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The HTS-IMU4 Inertial measurement unit is a small, non-GPS-aided inertial measurement unit weighing only 55 grams. It is suitable for a variety of commercial and military guidance and navigation applications. It has the same gyro performance as the HTS-E3/1A gyroscope module (alternative STIM210 Sensonor) and an accelerometer zero bias repeatability of less than 0.2 mg. The HTS-IMU4 inertial measurement unit has 3 built-in inclinometers to ensure accurate system leveling and provides an external synchronization signal input. The IMU (inertial measurement unit) is temperature compensated over a wide operating range, and all axes are mechanically and electrically aligned relative to the package reference plane. The HTS-IMU4 inertial measurement unit is not sensitive to magnetic fields. For higher-priced and heavier FOG-based inertial measurment systems, it is a relatively reliable, cost-effective inertial measurement unit. Its output format, sampling rate, filter settings, and data packet content can be set by the customer.


Features:                                                                                                                                                                                            Applications:

• Three-axis gyro zero bias instability is 0.05°/h                                                                                                                                     • Inertial navigation research and production                                                                            

• Three-axis gyro angle random walk is 0.02°/√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/40g/80g                                                                                                           • Unmanned equipment control

• Built-in inclinometer and 24-bit analog-to-digital conversion                                                                                                                • Attitude measurement and control

• Support external trigger input


Performance Characteristics

Speci

Unit

Model

HTS-IMU4

HTS-IMU4A

HTS-IMU4B

HTS-IMU4C

HTS-IMU4F

Gyro

Range (customizable)

°/s

±400

±400

±400

±2000

±300

Zero bias

°/h

15

10

5

30

3

Bias instability (@Allan error)

°/h

0.3

0.1

0.05

1

0.05

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

°/h

3

2

0.4

6

0.2

Bias repeatability

°/h

3

1

0.3

3

0.2

Bias error within full temperature range

°/h

20

10

2

30

1

Random walk

°/√h

0.15

0.05

0.02

0.3

0.02

Bias acceleration sensitivity

°/h/g

2

2

2

2

1

Resolution

°/h

2

1

0.5

5

2

Output noise (half peak)

°/s

0.3

0.25

0.15

0.45

0.03

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

IV Type

Accelerometer

Range (customizable)

g

±10

±40

±80

±10

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

mg

0.05

0.2

1

0.05

Bias repeatability

mg

0.2

1

0.5

0.3

Bias error within full temperature range 

mg

2

2

5

1

Resolution

mg

0.1

Bandwidth

Hz

125

100

Scale factor non-linearity

ppm

500

Scale factor repeatability

ppm

500

Cross coupling

%

0.1


Speci

Unit

Standard Type

Inclinometer

Range (customizable)

g

±1.7

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

mg

0.5

Scale factory non-linearity

ppm

500

Others

Stable start time

s

1

Data rate

Hz

1000

Voltage

V

5±0.5

Steady state power consumption

W

1.5

Ripple

mV

100

Working temperature

-45~85

-55~85

Storage temperature

-55~105

-55~105

Weight

g

55±5

Size

mm

44.8×38.6×20

Interface

——

RS-422

Dimension and Drawing

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