IMU-KERNEL-100
High Precision Inertial Measurement Unit and Digital Tilt Sensor (Pitch & Roll)
The Inertial Labs MEMS KERNEL Inertial Measurement Units & Digital Tilt Sensors are the latest addition to the Inertial Labs Advanced Miniature MEMS sensor-based family. Revolutionary due to its very compact, self-contained strapdown, industrial-grade Inertial Measurement Systems that measures linear accelerations and angular rates with three-axis MEMS accelerometers and three-axis MEMS gyroscopes.
Description
The Inertial Labs MEMS KERNEL Inertial Measurement Units & Digital Tilt Sensors are the latest addition to the Inertial Labs Advanced Miniature MEMS sensor-based family. Revolutionary due to its very compact, self-contained strapdown, industrial-grade Inertial Measurement Systems that measures linear accelerations and angular rates with three-axis MEMS accelerometers and three-axis MEMS gyroscopes. Angular rates and accelerations are determined with low noise and very good repeatability for both motionless and dynamic applications.
The Inertial Labs KERNEL-100 is the breakthrough, fully integrated inertial solution that combines the latest MEMS sensor technologies. Fully calibrated, temperature compensated, mathematically aligned to an orthogonal coordinate system, the IMU contains up to 2 deg/hr Bias in-run stability gyroscopes and 0.01 mg Bias in-run stability accelerometers with very low noise and high reliability.
Continuous Built-in Test (BIT), configurable communications protocols and flexible input power requirements make the Inertial Labs KERNEL easy to use in a wide range of higher order integrated system applications.
The Inertial Labs KERNEL models were designed for applications, like:
- Autonomous vehicles
- Antenna and Line of Sight Stabilization Systems
- Passengers trains acceleration / deceleration and jerking systems
- Motion Reference Units (MRU) and Motion Control Sensors (MCS)
- Gimbals, EOC/IR, platforms orientation and stabilization
- GPS-Aided Inertial Navigation Systems (INS)
- Attitude and Heading Reference Systems (AHRS)
- Land vehicles navigation and motion analysis
- Buoy or Racing Boat Motion Monitoring
- UAV & AUV/ROV navigation and control
Parameter KERNEL-100
GYROSCOPES
Measurement range: ±2000 deg/sec
Gyroscopes Bias in-run stability: 2 deg/hr
Gyroscopes Bias instability (over temperature range): 72 deg/hr
Gyroscopes Noise - Angular Random Walk: 0.38 deg/√hr
ACCELEROMETERS
Measurement range: ±8 g
Accelerometers Bias in-run stability: 0.01 mg
Accelerometers Bias instability (over temperature range): 0.7 mg
Accelerometers Noise - Velocity Random Walk: 0.02 m/sec/√hr
PITCH & ROLL ACCURACY
Pitch & Roll accuracy: 0.05 deg
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Specifications
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Environment
-
Min. operating temperature [C]
-40
Max. operating temperature [C]
85
Vibration
8 g, 10 – 2000 Hz
Shock
1500 g
-
Power Supply
-
Min. Voltage (DC)
4
Max. Voltage (DC)
15
Power consumption [W]
0.365
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Accelerometers
-
Num. of Accelerometers
3
Range [max g]
15
Bandwidth [ Hz ]
260
Alignment Error [ ± ° ]
0.0086
In-Run Bias Stability [mg]
0.03
Non-linearity [ % ]
0.08
Noise
0.045 m/sec/√hr
-
Operational
-
Interface types
Digital
Interfaces
RS-422
Output frequency [ Hz ]
2000
-
Gyroscopes
-
Num. of Gyroscopes
3
Range [± ° / sec]
2000
In-Run Bias Stability [ °/ hr]
2
Bandwidth [ Hz ]
260
Non-linearity [ % ]
0.035
Alignment Error [ ± ° ]
0.0086
Noise
0.38 deg/√hr
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General
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System components
Accelerometer(s), Gyroscope(s), Temperature sensor
Year of last update
2020
Year of initial development
2020
Height [mm]
8.5
Width [mm]
19.5
Length [mm]
26.5
Weight [gr]
7
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Accuracy
-
Heading static accuracy [ ° ]
0.05
Pitch and Roll static accuracy [ ° ]
0.05