Precision missile guidance for systems intercepting at small attack angles : a H‡ tracking approach
Contribuinte(s) |
Vadakkepat, Prahlad |
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Data(s) |
01/01/2003
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Resumo |
This paper uses the H1 tracking ideas in the missile guidance problem. The controller performs as a Precision guidance controller for small desired attack angles although theoretically the formulas are valid (when intercepting a maneuvering target in a precision guidance point of view) only for the case of head on collision. The controller essentially navigates the missile in a unique relative arc that is de ned by the missile and target location and the desired attack angle.<br /> |
Identificador | |
Idioma(s) |
eng |
Publicador |
CIRAS Organising Committee |
Relação |
http://dro.deakin.edu.au/eserv/DU:30005035/pathirana-precisionmissile-2003.pdf |
Direitos |
2003, CIRAS |
Tipo |
Conference Paper |