MEMS Based Inertial Measurement Unit With High Performance

Brand Name:Firepower
Certification:CE ROHS
Model Number:16497
Minimum Order Quantity:1
Payment Terms:T/T,L/C
Place of Origin:CHINA
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Location: Shenzhen Guangdong China
Address: 429, Building A10, Fuhai Information Port, Xinhe Community, Fuhai Street, Shenzhen, Guangdong, China
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Product Details

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

ParameterTest conditionsMinimum value Typical valueMaximum valueUnit
Dynamic measuring range500º/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

Resolution3.052×107º/s/LSB
Bandwidth200Hz
Dynamic measuring range16

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

Resolution1.221×108
Bandwidth200
Communication interface1-way SPIBaud rate15MHz
ParameterTest conditionsMinimum valueTypical valueMaximum valueUnit
1-way UARTBaud rate230.4Kbps
1-way CANBaud rate1MHz
SPI2001000Hz
Sampling frequencyUART200Hz
CAN200Hz
Voltage3.03.33.6V
Electrical characteristicsPower consumption1.5W
RippleP-P100mV
Structural characteristicsSize47×44×14mm
Weight50g

Use environment

Operating Temperature Storage Temperature

Vibration


Impact

-4080
-4585
20~2000Hz,
6.06g
1000g,0.5ms

Reliability

MTBF20000h
Continuous working time120h

IMU polarity definition

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


China MEMS Based Inertial Measurement Unit With High Performance supplier

MEMS Based Inertial Measurement Unit With High Performance

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