Geometrical Approach-Based Defense-Missile Intercept Guidance for Aircraft Protection Against Missile Attack
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.
T. Yamasaki et al., "Geometrical Approach-Based Defense-Missile Intercept Guidance for Aircraft Protection Against Missile Attack," Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, SAGE Publications, Jan 2012.
The definitive version is available at http://dx.doi.org/10.1177/0954410011416053
Mechanical and Aerospace Engineering
Article - Journal
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