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2005•Journal of Projectiles.Rockets.Missiles and GuidanceRequires access

The Research of Laser Seeker for Terminal Guidance of Ballistic Missile

Wang Chen

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Abstract

The ballistic missile adopts the single guidance style that results the low accuracy.This paper presents a pro- ject that the missile terminal guidance is introduced through using the laser seeker.Based on the optimal control theory and the flighting dynamic principle the guidance law is derivated which takes into account the velocity and its direction of missile.The factors to realize this guidance law are presented.The models of this laser seeker are built.This paper can provide a reference for the future design.

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What this paper is about

The ballistic missile adopts the single guidance style that results the low accuracy.This paper presents a pro- ject that the missile terminal guidance is introduced through using the laser seeker.Based on the optimal control theory and the flighting dynamic principle the guidance law is derivated which takes into account the velocity and its direction of missile.The factors to realize this guidance law are presented.The models of this laser seeker are built.This paper can provide a reference for the future design.

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Available abstract

The ballistic missile adopts the single guidance style that results the low accuracy.This paper presents a pro- ject that the missile terminal guidance is introduced through using the laser seeker.Based on the optimal control theory and the flighting dynamic principle the guidance law is derivated which takes into account the velocity and its direction of missile.The factors to realize this guidance law are presented.The models of this laser seeker are built.This paper can provide a reference for the future design.

Key concepts: Missile, Ballistic missile, Missile guidance, Terminal guidance, Terminal (telecommunication), Laser, Guidance system, Aerospace engineering

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