An Interacting-Multiple-Model Method for Tracking a Hypersonic Glide Target

被引：0

作者：

Huang, Jingshuai ^{[1
]}

Zhang, Hongbo ^{[1
]}

Wu, Shang ^{[2
]}

Tang, Guojian ^{[1
]}

Bao, Weimin ^{[1
,3
]}

机构：

[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Peoples R China

[2] Sci & Technol Complex Aviat Syst Simulat Lab, Beijing 10076, Peoples R China

[3] China Aerosp Sci & Technol Corp, Beijing 100048, Peoples R China

来源：

PROCEEDINGS OF THE 32ND 2020 CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2020) | 2020年

关键词：

Hypersonic Glide Target; Target Tracking; Singer Model; Interacting Multiple Model; Unscented Kalman Filter;

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 terms of tracking a hypersonic glide target (HGT), a tracking method is proposed based on interacting-multiple-model (IMM). Target tracking mainly contains two missions: system modeling and choosing filtering algorithm. First, a tracking system is established composed of state and measurement equations on basis of ground-based radar measuring. The Singer model is used to represent the unknown aerodynamic acceleration. Then, to enhance model adaptation of the tracking method, three-model interacting filter is constructed with maneuver-frequency adaption based on unscented Kalman filter (UKF). Through tracking a flight trajectory generated by Gauss Pseudospectral Method, the effectiveness of the proposed method is validated and the multiple-model is superior to the single-model.

引用

页码：1702 / 1707

页数：6

共 2 条

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[2] Coupled dynamic model of state estimation for hypersonic glide vehicle [J].

Zhang Kai ;

Xiong Jiajun ;

Fu Tingting .

JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2018, 29 (06) :1284-1292

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