Inertial Sense µINS - GNSS - INS RTK Sensor
Inertial Sense µINS is a miniature, GPS (GNSS) aided Inertial Navigation System (GPS-INS) RTK module
The Inertial Sense µINS is a miniature, GPS (GNSS) aided Inertial Navigation System (GPS-INS) module that includes all functionality of the µAHRS and provides orientation, velocity, and position. Base station corrections data can be applied to achieve CM level precision.
Inertial Sense
Salem, US
Description
The Inertial Sense µINS is a miniature, GPS (GNSS) aided Inertial Navigation System (GPS-INS) module that includes all functionality of the µAHRS and provides orientation, velocity, and position. Base station corrections data can be applied to achieve CM level precision.
Sensor data from MEMs gyros, accelerometers, magnetometers, barometric pressure, and GPS/GNSS is fused to provide optimal estimation.
Data out includes angular rate, linear acceleration, magnetic field, barometric altitude, and GPS time.
Specifications
-
Other specifications
-
Graphical user interface
Y
Typical application
Drones, unmanned vehicle navigation, stabilized platforms, robotics, personnel tracking.
Distinguishable features
Tiny, calibrated, easy to integrate, powerful, low cost, functional,
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Environmental
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Non-operating shock tolerance [g]
10000
Operating shock tolerance [g]
16
Min. operating temperature [°C]
-40
Max. operating temperature [°C]
85
Max. rotation speed [deg/s]
2000
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Software
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Name
EvalTool and SDK
Filtering
N
Adaptable filter strength
N/A
-
GNSS aided uncertainty
-
Heading [deg]
2
Heave: constant part [m]
5
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General
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Type of application
Air, Land, Marine
Year of initial development
2014
Min. Voltage (DC)
3
Max. Voltage (DC)
3
Splashproof casting
N
Water resistant casting
N
Water resistance [m]
0
Type of accelerometer
MEMS
Type of gyro
MEMS
Removable from base plate
Y
Moving parts
N
-
GNSS Positioning Sensor
-
Update rate [ Hz ]
5
Cold start [ seconds ]
10
Hot start [ seconds ]
120
-
Unaided uncertainty
-
Heading [deg]
2
-
Data formats
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NMEA formats
Yes
RTCM
N
Other
InertialSense Binary
-
Inertial Measurement Unit
-
Accelerometer bias [µ-g]
40
gyro bias [deg/hr]
10
-
GNSS positional accuracy
-
Horizontal Position Accuracy (SBAS) [ RMS in cm ]
3
Documents
Brochure
ins-datasheet
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