Ditemukan 1 dokumen yang sesuai dengan query
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This paper presents trajectory shaping of a surface-to-surface missile attacking a fixed with terminal impact angle
constraint. The missile must hit the target from above, subject to the missile dynamics and path constraints. The
problem is reinterpreted using optimal control theory resulting in the formulation of minimum integrated altitude. The
formulation entails nonlinear, two-dimensional missile flight dynamics, boundary conditions and path constraints. The
generic shape of optimal trajectory is: level flight, climbing, diving; this combination of the three flight ...
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Lembaga Penelitian Universitas Indonesia, 2007
Artikel Jurnal Universitas Indonesia Library
