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We investigate the minimum time transfer of a satellite around the Earth. Using an optimal control model, we study the controllability of the system and propose a geometrical analysis of the optimal command structure. Furthermore, in order to solve the problem numerically, a new parametric technique is introduced for which convergence properties are established.
We investigate the minimum time transfer of a
satellite around the Earth. Using an optimal control model, we study
the controllability of the system and propose a geometrical analysis
of the optimal command structure. Furthermore, in order to solve the
problem numerically, a new parametric technique is introduced for
which convergence properties are established.
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