Abstract: an integrated micro attitude heading reference system (MAHRS) was researched for micro aerial vehicles (MAV) based on the MEMS gyroscopes, accelerometers, and magnetic-sensors.
摘要：研究了基于硅mems陀螺、加速度计及磁阻式磁强计组合的微小型飞行器用姿态航向参考系统。
An integrated micro attitude heading reference system (MAHRS) was researched for micro aerial vehicles (MAV) based on the MEMS gyroscopes, accelerometers, and magnetic-sensors.
研究了基于硅mems陀螺、加速度计及磁阻式磁强计组合的微小型飞行器用姿态航向参考系统。
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