Nine Axis Digital Electric Compass Inclinometer Sensor HEC395 with Heading Accuracy 0.3-0.5 Degree

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Product
Nine Axis Digital Electric Compass Inclinometer Sensor HEC395 with Hea...
Posting date : Nov 13, 2017
Membership
Free Member Scince Nov 02, 2017
FOB Price
100-800 USD
Min. Order Quantity
1 PCS
Supply Abillity
10000 PCS/MONTH
Port
SHANGHAI
Payment Terms
TT Or PAYPAL
Package
12*12*6 cm
Keyword :
Category
Contact
Hanson
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Product Detail
Company Info
 
Quick Detail
Place of Origin
China [CN]
Brand Name
ZTS
Model Number
HEC395
HS-CODE
-
Package & Delivery Lead Time
Package
12*12*6 cm
Delivery Lead Time
3-5 days
Specifications
Type of Certification
CE.RoHS,ISO
Reference no.
6192210816
Name.
CE
Start Date (validity period)
0000-00-00
End Date (validity period)
0000-00-00
Detailed Description

IntroductionUnmanned vehicles are performing progressively more complex tasks-and requiring increasingly robust and accurate heading and orientation information. But existing AHRS modules leave too much room for error. They lose heading when encountering magnetic distortion; they suffer from errors when experiencing erratic motion; and often don’t provide accurate headings, even in a static environment. And at more than $2000 for a MEMS-based AHRS, it’s no wonder AHRS have only been integrated by a select few customers. So when there’s no room for error, HEC395 stays on track.The new HEC395 AHRS provides unparalleled heading accuracy when static, while moving and when encountering magnetic distortion. HEC395 employs a patented Kalman filtering algorithm that intelligently fuses Magnetic Sensors with gyros and accelerometers to overcome errors due to erratic motion and changes in the local magnetic field.And HEC395 is priced for commercial use — delivering more reliable heading than AHRS modules that cost twice as much.Features1. High Accuracy: 0.3-0.5°2. RS232/RS485/TTL Optional; Modbus Optional3. Widely working temperature: -40℃~+85℃4. Small size: L60*59*29mm5. Low power consumption6. Hard and soft iron correction with quality of calibration score7. User calibration proceduresPart of Applications1. Machine Equipment2. Solar tracking3. Bridge  Monitoring4. Building  Monitoring5. Excavation Tilt Monitoring6. Vehicle7. Slope Monitoring8. Construction Machinery9.  Platform Leveling10. Tower Crane11. Lifting Machinery12. Pole Tilt Monitoring13. Ship14. Agricultural Machinery15. Medical Devices16. UAV17. Antenna Adjustment18. Robot 

Performance Specifications
Parameters                                           Typical Units
Heading accuracy (static, compass mode) 0.3°  Deg RMS
Heading accuracy (dynamic motion or magnetic transient )
Resolution 0.01°
Max Dip Angle 85° Deg
Magnetometer Specifications
Parameters                      Typical                       Units
Calibrated Field Measurement Range ± 1.5 Gauss
Magnetic Resolution ± 0.5 mGauss
Tilt Specifications
Parameters                                            Typical Units
Pitch Accuracy Deg RMS
Roll Accuracy Deg RMS
Tilt Range All-attitude Deg
Tilt Resolution <0.01°
Calibration
Parameters                      Typical                       Units
Hard Iron Calibration Yes  
Soft Iron Calibration Yes  
Mechanical Specifications
Parameters Typical Units
Dimensions (L x W x H) 60*59*29 mm
Weight 140 g
Mounting Options Screw mounts/standoffs; horizontal  
Connector for RS-232 (RS485 and TTL available) 5-pin  
I/O Specifications
Parameters                                               Typical Units
Latency from Power-On < 50 mSec
Maximum Sample Rate 50 samples/sec
Communication Rate 2400 to 115200 baud
Output Formats Binary and NMEA0183  
Power Specifications
Parameters                                            Typical Units
Supply Voltage 5V VDC
Current Draw(Continuous Output) Max 40 mA
TYP 30
Environmental Specifications
Parameters                                            Typical Units
X Operating Temperature – 40 to85 °C
Storage Temperature – 40 to125 °C
Shock 3000 G
Vibration Z-Axis, Skewed Block, at 1, 2 & 4 G rms @ 10±1000 KHz for 30 min  
Humidity 70°C with 95% R.H .for 168 hrs.  

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