Triangle Intercept Guidance for Aerial Defense

Takeshi Yamasaki; S. N. Balakrishnan

doi:10.2514/6.2010-7876

Triangle Intercept Guidance for Aerial Defense

Takeshi Yamasaki
, S. N. Balakrishnan

Missouri University of Science and Technology

Research output: Contribution to journal › Article › peer-review

Abstract

This paper focuses on missile guidance methods 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 simple geometrical approach. The potential of the guidance law is demonstrated and discussed with some simulation results. Performance comparison with a conventional guidance law is also presented. Copyright © 2010 by Takeshi Yamasaki and S.N. Balakrishnan.

Original language	American English
Journal	Proceedings of the AIAA Guidance, Navigation, and Control Conference (2010, Toronto, ON)
DOIs	https://doi.org/10.2514/6.2010-7876
State	Published - Aug 5 2010

Disciplines

Aerospace Engineering
Mechanical Engineering

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https://doi.org/10.2514/6.2010-7876

Cite this

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title = "Triangle Intercept Guidance for Aerial Defense",

abstract = " This paper focuses on missile guidance methods 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 simple geometrical approach. The potential of the guidance law is demonstrated and discussed with some simulation results. Performance comparison with a conventional guidance law is also presented. Copyright {\textcopyright} 2010 by Takeshi Yamasaki and S.N. Balakrishnan.",

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AB - This paper focuses on missile guidance methods 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 simple geometrical approach. The potential of the guidance law is demonstrated and discussed with some simulation results. Performance comparison with a conventional guidance law is also presented. Copyright © 2010 by Takeshi Yamasaki and S.N. Balakrishnan.

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Triangle Intercept Guidance for Aerial Defense

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