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What is Robust Control for Planetary Landing about?

This thesis focuses on developing an adaptive guidance algorithm for planetary landing that updates the trajectory to the surface by solving an optimal control problem to minimize fuel consumption. A semi-analytical approach is used where the trajectory is expressed as a polynomial satisfying 17 boundary conditions. By imposing these conditions, a determined guidance profile is obtained as a function of time of flight and initial thrust. The optimal guidance computation is reduced to determining these param

Author

Freddy Aguirre

Language

EN