Altitude Sensing Inertial Measurement Unit

Product Details
Customization: Available
Type: Inertial Measurement Unit
Output Signal Type: Digital Output
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Registered Capital
1000000 RMB
Plant Area
>2000 square meters
  • Altitude Sensing Inertial Measurement Unit
  • Altitude Sensing Inertial Measurement Unit
  • Altitude Sensing Inertial Measurement Unit
  • Altitude Sensing Inertial Measurement Unit
  • Altitude Sensing Inertial Measurement Unit
  • Altitude Sensing Inertial Measurement Unit
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Basic Info.

Model NO.
imu80
Accuracy Grade
Gyro: 4deg/H, Accelerometer: 10ug
Certification
ISO
Customized
Non-Customized
Interface
Spi / Uart
Power Supply
5VDC
Transport Package
Carton
Specification
23.4x 22.4x 8(mm)
Trademark
SkyMEMS
Origin
China
HS Code
9014100000
Production Capacity
2000/Month

Product Description

IMU80 Low Cost IMU Inertial Measurement Unit

Altitude Sensing Inertial Measurement Unit
Main Features
-High Precision 6 DoF MiniIMU with Full Calibration
-Fully Similar as ADIS16460, Better Performance
-3 Angular Rates and 3 Linear Acceleration Outputs
-Data OutputRate: 200Hz
-Range: Gyro ±400°/s, Accelerometer±6g
-Bias Instability: Gyro 4°/h, Accelerometer±10μg
-Compact and Light weight23.4x 22.4x 8(mm), <15g
-Wide Working Temperature: -40°C~+85°C


Altitude Sensing Inertial Measurement Unit
Brief Introduction
IMU80High PerformanceInertial Measurement Unit is a rugged industrial inertial navigation systemprovidingpreciseyaw, pitch, roll as well as 6-axis outputs of angular rate and acceleration at 200Hz.IMU80 adopts MEMS-based inertial sensors and extended Kalmanfilter algorithm, which provides super cost-effective solution for customers
IMU80 Inertial Measurement Unitenjoys small size and light weight, and it is housed in an ultra-durable and compact aluminum housing, it enjoys high reliability in harsh environment, ithas been widely applied in dynamic control systems and attitude systems including Unmanned Aircraft and ROVs, Smart Agriculture, Machine Control, Platform Stabilization, AGV,robotics,etc.


Altitude Sensing Inertial Measurement Unit
Technical Specifications
Parameter            Value
Min Typical Max
Gyroscopes
Range: -400°/s   +400°/s
Bias Instability 3°/h 4°/h 5°/h
Initial Bias Error 0.08°/s 0.1°/s 0.2°/s
Resolution   0.01°/s  
Scale Factor  Accuracy   0.10%  
Non-linearity   0.1%FS  
Random Walk 0.2º/√hr 0.3º/√hr 0.5º/√hr
Bandwidth   50Hz  
Accelerometers
Range: X, Y, Z -6g   +6g
Bias Instability 5μg 10μg 15μg
Initial Bias Error   3mg 4mg 5mg
Resolution   0.5mg  
Scale Factor  Accuracy   0.10%  
Non-linearity   0.1%FS  
Random Walk 0.03m/s/√hr 0.05m/s/√hr 0.07m/s/√hr
Bandwidth   50Hz  
Environment Conditions
Working Temperature -40~+85°C
Storage Temperature -55~+100°C
Housing Material  aluminum
Electrical Features
Input Power Supply 3.3VDC
Power Consumption <0.15W
Interface SPI / UART (optional)
Output Frequency 200Hz
Physical Parameter
Size 23.4 x 22.4 x 8mm
Weight <15grams
Connector 7*2 pins
Remarks g=9.80665 m/s2

Altitude Sensing Inertial Measurement Unit
Typical Applications
- Unmanned Aircraft and ROVs
- Smart Agriculture
- Machine Control
- Platform Stabilization
- AGV
- robotics




Altitude Sensing Inertial Measurement Unit

 

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