2002Journal of Projectiles.Rockets.Missiles and GuidanceRequires access

A New Method for Time-to-go using the Acceleration Along the Axis of Missile

LI Yan-jun

Open publisher page 0 citations

Abstract

The estimation of the time-to-go is very important in the missile terminal guidance.For the infrared seeker,the distance distance and velocity between the missile and the target are not accurately available because the missile and the target are maneuverable.Under the condition,a new method is derived,which the target maneuver is considered.

About this research paper

What this paper is about

The estimation of the time-to-go is very important in the missile terminal guidance.For the infrared seeker,the distance distance and velocity between the missile and the target are not accurately available because the missile and the target are maneuverable.Under the condition,a new method is derived,which the target maneuver is considered.

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 estimation of the time-to-go is very important in the missile terminal guidance.For the infrared seeker,the distance distance and velocity between the missile and the target are not accurately available because the missile and the target are maneuverable.Under the condition,a new method is derived,which the target maneuver is considered.

Key concepts: Missile, Acceleration, Missile guidance, Terminal guidance, Computer science, Control theory (sociology), Aerospace engineering, Engineering

Related papers

Back to paper searchBrowse research topicsOriginal source
A New Method for Time-to-go using the Acceleration Along the Axis of Missile — Research Paper | ScholarLens