摘要
提出了一种测速定轨的实时算法。该方法基于样条表示飞行轨道速度参数 ,在只有多个测速元信息的情况下 ,建立了自适应Kalman滤波递推算法 。
Based on spline filtering, this paper presents a novel self-adaptive approach for trajectory determination by using velocity measurements. The spline function is adopted to express the parameters of the trajectory so that an iterative algorithm of self-adaptive Kalman filter is established. When information of velocity measurement is merely provided, this approach can give real-time trajectory parameters of the aircraft with high precision .
出处
《国防科技大学学报》
EI
CAS
CSCD
北大核心
2001年第6期38-41,共4页
Journal of National University of Defense Technology
基金
国家自然科学基金 ( 6 9872 0 39)
教育部振兴计划高校骨干教师资助计划项目