Target maneuvering estimation algorithm based on target motion characteristics analysis

被引:0
|
作者
Yang Baoqing [1 ]
Yi Ru [1 ]
Wu Kaining [2 ]
Wu Jingchuan [1 ]
机构
[1] Harbin Inst Technol, Control & Simulat Ctr, Harbin 150080, Peoples R China
[2] Harbin Inst Technol Weihai, Dept Math, Huanctai Dist 264209, Weihai, Peoples R China
基金
中国国家自然科学基金;
关键词
Interacting Multiple Model; Unscented Kalman Filter; Tracking; Near Space; TRACKING;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper, the maneuvering target estimation algorithms is studied based on the near space hypersonic vehicle trajectory. Firstly, we analyze the possible maneuver forms. Basic description of typical target maneuvering scenarios is given such as cross range maneuver, longitudinal skip maneuver and terminal dive maneuver. Then, mathematical models of target maneuver estimation problems are obtained by combining the missile-target relative motion model and target maneuvering models. Moreover, this paper presents a target maneuvering estimation algorithm based on interacting multiple model with unscented Kalman filter (IMM-UKF). Finally, a simulation with different forms of target maneuvering is given to illustrate the effectiveness of the given filtering algorithm.
引用
收藏
页码:5605 / 5610
页数:6
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