Aircraft electronic compass HEC390

3D

Nine axis all attitude electronic compassHEC390 Product Introduction： HEC390 nine axis attitude heading reference system is a micro inertial sensor specially designed to provide high precision roll, pitch and azimuth measurements for magnetic interference and dynamic motion environments. Technical Specifications Heading Accuracy：0.3° (RMS，Static,Compass operating mode ) Pitch Accuracy：2º（RMS） Roll Accuracy：2º（RMS） Voltage：5V DC Output Mode：RS232/RS485/TTL Optional, Modbus Optional Dimension: 44×35×11mm Protection Level: IP67 If garbled characters appear on this manual when you preview online, please download it. This problem could be solved. We recommend Adobe Acrobat Reader DC. If still cannot, please contact us (sales@bwsensing.com), we will send you the newest manual via email. Thank you for your understanding. Designed by Bewis Sensing Technology LLC, HEC390 attitude heading reference System is an inertial product to provide high-precision roll, pitch and azimuth measurements for magnetic interférence and dynamic motion environments. The product includes a 9-degree-of-freedom sensor: a 3-axis accélération sensor, a 3-axis magnetic sensor and a 3-axis gyroscope. Through the optimized extended Kalman filter algorithm, the product outputs high-precision attitude information in real time. The HEC390 is specifically designed to improve the anti-jamming capability of the magnetic compass. It maintains high-precision orientation information when the iron interférence is close to.