2009•Fire Control and Command ControlRequires access

A 3-D Guidance Law for Air to Surface Missile

Chen Shengqi

Abstract

Three dimension kinematic model for air to surface missile is given, then a variable structure guidance law is designed considering the characteristics of surface maneuver target. Performance of the guidance system is analyzed theoretically. Guidance law proposed in the paper can be implemented conveniently in engineering as it needs little target information. Numerical simulation result sustains the effectiveness of the guidance law.

About this research paper

What this paper is about

Why it matters

OpenAlex reports 1 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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

Key concepts: Missile, Kinematics, Guidance system, Missile guidance, Air-to-air missile, Surface (topology), Law, Aerospace engineering