Multi-Objective Optimal Control of Re-entry and Abort Scenarios

Abstract

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Robust Trajectory Optimisation of a TSTO Spaceplane Using Uncertainty-Based Atmospheric Models

“…It works for arbitrarily connected multi-phase problems with general dynamics, and ensures an even spread set of solutions within the Pareto-optimal set. The software has been successfully used for the trajectory and design optimisation of vertical and horizontal launch systems [10,11], deployment of constellations [12], interplanetary exploration missions [13] and the design of multi-debris removal missions.…”