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Channel: Gyros & Inertial Sensor | AHRS, Magnetometer, Accelerometer, GPS & Magnetic Compass | Watson Industries » Heading Reference | Gyros & Inertial Sensor | AHRS, Magnetometer, Accelerometer, GPS & Magnetic Compass | Watson Industries
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Strapdown Heading Reference SHR-S360 (Gyro-Stabilized)

The SHR-S360 is the smallest version of our Strapdown Heading Reference line of sensors. This product uses MEMS gyros to make the SHR-S360 more economical and slightly smaller than the SHR-E360 heading...

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Strapdown Heading Reference SHR-E360 (Gyro-Stabilized)

The SHR-E360 provides heading and sensor information. It includes a high accuracy triaxial fluxgate magnetometer, a triaxial accelerometer, and an angular rate gyro. This unit is a “strapdown” or...

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Strapdown Heading Reference SHR-360

The SHR-360 provides heading and sensor information. It includes a high accuracy triaxial fluxgate magnetometer and a triaxial accelerometer. This unit is a “strapdown” or “body-axis” sensor. The...

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Inertial Measurement System DMS-SGP02 (Dual Antenna GPS)

The DMS-SGP02 is a miniaturized version of the DMS-EGP02. To allow for a smaller package, the DMS-SGP02 uses our S series MEMS rate gyro. The DMS may be used in almost any application where triaxial...

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Inertial Measurement System DMS-EGP02 (Dual Antenna GPS)

Originally developed to meet the needs of automotive testing professionals, the Dynamic Measurement System (DMS) was designed for monitoring the drive and handling characteristics of vehicles. The DMS...

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GPS Compass Magnetometer GCM-360

The GCM-360 is a unique product for defining the magnetic field of the earth. This unit provides heading, GPS coordinates and sensor information. It includes a high accuracy triaxial fluxgate...

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Attitude & Heading Reference System AHRS-S305

The AHRS-S305 is Watson Industries’ newest Attitude and Heading Reference System. Standard for an attitude gyro system, the AHRS-S305 has a sensor package that consists of three solid state angular...

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Attitude & Heading Reference System AHRS-E304

The signals from three solid state angular rate sensors are coordinate transformed and then integrated to produce attitude and heading outputs that reflect normal aircraft attitude coordinates. These...

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