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Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable
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home
about us
Company Profile
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products

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable
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solutions
contact us
quote

products details

Created with Pixso. Home Created with Pixso. Products Created with Pixso.
IMU Accelerometer Gyro
Created with Pixso.

STIM300 Analog MEMS IMU Sensor , 3 Gyro Inertial Measurement Sensor

STIM300 Analog MEMS IMU Sensor , 3 Gyro Inertial Measurement Sensor

STIM300 Analog MEMS IMU Sensor , 3 Gyro Inertial Measurement Sensor

Brand Name: Firepower
Model Number: IMU6
MOQ: 1
Price: 3000~6000 USD
Payment Terms: T/T
Detail Information
Product Description
Detail Information
Place of Origin:
CHINA
Certification:
CE ROHS
Product Name:
9 Axis MEMS IMU
Gyro Measuring Range:
±400°/s
Zero-bias Stability:
≤ 1 °/H
Random Walk:
≤ 0.2 °/√ H
Resolution:
1 °/H
Scale Factor Nonlinearity:
500 Ppm
Bandwidth:
125Hz
Highlight:

Analog MEMS IMU Sensor

,

9 Axis MEMS IMU Sensor

,

125Hz Inertial Measurement Sensor

Product Description

STIM300 Analog MEMS IMU Sensor Low Price Inertial Measurement Sensor 3 Accelerometer, 3 Gyro, Pitch Rolll Heading Temp



Gyroscope specifications


Parameter Unit IMU6-1 IMU6-1A
Measuring range (customizable) °/s ±400 ±400

Zero bias stability

(@ Allan Variance)

 °/h 1 0.5

Zero bias stability

(1s smooth, 1σ, room temperature)

 °/h 10 5

Zero bias stability

(10s smooth, 1σ, room temperature)

 °/h 5 1
Zero-bias error over full temperature range °/h 20 10
Random walk °/√h 0.2 0.1
Zero-bias repeatability °/h 10 5
Zero bias acceleration sensitivity °/h/g 1 1
Resolution °/h 2 1
Scale factor nonlinearity ppm 500
Scale factor repeatability ppm 500
Cross coupling % 0.1
Bandwidth Hz 125



Add table technical indicators

Parameter Unit IMU6-1y-1 IMU6-1y-2
Measuring range (customizable) g ±10 ±30
Zero-bias stability (Allan Variance @ 25 ℃) mg 0.02 0.05
Zero-bias stability (1s smoothing) mg 0.1 0.5
Zero-bias stability (10 s smoothing) mg 0.05 0.2
Zero-bias error over full temperature range mg 1 3
Random walk m/s/√h 0.001 0.002
Zero-bias repeatability mg 0.1 0.5
Scale factor repeatability ppm 500
Scale factor nonlinearity ppm 500
Bandwidth Hz 125

The MEMS inertial measurement unit consists of a three-axis gyroscope, a three-axis acceleration meter, a three-axis inclination angle, a temperature sensor, a signal processing board, a structure and necessary software, and is used for measuring three-axis angular rate, three-axis acceleration and three-axis inclination angle of a carrier. And output that gyro, the loading table and the inclination data aft error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation and the like) through an RS-422 serial port according to an agreed communication protocol.

STIM300 Analog MEMS IMU Sensor , 3 Gyro Inertial Measurement Sensor 0


"IMU6-1y-x" in the drawing is the product code ". According to the product naming rules of the company," y "in IMU6-1y-x can be" A "," B "," C "or no letter to distinguish different performance index requirements, and" X "can be" 1 "," 2 "." 3 "and" 4 "to distinguish different product plus meter ranges. "XX-XXX" is the product number.

IMU6-1y-x IMU is installed through 3 Φ4.4 through holes, and installed with 3 M4 screws (with spring washer and flat washer). When installing the connector, the plug shall be locked with the socket and the cable shall be fixed. In the figureA,BIs the installation datum plane of the inertia group.

It is recommended that the flatness of the mounting surface opposite to the reference surface shall not be greater than 0.01 mm, the verticality shall not be greater than 0.02 mm, and the surface roughness shall not exceed 0.8 μm.




Tags: 

ADIS16488 IMU Accelerometer Gyro  

FOG IMU Inertial Measurement Unit  

MEMS Small Inertial Measurement Unit

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