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The HTS-IMU7 MEMS Based Inertial Measurement Unit  is a high peformance, affordable, non-GPS-aided inertial measurement unit, which consists of cost-effective MEMS gyrocope chip and MEMS accelerometer chip, its drive pickup circuit, temperature sensor, digital signal processing circuit, a structure and software, etc. It’s used to measure three-axis angular velocity and three-axis acceleration of the carrier in real time. This IMU uses flexible connection technology, built-in full temperature compensation, installation misalignment angle compensation, nonlinear compensation and other compensation algorithms, and can output stable and reliable measurement data for users after error compensation under static, dynamic and harsh conditions.


Features:                                                                                                                                                                                            Applications:

• Three-axis gyro zero bias instability is 5°/h                                                                                                                                          • Inertial navigation research and production

• Three-axis gyro angle random walk is 0.5°/√h                                                                                                                                     • Guidance and control system

• Three-axis accelerometer zero bias repeatability is 0.2mg                                                                                                                  • Mobile mapping platform attitude measurement

• Three-axis accelerometer range can be selected 10g/20g/50g                                                                                                           • Unmanned equipment control

• Gyro range up to 4000 °/s                                                                                                                                                                    • Attitude measurement and control

• Customized service provided


Performance Characteristics

Speci

Unit

Model

HTS-IMU6

HTS-IMU6A

HTS-IMU6B

HTS-IMU6C

HTS-IMU6F

Gyro

Range (customizable)

°/s

±400

±400

±400

±2000

±400

Zero bias

°/h

15

10

5

30

3

Bias instability (@Allan error)

°/h

0.3

0.1

0.05

1

0.03

Bias stability (10s smooth, 1σ, room temperature)

°/h

3

2

0.4

6

0.2

Bias repeatability

°/h

3

1

0.3

3

0.1

Bias error within full temperature range

°/h

20

10

2

30

1

Random walk

°/√h

0.15

0.05

0.02

0.3

0.01

Bias acceleration sensitivity

°/h/g

2

2

2

2

2

Resolution

°/h

2

1

0.5

5

0.3

Output noise (half peak)

°/s

0.3

0.25

0.15

0.45

0.15

Bandwidth

Hz

125

100

Scale factor non-linearity

ppm

100

Scale factor repeatability

ppm

100

Cross coupling

%

0.1


Speci

Unit

I Type

II Type

III Type

Accelerometer

Range (customizable)

g

±10

±20

±40

Bias stability (10s smooth, 1σ, room temperature)

mg

0.05

0.1

0.2

Bias repeatability

mg

0.2

0.5

1

Bias error within full temperature range 

mg

2

2

2

Resolution

mg

0.1

Bandwidth

Hz

100

Scale factor non-linearity

ppm

500

Scale factor repeatability

ppm

500

Cross coupling

%

0.1



Speci

Unit

Standard Type

Others

Stable start time

s

1

Data rate

Hz

1000

Voltage

V

5±0.25

Steady state power consumption

W

≤0.4

Ripple

mV

100

Working temperature

-45~85

Storage temperature

-55~105

Weight

g

12

Size

mm

22×20×10.2

Interface

——

RS-422


Dimension and Drawing




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