Gyro

Name: High Precision Navigation Mems Imu KTEX91 for Inertial Navigation with Builtin 3 Axis Gyro
Brand: AVIC
Price: 1 USD

Brand Name : AVIC

Model Number : KT-EX9-1

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

Weight : 50g

Bandwidth : 250Hz

Contact Now

High Precision Navigation Mems Imu KT-EX9-1 for Inertial Navigation with Built-in 3 Axis Gyro

Product Description

The 16488 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

Outline drawing

High Precision Navigation Mems Imu KT-EX9-1 for Inertial Navigation with Built-in 3 Axis Gyro

Production Environment

High Precision Navigation Mems Imu KT-EX9-1 for Inertial Navigation with Built-in 3 Axis Gyro

Packing& Shipping

High Precision Navigation Mems Imu KT-EX9-1 for Inertial Navigation with Built-in 3 Axis Gyro

High Precision Navigation Mems Imu KT-EX9-1 for Inertial Navigation with Built-in 3 Axis Gyro Images

Inquiry Cart 0

Send your message to this supplier


*From:	Your email address is incorrect!
*To:	Shenzhen Avionics Technology Co.,Ltd
*Subject:	Subject is empty!
*Message:	For the best results, we recommend including the following details: -Self introduction -Required specifications -Inquire about price/MOQ Characters Remaining: (0/3000) Please enter 20 to 3000 characters to contact this supplier!