Author(s)

Jian Shen, Heng Li, Junwei Lei and Jing Li

Corresponding Author

Jian Shen

Abstract

Firstly, the history and development of Standard 2 missile are introduced, and the characteristics of various types of missiles in service are sorted out. On this basis, the parameters of propulsion system, flight system and aerodynamic configuration of Standard 2 missile are estimated, which provides a basis for the establishment of the following mathematical model.

Keywords

Parameter Estimation; Simulation; Missile; Control system; Standard II