Bandwidth-based performance analysis of terminal guidance system

Author

Baiyang Zhu ; Baoqing Yang ; Zhaohaoran Zhang ; Yu Yao

Author_Institution

Harbin Inst. of Technol., Harbin, China

fYear

2015

fDate

23-25 May 2015

Firstpage

4683

Lastpage

4687

Abstract

The terminal guidance system of a missile is nonlinear. Therefore, traditional performance analysis methods of terminal guidance system are numerical. However, numerical methods have limitations in performance analysis. The bandwidth analytic expression is derived in this paper to analyze its principal influence factors. Then a new approach based on the bandwidth is present in this paper to analyze the performance of terminal guidance system followed by its applications in guidance and control. And the feasibility of this approach is proved by simulation. The result shows that this approach has advantages in performance analysis of terminal guidance system.

Keywords

missile guidance; numerical analysis; bandwidth analytic expression; bandwidth-based performance analysis; missile; numerical method; principal influence factor; terminal guidance system; traditional performance analysis method; Analytical models; Bandwidth; Mathematical model; Missiles; Performance analysis; Resonant frequency; Stability analysis; Bandwidth; Performance Analysis; Terminal Guidance System;

fLanguage

English

Publisher

ieee

Conference_Titel

Control and Decision Conference (CCDC), 2015 27th Chinese

Conference_Location

Qingdao

Print_ISBN

978-1-4799-7016-2

Type

conf

DOI

10.1109/CCDC.2015.7162752

Filename

7162752