Attitude Heading Reference System Microelectromechanical Systems Small Volume and Weight|selectable Interface|high Accuracy|static|dynamnic|proven Technology|used In Demanding Conditions for Unmanned Aerial Vehicle (MEMS AHRS)

Attitude Heading Reference System Microelectromechanical Systems Small Volume And Weight|selectable Interface|high Accuracy|static|dynamnic|proven Technology|used In Demanding Conditions For Unmanned Aerial Vehicle (MEMS AHRS)

1. Brief introduction

TY421 type MEMS AHRS is R & D by the Xi'an Jierui. This product uses MEMS gyro and MEMS accelerometer, as well as a mature attitude calculation algorithm, can autonomously complete the attitude calculation function in harsh environmental conditions, can also provide heading by being combined with dual antenna GPS or magnetometer. And the combination of dual antenna GPS can continuously and real-time provide the instant position (longitude and latitude), velocity, acceleration, heading and attitude of the aircraft.

2. Features

(1) Auto-output  of navigation information

(2) Meet the requirement of accurate measurement of attitude angle of aircraft, when in large maneuver flight and hovering.

(3) Small volume and weight.

(4) Communication interface RS422?CAN, to be selectable.

(5) Wide voltage input range.

(6) Can complete redevelopment according to customers’ requirement.

3. Performances

4. Applications

(1) Unmanned aerial vehicle

(2) Unmanned surface vessel

(3) Counter-terrorism, search for and rescue.

(4) Robots, unmanned vehicles

5. Packages

E-mail: info@gyro-nav.com