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Introduction FSS-IMUP9 is a 6-degree-of-freedom MEMS inertial s
Volume 38.6*44.8*21.5mm
Weight 48.5g
Application field Aerial surveying and mapping
Product features Tactical grade MEMS gyroscope, tactical grade MEMS
Software interface RS422
Hardware interface J30J-15TJL
86-15148215714
DetailTechnical IndexDownloadHardware and Structu

IMUP9 is a MEMS inertial measurement unit (IMU) with 6 degrees of freedom (DOF) developed by Forsense (Shanghai) Technology Co., Ltd. It features three_axis gyroscopes and three_axis accelerometers, measuring angular velocity and linear acceleration respectively.

High precision and high resolution combine to help capture subtle vibration and tilt. A large number of output parameters enable the perception of motion despite intense shaking. All IMU modules are calibrated independently on a rotary table and adjusted precisely over an ultra_wide temperature range in a temperature chamber before leaving the factory, so that they can deliver stable and consistent performance in most extreme conditions.


Features

MEMS Gyroscope

●Bias Instability: 0.2°/hr

●Angle Random Walk: 0.015°/√hr

●Temperature Drift: 30°/hr

(-40℃ ~ 85℃,≤1℃/min @1σ)

MEMS Accelerometer

●Bias Instability: 15μg

●Velocity Random Walk: 0.02m/s/√hr

●Temperature Drift: 0.5mg (-40℃ ~ 85℃,≤1℃/min @1σ)

Refined temperature compensation

●Temperature Compensation: -40℃ to 85℃

●Precise Temperature Calibration

Independent Rotary Table Calibration

●Sensitivity, bias instability, and misalignment

●Providing a user interface for calibrating installation errors

High-intensity Tolerance

●Ultra Shock Resistance: 2000g(0.5ms,Half-sine shock pulse,3-axis)

●Superb Vibration Resistance: 10g(10~2KHz,3-axis)

●Ultra-wide Operating Temperature Range: -40℃ to 85℃

●100% Magnetic Shielding

Benefits

●Real-time and Flexibility: Configurable output sampling rate up to 1KHz

●Digital Interface: RS-422

●Small Size and Low Weight: 38.6*44.8*21.5mm, about 48.5g


Gyroscope Key Metrics

Parameter

Test Conditions/ Remarks

Min.

Typ.

Max.

Unit

Measurement Range



±300


°/s

Bias instability

@25℃, ALLAN Variance, 1σ


XY:0.2

Z: 0.15


°/hr

Bias stability

GJB, 10s smooth


1.5


°/hr

Bias Repeatability

GJB

7


°/hr

Misalignment

0.01


deg

Internal Low-pass

Cutoff Frequency

Adjustable software


68


Hz

Sampling Rate



1000


Hz

Measure Delay



5.5


ms

Offset Error over

Temperature¹

-40℃ ~ 85°C

≤1℃/min @1σ


XY: 30

Z: 10


°/hr

Random Walk²

@25℃, ALLAN Variance, 1σ


0.1


°/√hr

Scale Coefficient Error



1.0


Scale Factor Nonlinear



100

200

ppm

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

Note 2: IEEE standard values acquired from Allan Variance analysis in a static environment (25°C)

Accelerometer Key Metrics

Parameter

Test Conditions/Remarks

Min.

Typ.

Max.

Unit

Measurement Range



±8


g

Bias Instability

@25℃, ALLAN Variance, 1σ


15


μg

Bias stability

GJB, 10s smooth


25


°/hr

Bias Repeatability

GJB

0.1


mg

Misalignment



1.5313


deg

Internal Low-pass Cutoff Frequency

Adjustable software


75


Hz

Sampling Rate



1000


Hz

Measure Delay



5.5


ms

Offset Error over

Temperature¹

-40~85℃

≤1℃/min @1σ


0.5


mg

Random Walk²

@25℃, ALLAN Variance, 1σ


0.02


m/s/√hr

Scale Coefficient Error

0.2


Scale Factor Nonlinear

50


ppm

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

Note 2: IEEE standard values acquired from Allan Variance analysis in a static environment (25°C)

External Structure

Outline Structure and Dimensions (unit: mm)

ch2 图3 外形结构及尺寸.jpg

IMU Array Center (unit: mm)

ch2 图4 IMU 测量中心位置.jpg