Triangle Intercept Guidance for Aerial Defense
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.
T. Yamasaki and S. N. Balakrishnan, "Triangle Intercept Guidance for Aerial Defense," Proceedings of the AIAA Guidance, Navigation, and Control Conference (2010, Toronto, ON), American Institute of Aeronautics and Astronautics (AIAA), Aug 2010.
The definitive version is available at https://doi.org/10.2514/6.2010-7876
AIAA Guidance, Navigation, and Control Conference (2010: Aug. 2-5, Toronto, ON)
Mechanical and Aerospace Engineering
Article - Conference proceedings
© 2010 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
05 Aug 2010