2010•Fire Control and Command ControlRequires access

Three-dimensional Trajectory Simulation of Air Defense Missile based on Matlab

Gao Zhong-chang

Open publisher page 0 citations

Abstract

A method for three-dimensional trajectory simulation of air defense missile based on matlab is studied.The guidance law and the trajectory simulation are presented.Taking the proportional guidance method as an example,air defense missile trajectory simulation modeling is established and the three-dimensional simulation of missile trajectory is protracted on Matlab language.The choice of some parameters and its influence on trajectory are discussed among the rest.Finally,the influence of the missile and target velocity including the guidance coefficient on the simulation trajectory and the encounter time are analyzed.The results of simulation show that this method is significant in improving trajectory optimization design.

About this research paper

What this paper is about

A method for three-dimensional trajectory simulation of air defense missile based on matlab is studied.The guidance law and the trajectory simulation are presented.Taking the proportional guidance method as an example,air defense missile trajectory simulation modeling is established and the three-dimensional simulation of missile trajectory is protracted on Matlab language.The choice of some parameters and its influence on trajectory are discussed among the rest.Finally,the influence of the missile and target velocity including the guidance coefficient on the simulation trajectory and the encounter time are analyzed.The results of simulation show that this method is significant in improving trajectory optimization design.

Why it matters

A significance statement is not available in the OpenAlex record.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

A method for three-dimensional trajectory simulation of air defense missile based on matlab is studied.The guidance law and the trajectory simulation are presented.Taking the proportional guidance method as an example,air defense missile trajectory simulation modeling is established and the three-dimensional simulation of missile trajectory is protracted on Matlab language.The choice of some parameters and its influence on trajectory are discussed among the rest.Finally,the influence of the missile and target velocity including the guidance coefficient on the simulation trajectory and the encounter time are analyzed.The results of simulation show that this method is significant in improving trajectory optimization design.

Key concepts: Trajectory, Missile, MATLAB, Missile guidance, Computer science, Control theory (sociology), Computer simulation, Trajectory optimization

Related papers

Back to paper searchBrowse research topicsOriginal source
Three-dimensional Trajectory Simulation of Air Defense Missile based on Matlab — Research Paper | ScholarLens