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Adaptive guidance of short-range tactical missiles

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dc.contributor Graduate Program in Mechanical Engineering.
dc.contributor.advisor Kuzucu, Ahmet.
dc.contributor.author Ağabay, Özcan.
dc.date.accessioned 2023-03-16T11:17:39Z
dc.date.available 2023-03-16T11:17:39Z
dc.date.issued 1986.
dc.identifier.other ME 1986 Ag12
dc.identifier.uri http://digitalarchive.boun.edu.tr/handle/123456789/15158
dc.description.abstract Missile control methods are briefly outlined, the notation and conventions used in guided missile literature are introduced. A realistic simulation model is formed considering the differential equations governing motion of the missile in plane, the measurement and control system and the intercept geometry. Computer simulations are repeated for various attack geometries and target escape scenarios using both proportional navigation guidance and suboptimal adaptive control. Good missile performance in terms of miss distance is obtained for proportional navigation guidance. Suboptimal adaptive control can be more useful if other performance criteria are important, such as impact angle at target.
dc.format.extent 30 cm.
dc.publisher Thesis (M.S.) - Bogazici University. Institute for Graduate Studies in Science and Engineering, 1986.
dc.relation Includes appendices.
dc.relation Includes appendices.
dc.subject.lcsh Guided missiles -- Control systems.
dc.title Adaptive guidance of short-range tactical missiles
dc.format.pages xiii, 79 +A22 leaves;


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