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Article Dans Une Revue IEEE Transactions on Automatic Control Année : 2020

Optimal Control of Endo-Atmospheric Launch Vehicle Systems: Geometric and Computational Issues

Résumé

In this paper we develop a geometric analysis and a numerical algorithm, based on indirect methods, to solve optimal guidance of endo-atmospheric launch vehicle systems under mixed control-state constraints. Two main difficulties are addressed. First, we tackle the presence of Euler singularities by introducing a representation of the configuration manifold in appropriate local charts. In these local coordinates, not only the problem is free from Euler singularities but also it can be recast as an optimal control problem with only pure control constraints. The second issue concerns the initialization of the shooting method. We introduce a strategy which combines indirect methods with homotopies, thus providing high accuracy. We illustrate the efficiency of our approach by numerical simulations on missile interception problems under challenging scenarios.
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Dates et versions

hal-01626869 , version 1 (31-10-2017)
hal-01626869 , version 2 (11-03-2019)

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Riccardo Bonalli, Bruno Hérissé, Emmanuel Trélat. Optimal Control of Endo-Atmospheric Launch Vehicle Systems: Geometric and Computational Issues. IEEE Transactions on Automatic Control, 2020, 65 (6), pp.2418--2433. ⟨10.1109/tac.2019.2929099⟩. ⟨hal-01626869v2⟩
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