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OEM Tactical Inertial Measurement Unit 3 Axis Compatible IMU MEMS Sensor

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OEM Tactical Inertial Measurement Unit 3 Axis Compatible IMU MEMS Sensor

Country/Region	china
City & Province	shenzhen
Categories	Measuring & Analysing Instrument Design Services

Product Details

Tactical Inertial Measurement Unit IMU Compatible/IMU MEMS Sensor for Ship and submarine robot

Introduction

The IMU560 series is a GPS/INS MEMS integrated navigation system built by RION.the inertial measurement unit (IMU) is precision calibrated throughout the temperature range to meet performance requirements in different environments. The multi-data Kalman filter fusion algorithm is realized by a built-in navigation computer, and outputs real-time accurate carrier posture, heading information, three-dimensional position and velocity information, and various inertial device information. The appearance is exquisite, the structure is small, the installation is convenient, the use is flexible, and the operation is more stable and reliable.

 
Feature

●Gyro bias instability 10°/h (Allan Variance)

●Accelerometer deviation 1.7mg (2g range)

Application

●Moving attitude unit

●Car navigation and measurement and control system

●High-speed train measurement and control system

●Surveying and mapping POS system

●Ship and ocean engineering

●Ocean and underwater mapping
 
●Flight control

Marketing orientation

The IMU560 series is positioned as a vehicle/shipborne general
inertial and integrated navigation product,
 
target market:
(1)Dynamic communication

(2)Vehicle navigation

(3)Dynamic attitude measure

Detailed Images

According to the rotation order of Z-Y-X, when the positive direction of the X-axis is directed to the front of the carrier, the angle of rotation around the Z-axis is the heading angle, the angle of rotation around the Y-axis is the pitch angle, and the angle of rotation around the X-axis is the roll angle. .

index	IMU560	Unit
gyro
Range	±300	°/s
Zero bias instability(Allan)	10	°/h
Zero bias stability(10s mean)	20	°/h
Zero bias repeatability	20	°/h
Nonlinear error	<0.1% of FS
Scale factor non-linearity1	<0.02	%
Scale factor repeatability	200	ppm
Resolution	<0.005	°/s
accelerometer sensitivity	<10°/h/g,rms Direction	°/h/g,rms
Angle random walk	<0.15	°/√hr
Bandwidth	250	Hz
Delay	<4	ms
Accelerometer
Range	±2	g
Zero bias stability	0.2	mg
Full temp. zero bias	1.7	mg
Scale factor repeatability	200	ppm
Resolution	0.1	mg
Non-linearity2	0.05	%
Bandwidth	125	Hz

*Factory qualified test indicators

1.1. Within ±100°/s, the symmetry and nonlinearity are required to be <200ppm, and the test angular rate is 0, ±0.1, ±0.2, ±0.5, ±1, ±2, ±5±n*5, n = 1,2 , 3...

2.Measure within ±1g and full scale separately

Uage and installation.

1. The power supply should be 9-36V DC, the ripple is <50mV, and
the current is at least 0.5A. If the power supply noise is large
and the power supply line is long, please use a filter or an
external voltage regulator.

2. The IMU application M4 semi-circular head screw is fixed on the
carrier, and the looseness during operation will affect the
measurement accuracy.

3. If possible, install it at the center of gravity of the carrier
or near the center of gravity.

4. Try to avoid severe vibration, sudden temperature changes (such
as installed next to the engine), and use shock absorbers if
necessary.

5. Align the IMU axis with the carrier axis as much as possible.

Dimension