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MEMS Based Inertial Measurement Unit With High Performance

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Province/State:guangdong
Country/Region:china
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MEMS Based Inertial Measurement Unit With High Performance

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Brand Name :Firepower
Model Number :16497
Certification :CE ROHS
Place of Origin :CHINA
MOQ :1
Price :negotiable
Payment Terms :T/T,L/C
Supply Ability :500/month
Packaging Details :sponge/box
Product name :MEMS Inertial Measurement Unit
Measuring range :±500º/s
zero bias stability :1deg/h
Zero-bias repeatability :0.1deg/s
cale factor nonlinearity :0.02%F
accelerometer range :16g
Zero bias stability :0.5mg
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MEMS Based Inertial Measurement Unit With A High-Performance MEMS Gyroscope And Accelerometer

1. Product overview

The 16497C-C0-IMU is a micromachining technology (MEMS) based inertial measurement unit (IMU) with a high-performance MEMS gyroscope and MEMS

The accelerometer outputs 3 angular velocities and 3 accelerations.

The 16497C-C0-IMU features high reliability and strong environmental adaptability. By matching different software, the product can be widely used in intelligent driving, tactical and industrial UAV, intelligent ammunition, seeker, mobile communication, mapping, stable platform and other fields.

2. Product features

  1. Three-axis digital gyroscope:
    1. ± 500º/s dynamic measuring range;
    2. Zero bias stability: 5 °/H (GJB, 10s), 1.0 °/H (ALLAN);
  2. Triaxial digital accelerometer:
    1. ± 16 G dynamic measuring range;
    2. Zero-bias stability: 0.5mg (GJB, 10s), 0.1mg (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 channel UART, 1 channel SPI, 1 channel CAN

3. Field of application

  1. Intelligent driving
  2. Tactical and Industrial UAV
  3. Smart Munitions
  4. Seeker
  5. Communication in motion
  6. Mapping
  7. Stabilize the platform

4. Product indicators

Parameter Test conditions Minimum value Typical value Maximum value Unit
Dynamic measuring range 500 º/s
Zero bias stability

Allan variance

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

1.0

5

º/h

º/h

Peg-top

Zero bias

Zero-bias range

Zero bias change over full temperature range ○ 1

±0.2

±0.06

º/s

º/s

Scale factor

Scale factor accuracy

Scale factor nonlinearity

0.3

0.02

%

%FS

Resolution 3.052×107 º/s/LSB
Bandwidth 200 Hz
Dynamic measuring range 16

g mg mg mg mg

%

%FS

g/LSB

Hz

Zero bias stability

Allan variance

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

0.1

0.5

Accelerometer

Zero bias

Zero-bias range

Change of zero bias within full temperature range, peak-to-peak value ○ 1

2

2

Scale factor

Scale factor accuracy

Scale factor nonlinearity

0.3

0.02

Resolution 1.221×108
Bandwidth 200
Communication interface 1-way SPI Baud rate 15 MHz
Parameter Test conditions Minimum value Typical value Maximum value Unit
1-way UART Baud rate 230.4 Kbps
1-way CAN Baud rate 1 MHz
SPI 200 1000 Hz
Sampling frequency UART 200 Hz
CAN 200 Hz
Voltage 3.0 3.3 3.6 V
Electrical characteristics Power consumption 1.5 W
Ripple P-P 100 mV
Structural characteristics Size 47×44×14 mm
Weight 50 g

Use environment

Operating Temperature Storage Temperature

Vibration

Impact

-40 80
-45 85
20~2000Hz,
6.06g
1000g,0.5ms

Reliability

MTBF 20000 h
Continuous working time 120 h

IMU polarity definition

3 gyros and 3 accelerometers is defined as shown in the figure below, and the direction of the arrow is positive.

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