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RS232 MEMS IMU Inertial Measurement Unit Movement Dual System

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MOQ
$1015/Pieces
Price
RS232 MEMS IMU Inertial Measurement Unit Movement Dual System
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Features
Specifications
Usage: Position Sensor
Theory: Capacitance Sensor
Output: Optional
Product Name: MEMS Integrated Inertia Navigation System
Range: ±300
Resolution: <0.005
Acceleration Sensitivity: <10°/h/g,rms Direction
Angle Random Walk: <0.15
Interface Type: Micro-DB9,RS422
Input Voltage: 9-36V(Ripple 50mV)
Horizontal Position Estimation Accuracy: 2M
Pure Inertial Position: <40m@1min
Azimuth Accuracy: 0.3°,P=50%@30m/s
Port: SHENZHEN
High Light:

RS232 IMU Inertial Measurement Unit

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IMU Inertial Measurement Unit Dual System

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MEMS inertial movement unit

Basic Infomation
Place of Origin: Guangdong, China
Brand Name: RION
Certification: CE
Model Number: IMU560-422
Payment & Shipping Terms
Packaging Details: CARTON
Delivery Time: 7 days
Payment Terms: T/T, Paypal
Supply Ability: 1000 Bag/Bags per Month
Product Description

IMU560 series GPS+MEMS Dual System Inertial Navigation Module/gps module rs232

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

 


.

    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 

RS232 MEMS IMU Inertial Measurement Unit Movement Dual System 0
Our Company
RS232 MEMS IMU Inertial Measurement Unit Movement Dual System 2
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Get in touch with us
Contact Person : Alice Du
Tel : 86-15625295088
Fax : 86-755-29761269
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