Trajectory Tracking for Hypersonic Glide Vehicles Based on Improved Sine-AIMM

被引:0
|
作者
Feng, Shan [1 ]
Tan, Qingke [1 ]
Li, Qingdong [1 ]
Ren, Zhang [1 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
maneuvering model; target tracking; hypersonic glide vehicle; IMM; Markov transition matrix;
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
To obtain a better performance of trajectory tracking for hypersonic glide vehicles (HGVs), this paper focuses on enhancing the accuracy of tracking model, an effective method with a modified tracking model is proposed. Firstly, according to the skip glide trajectory of HTV-2, a simplified trajectory model is established to describe the periodical characteristic of the trajectory. Secondly, a modified tracking model based on Sine model for HGVs is designed. Thirdly, for better model matching performance, an adaptive method is proposed to update the probability transition matrix of IMM. Finally, numerical simulation results are given to demonstrate that: interacting multiple model (IMM) algorithm based on the proposed Sine model is more accurate than that of Singer model, moreover, the adaptive IMM (AIMM) algorithm improves both the precision and the convergence rate of tracking for HGV.
引用
收藏
页码:5475 / 5480
页数:6
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