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IMU-600M-31A

By I-NAV Technology Co., Ltd. ↗

A MEMS inertial unit for unmanned aerial vehicles.

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I-NAV Technology Co., Ltd. IMU-600M-31A MEMS Inertial Unit
I-NAV Technology Co., Ltd. IMU-600M-31A MEMS Inertial Unit
Positioning interfacesBuilt-in magnetometer and external GNSSGNSS is external.
Gyroscope specificationsRange ±300°/s; bias stability 10°/h; bias repeatability 10°/hBias stability and repeatability are specified at 1σ.
Accelerometer specificationsRange ±6g; bias stability ≤200μg; bias repeatability ≤200μgBias stability and repeatability are specified at 1σ.
CalibrationFull-temperature-range precision calibration

Product overview

The unit incorporates a magnetometer and supports an external GNSS connection for positioning.

The gyroscope has a range of ±300°/s. Its bias stability and bias repeatability are both specified as 10°/h at 1σ.

The accelerometer has a range of ±6g. Its bias stability and bias repeatability are both specified as ≤200μg at 1σ.

The unit uses precision calibration across its full temperature range.

Specifications

SpecificationValue & conditions
Positioning interfacesBuilt-in magnetometer and external GNSSGNSS is external.
Gyroscope specificationsRange ±300°/s; bias stability 10°/h; bias repeatability 10°/hBias stability and repeatability are specified at 1σ.
Accelerometer specificationsRange ±6g; bias stability ≤200μg; bias repeatability ≤200μgBias stability and repeatability are specified at 1σ.
CalibrationFull-temperature-range precision calibration
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