2010Jisuanji fangzhenRequires access

Study on Parabola-trajectory Simulation of Air-to-air Missile

Xiao-Dong Li

Open publisher page 0 citations

Abstract

The Parabola-Trajectory was proposed,for the purpose of increase the effective attack range of the short/medium range air-to-air missile.In order to solve the Parabola-Trajectory guidance problem,parabola-trajectory compound guidance law was studied through the separate simulation study of the parameters of the three guidance stages:initial,midcourse and terminal guidance stage.The parabola-trajectory simulation system was built,which includes three typical maneuver targets models.By the analyses of simulation results of attacking various targets with different heights and distances,the characteristics of the trajectory were shown.The simulation shows that the parabola-trajectory can effectively increase the attack range of the missile,and can be used in the missile's technical upgrade.

About this research paper

What this paper is about

The Parabola-Trajectory was proposed,for the purpose of increase the effective attack range of the short/medium range air-to-air missile.In order to solve the Parabola-Trajectory guidance problem,parabola-trajectory compound guidance law was studied through the separate simulation study of the parameters of the three guidance stages:initial,midcourse and terminal guidance stage.The parabola-trajectory simulation system was built,which includes three typical maneuver targets models.By the analyses of simulation results of attacking various targets with different heights and distances,the characteristics of the trajectory were shown.The simulation shows that the parabola-trajectory can effectively increase the attack range of the missile,and can be used in the missile's technical upgrade.

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

The Parabola-Trajectory was proposed,for the purpose of increase the effective attack range of the short/medium range air-to-air missile.In order to solve the Parabola-Trajectory guidance problem,parabola-trajectory compound guidance law was studied through the separate simulation study of the parameters of the three guidance stages:initial,midcourse and terminal guidance stage.The parabola-trajectory simulation system was built,which includes three typical maneuver targets models.By the analyses of simulation results of attacking various targets with different heights and distances,the characteristics of the trajectory were shown.The simulation shows that the parabola-trajectory can effectively increase the attack range of the missile,and can be used in the missile's technical upgrade.

Key concepts: Parabola, Trajectory, Missile, Missile guidance, Range (aeronautics), Air-to-air missile, Guidance system, Aerospace engineering

Related papers

Back to paper searchBrowse research topicsOriginal source
Study on Parabola-trajectory Simulation of Air-to-air Missile — Research Paper | ScholarLens