计算机与现代化Issue(3)：62-64,70,4.DOI:10.3969/j.issn.1006-2475.2015.03.013
基于改进自适应UKF算法的飞行器姿态确定
Aircraft Attitude Estimation System Based on Improved Adaptive UKF Algorithm
摘要
Abstract
To address the aircraft attitude estimation problem, Unscented Kalman Filter ( UKF) does not have the ability to over-come the disturbance. In order to obtain better estimation precision, an adaptive UKF is proposed. The algorithm can overcome the disturbance by introducing an adaptive factor to adjust the state gain matrix. The simulation results show the effectiveness of the proposed algorithm.关键词
飞行器姿态估计/UKF/自适应/估计精度Key words
aircraft attitude estimation/UKF/adaptive/estimation accuracy分类
信息技术与安全科学引用本文复制引用
郑均辉,张国平..基于改进自适应UKF算法的飞行器姿态确定[J].计算机与现代化,2015,(3):62-64,70,4.基金项目
河南省科技攻关基金资助项目(122102210258) （122102210258）
