摘要
针对制约四轴飞行器的导航控制精度的主要因素,提出了基于卡尔曼滤波的四轴飞行器组合导航方法,该方法将MIMU(微惯性测量组合)与GPS(全球定位系统)导航的数据融合,进行MIMU/GPS组合导航。仿真实验和实际应用结果表明,该方法能够提高导航定位精度,具有良好的容错性。
Navigation control accuracy of Quadrocopter is the main factor restricting its application. Quadrocopte navigation algorithm was put forward based on Kalman filter. The method mixes MIMU and GPS together. The simulation experiment and practical application indicate that the method can improve the accuracy of navigation and positioning, and has good error toler-
出处
《武汉理工大学学报（信息与管理工程版）》
CAS
2012年第3期265-267,共3页
Journal of Wuhan University of Technology：Information & Management Engineering
基金
武汉理工大学自主创新研究基金资助项目(2010-ZY-ZDH-023)
