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Minimum integrated altitude for the terminal bunt manoeuvre
Author(s) -
Subchan S.
Publication year - 2007
Publication title -
pamm
Language(s) - English
Resource type - Journals
ISSN - 1617-7061
DOI - 10.1002/pamm.200700283
Subject(s) - terminal (telecommunication) , missile , altitude (triangle) , trajectory , low altitude , path (computing) , aerospace engineering , surface (topology) , fixed wing , control theory (sociology) , geodesy , aeronautics , control (management) , engineering , mathematics , computer science , geology , physics , wing , geometry , telecommunications , artificial intelligence , astronomy , programming language
This paper presents trajectory shaping of a surface‐to‐surface missile attacking a fixed target with varying flight‐path angle. The problem is reinterpreted using optimal control theory resulting in the formulation of minimum integrated altitude. (© 2008 WILEY‐VCH Verlag GmbH & Co. KGaA, Weinheim)
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