Title

Geometrical Approach-Based Defense-Missile Intercept Guidance for Aircraft Protection Against Missile Attack

Abstract

This article develops a missile guidance technique for a “defense missile” trying to protect a cooperative aircraft from guided munitions which have the same thrust and maneuvering capabilities as that of the defense missile. A novel guidance law for the missile-to-missile intercept is developed via a geometrical approach. Performance of the guidance law is analysed in detail and its potential is demonstrated with results from a six degrees-of-freedom simulation and comparison with a conventional guidance law. © Authors 2011.

Department(s)

Mechanical and Aerospace Engineering

Document Type

Article - Journal

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 2012 SAGE Publications, All rights reserved.


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