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High Reliability 6 Axis MEMS IMU Inertial Measurement Unit with Compact 2.24*2.23*1.37cm Dimensions for Navigation

High Reliability 6 Axis MEMS IMU Inertial Measurement Unit with Compact 2.24*2.23*1.37cm Dimensions for Navigation

High Reliability Mems Based Imu

6 Axis Mems Based Imu

6 Axis imu mems sensor

Place of Origin:

China

Brand Name:

Liocrebif

Certification:

GJB 9001C-2017

Model Number:

LKF-MSU104

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Product Details
Dimensions:
2.24*2.23*1.37cm
Color&Classification:
LKF-MSU104
Brand:
Liocrebif
Output Format:
RS422
Application:
Vibration Resistance And Attitude Control Of Industrial Equipment, Automated Control, Robot Control, Gimbal Stabilization And Control, Instrumentation, UAV/vehicle/ship/boat Attitude Reference, Mobile Mapping And Data Collection, Vehicle Positioning And Or
Original Place:
China
Highlight:

High Reliability Mems Based Imu

,

6 Axis Mems Based Imu

,

6 Axis imu mems sensor

Payment & Shipping Terms
Minimum Order Quantity
1
Price
5000-25000CHY
Packaging Details
Wooden box/Cardboard box/Container
Delivery Time
2-4 weeks
Payment Terms
T/T
Supply Ability
10000
Product Description
Product Overview
LKF-MSU104 MEMS Inertial Measurement Unit is a highly reliable, cost-effective six-axis MEMS IMU designed for navigation, control, and measurement applications in vehicles, ships, and unmanned aerial vehicles.
Essential Specifications
MOQ: 1
Dimensions: 2.24 × 2.23 × 1.37 cm
Model: LKF-MSU104
Technical Parameters
Parameters Technical Specification
Gyroscope
Range (°/s) ±400
Full-temperature zero bias (°/h, 3σ) ≤80
Bias stability (°/h, 10s smoothing) ≤5
Bias instability (°/h, Allan, typical) ≤1
Bias repeatability (°/h) ≤5
Angular random walk (°/√h) ≤0.3
Scale factor nonlinearity (ppm) ≤150
Cross-coupling (rad) ≤0.001
Bandwidth (Hz) ≥200Hz
Accelerometer
Range (g) ±10
Full-temperature zero bias (mg, 3σ) ≤5
Bias stability (μg, 10s smoothing) ≤300
Bias instability (μg, Allan, typical) ≤30
Bias repeatability (μg) ≤50
Velocity random walk (m/s/√h) ≤0.03
Scale factor nonlinearity (ppm, ±1g) ≤200
Cross-coupling (rad) ≤0.001
Bandwidth (Hz) ≥200Hz
Physical Characteristics
Power supply (V) 3.3V
Steady-state power (W) ≤1
Start-up time (s) ≤2
Communication interface One SPI, one UART
Update rate (Hz, max) 1000
Dimensions (mm × mm × mm) 22.4*22.3*13.7
Weight (g) 12±2
Operating Environment
Operating temperature (°C) -40~80
Storage temperature (°C) -55~85
Vibration (g, RMS) 20~2000HZ,6.06
Shock (g) 1000/1ms
Pin Definitions
No. Definition Type Note
1 DR Output Data Ready Indicator
2 SYNC Input/Output External Synchronous Input and Output
3 SPI1_SCK Input/Output SPI Serial Clock
4 SPI1_MISO Output SPI Data Output. The DOUT pin is clocked on the falling edge of SCLK
5 SPI1_MISI Input SPI Data Input. The DIN pin is clocked on the rising edge of SCLK
6 SPI_SS0 Input SPI Chip Select
7 UART_RX Input UART Input Port
8 NRST Input Reset
9 WM Output Watermark interrupt signal for tracking the fill level of a first-in-first-out (FIFO) queue
10 UART_TX Output UART output signal
11 VDD Power Positive Power supply positive
12 SWCLK Input SWD clock signal
13 GND Power Negative Power supply negative
14 SWD Output/Output SWD bidirectional data signal
Key Features
  • Three-axis digital gyroscope, range ±400°/s
  • Three-axis digital accelerometer, range ±10g
  • -40°C to +80°C full temperature calibration compensation (gyroscope and accelerometer)
  • Compatible with SPI serial communication
  • Built-in temperature sensor
  • Small size, light weight
  • Compatible with ADIS16575
Applications
  • Vibration resistance and attitude control of industrial equipment
  • Automated control
  • Robot control
  • Gimbal stabilization and control
  • Instrumentation
  • UAV/vehicle/ship/boat attitude reference
  • Mobile mapping and data collection
  • Vehicle positioning and orientation
Product Dimensions
High Reliability 6 Axis MEMS IMU Inertial Measurement Unit with Compact 2.24*2.23*1.37cm Dimensions for Navigation 0
Pin Definition Diagram
High Reliability 6 Axis MEMS IMU Inertial Measurement Unit with Compact 2.24*2.23*1.37cm Dimensions for Navigation 1

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