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Introduction FSS-IMU16460-C is a 6-degree-of-freedom MEMS inertia
Volume 22.4*22.4*9.0
Weight 8.6g
Application field Autonomous driving: vehicle mounted, robot, underwater, engineering machinery stable platform: pan tilt, in motion communication automatic control: self-control system, fixed wing unmanned aerial vehicle
Software interface TTL
Hardware interface Molex Pico Clasp 6-Pin
86-15148215714
DetailTechnical IndexDownloadHardware and Structu

FSS_IMU16460-C is a 6_DOF MEMS inertial sensor module created by Forsense. It comes standard with the output of 3-axis gyroscope and 3-axis acceleration information.

High precision and high resolution can capture subtle vibrations and tilts. A wide range of output makes it possible to sense motion under large dynamics. All modules are equipped with ultra_wide temperature range refined temperature compensation and independent calibration before leaving the factory, so that each module can perform stably under various extreme working conditions, while ensuring that the performance of all products is highly consistent.

Application Areas

  • Autonomous driving: vehicle_mounted, robot, engineering vehicle, underwater

  •         Precision measurement: underground, tunnel, vibration, tilt

  •         Stable platform: PTZ, dynamic communication

  •         Automatic control: automatic control system, fixed-wing UAV

Characteristic

Tactical-Grade MEMS Gyroscope

  • 1.5 °/hr Bias instability

  • 0.12°/√hr Angular random walk

  • 0.04 °/s Temperature drift (-40℃~85℃, ≤1℃/min @1σ)

Tactical-Grade MEMS Accelerometers

  • 20 μg Bias instability

  • 0.02 m/s/√hr Speed Random Walk

  • 1.0 mg Temperature Drift (-40~85℃, ≤1℃/min @1σ)

Wide range of refined temperature compensation

  • -40℃ to 85℃ temperature compensation

  • Fine temperature calibration

Independent turntable calibration

  • Independent calibration of each module: sensitivity, zero bias, non-positiveCross Error

High intensity working condition tolerance

  • Super strong impact resistance: 2000g (0.5ms, half sine, 3axis

  • Super strong vibration tolerance: 10g (10~2KHz, 3axis

  • Stable operation in full temperature environment: -40℃~85℃

  • 100%Magnetic shielding

Real-time and flexible digital interface, compact size

  • Configurable output sampling rate up to 1KHz

  • Support serial port interface

  • 22.4*24.02*9.0mm, weight 8.6g


Gyroscope Key Metrics

Parameters

Test Condition/Remark

Min.

Typ.

Max.

Unit

Measurement Range



±300


°/s

Bias Instability¹

@25℃, ALLAN Variance, 1σ


1.5


°/hr

Bias stability

GJB,10s smooth

4


°/hr

Bias Repeatability

GJB

XY: 10

Z: 20


°/hr

Resolution



0.0088


°/s

Misalignment



0.02


deg

Internal Low-pass Cutoff Frequency

Adjustable software


49


Hz

ODR



1000


Hz

Measure Delay



7


ms

Offset Error over Temperature²

-40 ~ 85℃, ≤1℃/min @1σ


0.04


°/s

Random Walk

@25℃, ALLAN Variance, 1σ


XY: 0.15

Z: 0.12


°/√hr

Scale Coefficient Error

2


Scale Factor Nonlinear



200


ppm

Note 1: IEEE standard values acquired from Allan Variance analysis in a static environment (25°C)

Note 2: 1σ variation of full-temperature bias at a heating rate of 1°C/min


Accelerometer Key Metrics

Parameters

Test Conditions/Remarks

Min.

Typ.

Max.

Unit

Measurement Range



±16


g

Bias instability¹

@25℃, ALLAN Variance, 1σ


XY: 25

Z: 20


μg

Bias stability

GJB,10s smooth

50


μg

Bias Repeatability

GJB

0.2


mg

Resolution



0.244


mg

Misalignment

0.02


deg

Internal Low-pass Cutoff Frequency

Adjustable Software


49


Hz

ODR



1000


Hz

Measure Delay



7


ms

Offset Error over Temperature²

-40 ~ 85℃, ≤1℃/min @1σ


1.0


mg

Random Walk

@25℃, ALLAN Variance, 1σ


0.02


m/s/√hr

Scale Coefficient Error



0.5


Scale Factor Nonlinear



100


ppm

Note 1: IEEE standard values acquired from Allan Variance analysis in a static environment (25°C)

Note 2: 1σ variation of full-temperature bias at a heating rate of 1°C/min



External Structure

Outline Structure and Dimensions (unit: mm)