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Helicopter Attitude, Heading and Reference System (AHRS) / 直升機姿態,航向參考系統(AHRS)
Attitude, Heading and Reference Systems, AHRS in short, are 3-axis sensor
systems which provide real-time 3D data concerning the attitude and positioning
of helicopter by calculating pitch, roll and heading. In many cases, AHRS sensors experience gyro bias drifts, which can lead to a misreading of the aircraft’s true trajectory. In order to counter that, AHRS require a filter structure and independent measurements from accelerometers so that they might provide the initial attitude reference and on-flight corrections required to correct the bias drifts. The MEMS sensorsDesigned to replace traditional gyro-based instruments, MEMS-based AHRS provide superior reliability and accuracy due to having 3-axis magnetic, 3-axis acceleration and 3-axis gyroscopic sensors. In order for the AHRS to work properly, all these sensors combine with a built-in processor to create an inertial sensor system able to measure the attitude of objects in 3D space. MEMS accelerometers provide exceptional levels of performance in terms of long-term stability, temperature stability and accuracy and are able to function successfully under harsh conditions. Colibrys MEMS accelerometerOur MS9000 sensor is available in various range from ±2g to ±200g and is part of the exclusive group of MEMS used in EASA, FAA and DAL A certified systems. The MS9000 is a single-axis analog accelerometer based on bulk micro-machined silicon elements. It is specifically designed for high bias stability over temperature in harsh environments. The MS9000 embeds a low-power ASIC (0.5 mA) and a temperature sensor. It comes fully calibrated from the get-go in a robust, hermetically-sealed LCC20 ceramic package, guaranteeing long-term stability and durability. |
公司電話:+886-2-26958906 上次更新日期: 2022年08月03日。 |