Adaptive guidance of short-range tactical missiles

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.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.format.pages	xiii, 79 +A22 leaves;
dc.identifier.other	ME 1986 Ag12
dc.identifier.uri	https://digitalarchive.library.bogazici.edu.tr/handle/123456789/15158
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

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