Vehicle Navigation IMU Inertial Sensor 6 Axis GPS Ship UAV Motion

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Shenzhen Rion Technology Co., Ltd.

City: shenzhen

Country/Region:china

Tel:86-755-29657137-804

Contact Person:
Ms.Alice Du View Contact Details

Vehicle Navigation IMU Inertial Sensor 6 Axis GPS Ship UAV Motion

Brand Name	RION
Model Number	IMU560-422
Certification	CE
Place of Origin	Guangdong, China
Minimum Order Quantity	1
Price	$1015/Pieces
Payment Terms	T/T, Paypal
Supply Ability	1000 Bag/Bags per Month
Delivery Time	7 days
Packaging Details	CARTON
Usage	vehicle navigation
Range	±300
Resolution	<0.005
Acceleration sensitivity	<10°/h/g,rms Direction
Angle random walk	<0.15
Interface Type	Micro-DB9,RS422
horizontal position Estimation accuracy	2M
Pure inertial position	<40m@1min

Detailed Product Description

Vehicle navigation sensor 6 axis GPS IMU ship inertial motion sensor UAV inertial sensor

Download datasheet please click below

IMU560 IMU COMBINED INERTIAL NAVIGATION SYSTEM.pdf...

Application

★ High-speed train measurement and control system

★ Marine and underwater surveying and mapping

★ Surveying and mapping POS system

★ Ship and ocean engineering

★ Vehicle positioning and navigation

★ UAV navigation and control

★ Vehicle navigation and measurement and control system

The IMU560 series is a GPS/INS MEMS integrated navigation system built by RION.

The IMU560 series is positioned as a vehicle/shipborne general inertial and integrated navigation product

target market:

(1) moving through

(2) Car navigation

(3) Dynamic attitude measurement

Specifications

IMU560		PARAMETER	UNIT
Roll/pitch 1σ (dynamic)		0.3	°
HEADING POSITION ESTIMATION ACCURACY	Heading Accuracy 1σ	0.3 ° (GPS effective)	°
	Heading Accuracy 1σ	0.5°(GPSunlock 5min)	°
	Pure Inertial Position Estimation Accuracy 1σ	<40m@1min(GPS unlock)	m@1min
	Output Frequency	1~100	Hz
GYRO	Range	±300	°/s
	Zero Bias Instability(Allan)	10	°/h
	Zero Bias Stability(10s Mean)	15	°/h
	Zero Bias Repeatability	15	°/h
	Nonlinear Error	<0.1% of FS
	Scale Factor Nonlinearity1	<0.02	%
	Scale Factor Change ( 25 ° C)	±0.3	%
	Resolution	＜0.01	°/s
	Acceleration Sensitivity	<0.0028	°/s/g,rms
	Angle Random Walk	<0.15	°/√hr
	Noise Intensity	0.014	°/s/√hr
	Bandwidth	100	Hz
ACCELEROMETER	Range	±4	g
	Zero Bias Stability	0.2	mg
	Full Temperature Zero Bias	1.7	mg
	Scale Factor Stability	＜0.1	%
	Resolution	0.1	mg
	Nonlinear 2	0.1	%
	Noise Intensity	200	ug/√hr
	Bandwidth	100	Hz
MAGNETOMETER	Range	±2	Gauss
MAGNETIC AZIMUTH	Range	±180	°
MAGNETIC AZIMUTH	Accuracy	±1.0	°
Air pressure	Pressure range	1000~120000
Air pressure	Barometric error	±250	Pascal
STANDARD GPS PARAMETERS	Start Time	Cold start: 29s hot start: 1s
	Sensitivity	-166dBm
	Speed	0.05m/s
	Azimuth Accuracy	0.3°,P=50%@30m/s
	level reckoned accuracy	2m
ENVIRONMENTAL CHARACTERISTICS	Vibration Resistant	10grms,10～1000Hz
	Impact Resistance	100g@11ms,3 Axial Direction (Half Sinusoid)
	Range Of Working Temp.	-40°C~+85°C
ELECTRICAL INTERFACE	Input Current	＜100mA
	Input Voltage	9-36V(Ripple 50mV)
	Interface Type	J30J-9ZKP
COMPATIBLE SATELLITE MODE		GPS L1C/A, SBAS L1C/A, GLONASS L1OF, BEIDOU B1
WEIGHT		≤100g (Excluding cables)

INSTALLATION AXIS

IMU560 use NED coordinate, right hand coordinate, axis direction above.

By the rotation direction Z-Y-X, when X forward direction point to the front of carrier, then the angle rotating Z axis is yaw, Y axis pitch, X axis roll.

SIGNAL DEFINITION

Product Tags: 6 Axis IMU Inertial Sensor Navigation IMU Inertial Sensor UAV IMU Inertial Measurement Unit

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