Attitude And Heading Reference System Microelectromechanical Systems Small Volume And Weight|selectable Interface|high Accuracy|static|dynamnic|proven Technology|used In Demanding Conditions For Unmanned Vehicles (MEMS AHRS)
1. Brief introduction
TY421 is a low cost system which can be used in simple vehicle navigation “Satcom on the move” antenna platform stabilization. This MEMS gyro, MEMS accelerometer, as well as algorithm suitable for conical scanning of antenna and satellite data correction this system uses, makes the requirement of hardware reduce greatly. Finally, the combination of dual antenna GPS or magnetometer can provide precise navigation and position info for users.
(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.
≤1° 1σ (static)
≤2° 1σ (dynamic)
≤0.2°/ Baseline(GPS combined)
10 m (GPS combined)
Horizontal position accuracy
10m (CEP)(GPS combined)
0.02m/s (GNSS combined)
Meet the vehicle vibration requirement of GJB150.16A-2009
Working power dissipation
Data refresh rate
(1) “Satcom on the move” antenna stabilization
(2) Unmanned vehicles
If you are interested in the attitude and heading reference system microelectromechanical systems small volume and weight|selectable interface|high accuracy|static|dynamnic|proven technology|used in demanding conditions for unmanned vehicles (mems ahrs), consult the price with our manufacturers in China now. With advanced technology, our products take high accuracy, high precision, high sensitivity, high reliability, high performance, high stability and low cost as main advantages.