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: We present the numerical solution of an atmospheric reentry problemfor a space shuttle. We discretize the control and state with the same grid, and usea large-scale successive quadratic programming technique. With the help of slidinghorizon and successive refinement of the discretization, we can solve on a workstationa problem with 1600 time step, an unusually large figure for this kind of real worldoptimal control problem.Key-words: Optimal control, Discretization, Path following,...

Large-Scale Direct Optimal Control Applied to a Re-Entry Problem