2009Acta ArmamentariiRequires access

Research on 3D Terminal Guidance Laws Based on Actively Self-homing Spiral Variable Trajectory

Hongchao Zhao

Open publisher page 1 citations

Abstract

Design scheme of 3D guidance laws(GLs) based on actively self-homing spiral variable trajectory for the supersonic antiship missile was proposed to solve that the friendly missile can either evade the enemy interceptor or hit the sea maneuver target.Geometric relation models of relative motions among the missile,the interceptor and the ship were established;spiral variable trajectory of the missile during the course of pursuit was realized by making angular rate of lineof-sight-angle(LOSA) track the given spiral variable trajectory command signal based on the adaptive sliding mode variable structure control idea to evade the enemy interceptor;angular rate of LOSA during the course of flying was approached to zero by selecting the reasonable parameters to ensure that the friendly missile can hit the sea maneuver ship.The simulated results show that the GLs can either make the antiship missile perform actively spiral variable trajectory,i.e.make the miss amount of the enemy interceptor reach the minimum of 209.233 m at the time of 4.41 s,or hit the sea maneuver ship at the precision indicated by the miss amount of 0.932 m.

About this research paper

What this paper is about

Design scheme of 3D guidance laws(GLs) based on actively self-homing spiral variable trajectory for the supersonic antiship missile was proposed to solve that the friendly missile can either evade the enemy interceptor or hit the sea maneuver target.Geometric relation models of relative motions among the missile,the interceptor and the ship were established;spiral variable trajectory of the missile during the course of pursuit was realized by making angular rate of lineof-sight-angle(LOSA) track the given spiral variable trajectory command signal based on the adaptive sliding mode variable structure control idea to evade the enemy interceptor;angular rate of LOSA during the course of flying was approached to zero by selecting the reasonable parameters to ensure that the friendly missile can hit the sea maneuver ship.The simulated results show that the GLs can either make the antiship missile perform actively spiral variable trajectory,i.e.make the miss amount of the enemy interceptor reach the minimum of 209.233 m at the time of 4.41 s,or hit the sea maneuver ship at the precision indicated by the miss amount of 0.932 m.

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

Design scheme of 3D guidance laws(GLs) based on actively self-homing spiral variable trajectory for the supersonic antiship missile was proposed to solve that the friendly missile can either evade the enemy interceptor or hit the sea maneuver target.Geometric relation models of relative motions among the missile,the interceptor and the ship were established;spiral variable trajectory of the missile during the course of pursuit was realized by making angular rate of lineof-sight-angle(LOSA) track the given spiral variable trajectory command signal based on the adaptive sliding mode variable structure control idea to evade the enemy interceptor;angular rate of LOSA during the course of flying was approached to zero by selecting the reasonable parameters to ensure that the friendly missile can hit the sea maneuver ship.The simulated results show that the GLs can either make the antiship missile perform actively spiral variable trajectory,i.e.make the miss amount of the enemy interceptor reach the minimum of 209.233 m at the time of 4.41 s,or hit the sea maneuver ship at the precision indicated by the miss amount of 0.932 m.

Key concepts: Missile, Trajectory, Control theory (sociology), Spiral (railway), Terminal guidance, Variable (mathematics), Missile guidance, Engineering

Related papers

Back to paper searchBrowse research topicsOriginal source
Research on 3D Terminal Guidance Laws Based on Actively Self-homing Spiral Variable Trajectory — Research Paper | ScholarLens