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Virginia Polytechnic Institute and State University

Optimal and near-optimal medium range air-to-air missile guidance against maneuvering targets

Abstract

dc:description.abstract

Optimal intercept trajectories for a boost-sustain-coast medium-range air-to-air missile are synthesized using optimal control theory. Optimality in time/range/energy at intercept of a target is the main objective. Attainable sets and their boundaries are obtained and used to generate optimal intercept points in a three-dimensional scenario. A three-phase closed-loop guidance scheme is used to generate an efficient guidance law against a maneuvering target. In the present study, target maneuvers are restricted to the horizontal plane. An initial boost-phase with near-optimal guidance in the presence of active control constraints and thrust switches is simulated. Target maneuvers are neglected during this phase. A new method of gain evaluation is detailed. A midcourse guidance scheme with neighboring guidance, transversal comparisons, and chasing center-of-attainability of target to augment performance is studied. Modifications in terminal guidance using proportional navigation, such as chasing the center-of-attainability of target, altitude shaping, and drag-resolution schemes are used to attempt better performance at intercept. A composite guidance strategy using a combination of neighboring guidance and proportional navigation for the midcourse guidance is introduced. The excellent performance of this guidance strategy and the improvement in storage requirements for on-board use make it a very special scheme.

Degree

thesis:*
Name thesis:degree_name
Ph. D.
Level thesis:degree_level
doctoral
Discipline thesis:degree_discipline
Aerospace and Ocean Engineering
Department dc:contributor.department
Aerospace and Ocean Engineering
Grantor dc:publisher
Virginia Polytechnic Institute and State University
Year dc:date.issued
1989

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Kumar, Renjith R.
Chair dc:contributor.committeechair
  • Cliff, Eugene M.
Committee members dc:contributor.committeemember
  • Lutze, Frederick H.
  • Burns, John A.
  • Kraige, Luther
  • Mason, William

Rights

dc:rights
Statement dc:rights
  • In Copyright
Language dc:language.iso
en_US

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/10919/54224
OAI identifier oai:identifier
oai:vtechworks.lib.vt.edu:10919/54224

Chain of custody

source
Harvested from
Virginia Tech
Base URL
vtechworks.lib.vt.edu/oai/request
Last updated
2026-07-24
Source record
OAI-PMH GetRecord
related terms
citation

Kumar, Renjith R.. Optimal and near-optimal medium range air-to-air missile guidance against maneuvering targets. doctoral thesis, Virginia Polytechnic Institute and State University, 1989. http://hdl.handle.net/10919/54224