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• W4280498086 abstract "This paper studies a vertical powered descent problem in the context of planetary landing, considering glide-slope and thrust pointing constraints and minimizing any final cost. In a first time, it proves the Max-Min-Max or Max-Singular-Max form of the optimal control using the Pontryagin Maximum Principle, and it extends this result to a problem formulation considering the effect of an atmosphere. It also shows that the singular structure does not appear in generic cases. In a second time, it theoretically analyzes the optimal trajectory for a more specific problem formulation to show that there can be at most one contact or boundary interval with the state constraint on each Max or Min arc." @default.
• W4280498086 created "2022-05-22" @default.
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• W4280498086 date "2022-01-01" @default.
• W4280498086 modified "2023-10-17" @default.
• W4280498086 title "Structure of optimal control for planetary landing with control and state constraints" @default.
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• W4280498086 doi "https://doi.org/10.1051/cocv/2022065" @default.
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