Computational Optimal Control of the Terminal Bunt Manoeuvre
This work focuses on a study of missile guidance in the form of trajectory shaping of a generic cruise missile attacking a fixed target which mu ·t be struck from above. The problem is reinterpreted using optimal control theory resulting in two formulations: I ) minimum time-integrated altitude and...
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| Language: | en |
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Cranfield University
2016
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/11047 |