Mems Gyro Strap-down Flight Attitude System 02pw

These MEMS Gyro Strap-down Flight Attitude System 02PW is a low cost inertia system for MEMS gyro strap-down flight attitude system. It offers a variety of navigation information to the carrier, includes heading, pitch angle, roll angle, altitude, air speed, triaxial acceleration, triaxial angular rate and so on to fit a wide range of application needs such as aircraft, unmanned air vehicles, vehicles and other applications.
The 02PW consists of three-axis MEMS gyro, trixial accelerometer, trixial magnetic sensors, static pressure transducer and dynamic pressure transducer. With the 422 serial interface , internal strap-down algorithm and process unit, the 02PW can easily connect with GPS, GLONASS, CNSS to build the strap-down flight attitude system or strap-down inertial navigation system . The composition of the systems can be configured depending on the actual requirements.

(Integrated Navigation(INS/GPS))
*Setup Time3 min
*True Airspeeda 5m/s (airspeedi Y50km/h)
*Speed1m/s (RMS)
*HeadingStatic a 1A
*AttitudeStatic a 0.5A
*VoltageDC 27VA 10%
*Power Dissipation<30W