Research on the Method of Simulation Modeling on the Control System of Certain Missile

Author

Xi-Wei, Guo ; Zi-Hua, Kong ; Zhu-Lin, Wang

Author_Institution

Ordnance Eng. Coll. OEC, Shijiazhuang, China

fYear

2011

fDate

21-23 Oct. 2011

Firstpage

909

Lastpage

912

Abstract

The method of system simulation for analyzing fly condition of the missile has two advantages: it costs little, and the parameters can be set and recorded expediently. In this paper, the constitution method on simulation model of control system of certain missile is introduced for analyzing the fly condition of this missile. Firstly, principle and mathematic model are introduced based on the composition of control system. Then the simulation models of angle measurement link, nonlinear link and missile body and motion link are discussed in detail. At last, the simulation model for the whole control system is constituted, and it can be used to analyze the fly condition of this missile.

Keywords

angular measurement; missile control; motion control; nonlinear control systems; simulation; angle measurement link; constitution method; missile body; missile control system; missile fly condition; motion link; nonlinear link; simulation modeling method; Analytical models; Computational modeling; Control systems; Goniometers; Mathematical model; Missiles; Transfer functions; control system; mathematic model; missile; simulation model;

fLanguage

English

Publisher

ieee

Conference_Titel

Instrumentation, Measurement, Computer, Communication and Control, 2011 First International Conference on

Conference_Location

Beijing

Print_ISBN

978-0-7695-4519-6

Type

conf

DOI

10.1109/IMCCC.2011.229

Filename

6154255