Telephone: | 86-15148215714 |
E-MAIL : | yang_fan@forsense.cn |
Position : | Room 4F,Building 16,No. 1000 JinhaiRoad, City of Elite,,Pudong New Area,Shanghai |
Sample purchase |
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
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
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)