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تفاصيل المنتجات

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مقياس تسارع IMU الدوران
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Advanced MEMS Inertial Measurement Unit Sensor with 0.2° Bias Honeywell HG4930C IMU

Advanced MEMS Inertial Measurement Unit Sensor with 0.2° Bias Honeywell HG4930C IMU

اسم العلامة التجارية: Firepower
رقم الطراز: HG4930C
الـ MOQ: 1
السعر: 2000$
شروط الدفع: L/C,D/A,D/P,T/T,Western Union
القدرة على التوريد: 500/month
معلومات مفصلة
Place of Origin:
China
Gyro Measuring range:
±200°/s
Zero-bias stability (@ Allan variance):
0.2°/h
Zero-bias stability (10 s smoothing, 1σ, room temperature):
0.5°/h
Random walk:
0.02°/√h
Scale Factor Repeatability (1σ ):
1°/h
3 dB Bandwidth:
100Hz
Accelerometer bias stability:
30ug
Acc Measuring range (customizable):
30g
Weight:
120g
Power consumption:
1.5W
Packaging Details:
BOX+Sponge
Supply Ability:
500/month
إبراز:

Honeywell Inertial Measurement Unit,Advanced MEMS Inertial Measurement Unit,0.2° Bias Inertial Measurement Unit

,

Advanced MEMS Inertial Measurement Unit

,

0.2° Bias Inertial Measurement Unit

وصف المنتج

Advanced MEMS Inertial Measurement Unit Sensor with 0.2° Bias Honeywell HG4930C IMU


  • Product Description

  MEMS Inertial Measurement Unit (IMU) consists of three-axis gyroscope, three-axis accelerometer, temperature sensor, signal processing board, structure and necessary software, and is used for measuring the three-axis angular rate, three-axis acceleration and three-axis inclination angle of a carrier. And output the data of the gyroscope and the accelerometer after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation and etc) through RS-422 serial port according to an agreed communication protocol.

  • Technical Parameters

Gyroscope Specifications

Parameter

Unit

HG4930C

Measuring range (customizable)

°/s

±200

Zero-bias stability (@ Allan variance)

°/h

0.2

Zero-bias stability (10 s smoothing, 1σ, room temperature)

°/h

0.5

Zero-bias error over full temperature range

°/h

2.5

Random walk

°/√h

0.02

Zero-bias repeatability

°/h

1

Zero bias acceleration sensitivity

°/h/g

1

Resolution

°/h

2

Scale factor nonlinearity

ppm

100

Scale factor repeatability

ppm

100

Cross coupling

%

0.2

Bandwidth

Hz

100


            Accelerometer Technical Indicators

Parameter

Unit

HG4930C

Measuring range (customizable)

g

±30

Zero-bias stability (Allan Variance @ 25 ℃)

ug

30

Zero-bias stability (1s smoothing)

ug

700

Zero-bias error over full temperature range

mg

1.5

Random walk

m/s/√h

0.01

Zero-bias repeatability

mg

2

Scale factor repeatability

ppm

200

Scale factor nonlinearity

ppm

200

Cross coupling

%

0.2

Bandwidth

Hz

100


Electrical Characteristics

Parameter

Unit

HG4930C

Voltage

V

5

Power consumption

W

1.5

Ripple

mV

100


 Environmental Adaptability

Parameter

Unit

HG4930C

Operating temperature

-45~85

Storage temperature

-60~105

Vibration

--

10~2000Hz,6.06g

Impact

--

15000g,4ms


  • Outline Structure

Advanced MEMS Inertial Measurement Unit Sensor with 0.2° Bias Honeywell HG4930C IMU 0