Flight Test of the Quadrotor based on Algorithm of Multi-sensor Fusion

摘要：

　　This paper introduces a multi-sensor fusion technology and verify Whether the integrated navigation system is valid.IMU and GPS/ barometer is complementary,the formers long-term stability is poor and short-term stability is good,and the latter is just the opposite.Therefore,the fusion algorithm can be used to combine the three data,the output of three-dimensional position information,speed information,attitude information,to provide navigation information for quadrotor.In loiter mode,fluctuations of roll channel and elevation channel are reduced,height tracking situation is better.

关键词： Kalman filter integrated navigation system flight test

作者: Lingyu Liu Xinhua Wang Qingyan Tan

作者单位: Nanjing University of Aeronautics and Astronautics,China

会议类型: 国际会议

会议名称: 2016信息技术和机电一体化工程国际会议

会议地点: 重庆

会议语种:英文

页码: 323-328

在线出版日期: 2016-05-21（万方平台首次上网日期，不代表论文的发表时间）