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High-Stability IMU for Advanced Driver Assistance Systems ADAS

Shenzhen Fire Power Control Technology Co., LTD
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High-Stability IMU for Advanced Driver Assistance Systems ADAS

Brand Name : Firepower

Model Number : IMU115

Place of Origin : CHINA

MOQ : 1

Price : Negotiable

Payment Terms : T/T

Supply Ability : 200/MONTH

Delivery Time : 30 DAYS

Packaging Details : Sponge+ box

Range : ≥250 °/s

Bias stability : ≤3°/h

Acc Bias Stability : 0.12 mg

Acc Range : 4/16 g

Overall Dimension : 22.4mm X 22.4mm X 9.5mm

Random Vibration : 3g,20~2000Hz

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IMU115 MEMS inertial unit integrates 3-axis gyro and accelerometer, providing precise angular velocity and linear acceleration measurements. Features include ±250°/s gyro, ±4g accelerometer, and built-in compensation for temperature and installation errors. Compact and reliable, ideal for UAV navigation, autonomous driving, mapping, and stabilization.



1. Product features

1) Three-axis digital gyroscope:

a) ± 250º/s dynamic measuring range (500 °/s optional);

b) Zero bias stability: 10 °/h (GJB, 10s, typical value), 6.0 °/h(ALLAN, typical value);

2) Triaxial digital accelerometer:

a) ± 4g dynamic measurement range (configurable 16g);

b) Zero-bias stability: 0.12 mg (GJB, 10s), 0.065 mg (ALLAN);

3) High reliability: MTBF > 20000h;

4) Guaranteed accuracy within the full temperature range (-40 ℃ ~ 80 ℃):

built-in high-performance temperature calibration and compensation algorithm;

5) Suitable for working under strong vibration conditions;

6) Interface 1-way UART.

2. Field of application

Intelligent driving

Communication in motion

Mapping

Stabilize the platform

3. Product indicators

Table 1 Product indicators

Parameter

Test conditions

Minimum value

Typical value

Maximum value

Unit

Gyroscope

Dynamic measuring range

250

500

º/s

Zero bias
stability

Allan variance

3.0

º/h

10 s average (-40 ℃ ~ + 80 ℃, constant temperature)

6.0

º/h

Zero bias

Zero bias
range

±0.2

º/s

Zero bias variation over
full temperature range1

±0.3

º/s

Scale factor

Scale factor accuracy

0.2

%

Scale factor nonlinearity

0.02

%FS

Bandwidth

80

Hz

Accelerometer

Dynamic measuring range

4

16

g

Zero bias
stability

Allan variance

0.065

mg

10 s average (-40 ℃ ~ + 80 ℃,
constant temperature)

0.12

mg

Zero bias

Zero bias
range

±3

mg

Zero bias change in full
temperature range, peak-to-peak value1

±6

mg

Scale factor

Scale factor accuracy

0.3

%

Scale factor nonlinearity

0.03

%FS

Bandwidth

80

Hz

Communication interface

1-way UART

Baud rate

115.2

460.8

Kbps

Sampling frequency

UART

200

1000

Hz

Electrical characteristics

Voltage

4.5

5

5.5

V

Power consumption

0.35

W

Ripple

P-P

20

mV

Structural characteristics

Size

22.4×22.4×9.5

mm

Weight

16

g

Use environment

Operating temperature

-40

80

Storage temperature

-45

85

Vibration

20~2000Hz,3g

Impact

1000g,0.5ms

Reliability

MTBF

20000

h

Continuous working time

120

h

1: Calculate the zero bias of the whole temperature change process, the temperature change rate is ≤ 1 ℃/min, and the temperature range is -40 ℃ ~ + 80 ℃;

structure outline


High-Stability IMU for Advanced Driver Assistance Systems ADAS


Product Tags:

UAV integrated optic gyroscope

      

sagnac effect integrated optic gyroscope

      
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