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Navigation Grade MEMS IMU with 3 Axis Accelerometer Gyroscope

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Navigation Grade MEMS IMU with 3 Axis Accelerometer Gyroscope

Brand Name : FIREPOWER

Model Number : IMU6-4

Place of Origin : China

MOQ : 1

Payment Terms : L/C,T/T,Western Union

Supply Ability : 500/month

Delivery Time : 1 week for sample

Packaging Details : sponge +carton

Weight : 55±5g

Measuring range : ±400°/s

Zero-bias instability : 1°/h

Random walk : 0.15。/√h

Zero-bias repeatability : 10°/h

Zero bias acceleration sensitivity : 1°/h/g

Scale factor nonlinearity : 300ppm

Bandwidth : 250Hz

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1.1 Composition and function

The inertial measurement unit consists of three-axis gyroscope, three-axis acceleration meter, three-axis tilt angle (without this sensor by default), temperature sensor, signal processing board, structure and necessary software, and is used to measure the three-axis angular rate, three-axis acceleration and three-axis tilt angle of the carrier. And output the gyro, accelerometer and inclination data after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation and etc) through an RS-422 serial port according to an agreed communication protocol.

1.2 Main technical parameters

1.2.1 Gyroscope technical index

Parameter

Unit

Test conditions

IMU6-4

IMU6-4A

IMU6-4B

IMU6-4C

Measuring range

°/s

±400

±400

±400

±2000

Zero-bias instability

°/h

Allan variance

1

0.1

0. 05

3

Zero bias stability

°/h

1s smooth, RMS, normal temperature

10

5

1

20

Zero bias variation at full temperature

°/h

10s smooth, RMS, temperature change rate

1 ℃/min

20

10

2

40

Random walk

./√h

Allan variance

0.15

0.05

0.02

0.3

Zero-bias repeatability

°/h

Q = 6, normal temperature

10

5

1

20

Zero bias acceleration sensitivity

°/h/g

Test at ± 1 g

1

1

1

1

Resolution

°/h

2

1

0.5

5

Output noise

°/s

Peak (half peak, STD * 3)

0.3

0.25

0.15

0.45

Scale factor nonlinearity

ppm

Normal temperature

300

Scale factor repeatability

ppm

Q = 3, normal temperature

300

Cross coupling

%

Normal temperature

0.2

Bandwidth

Hz

250

250

150

250

1.2.2 Accelerometer technical index

Parameter

Unit

Test conditions

IMU6-4y-1

IMU6-4y-2

IMU6-4y

Measuring range

g

±10

±20

±40

Zero bias stability

mg

1s smooth, RMS, normal temperature

0.1

0.2

0.3

Zero bias variation at full temperature

mg

10s smooth, RMS, temperature change rate

1 ℃/min

3

3

5

Zero-bias repeatability

mg

Q = 6, normal temperature

0.2

0.5

1

Resolution

mg

0.1

0.1

0.1

Scale factor nonlinearity

ppm

Normal temperature

500

Scale factor repeatability

ppm

Q = 3, normal temperature

500

Cross coupling

%

Normal temperature

0.2

Bandwidth

Hz

150

1.2.3 Inclination angle technical index

Parameter

Unit

IMU6-4y-x

Measuring range

g

±1.7

Zero-bias stability (1s smoothing)

mg

0.5

Scale factor nonlinearity

ppm

500

1.2.4 Electrical characteristics

Parameter

Unit

IMU6-4y

Voltage

V

+5±0.5

Starting current

mA

<400

Steady-state power consumption

W

<1.2

Ripple

mV

100

1.2.5 Environmental adaptability

Parameter

Unit

IMU6-4y-x

Operating temperature

-45~85

Storage temperature

-55~105

1.2.6 Others

Parameter

Unit

IMU6-4y-x

Weight

g

55±5

Start time

s

1

Outline drawing

Navigation Grade MEMS IMU with 3 Axis Accelerometer Gyroscope


Product Tags:

navigation grade MEMS IMU sensor

      

3 axis accelerometer gyroscope

      

MEMS IMU with gyroscope

      
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