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• W2786483361 abstract "In the paper, the problem of minimum-fuel aeroassisted spacecraft regional reconnaissance (orbital hopping) is considered. A new nonlinear constrained optimal control formulation is designed and constructed so as to describe this mission scenario. This formulation contains multiple exo-atmospheric and atmospheric flight phases and correspondingly, two sets of flight dynamics. The constructed continuous-time optimal control system is then discretized via a multi-phase global collocation technique. The resulting discrete-time system is optimized using a newly proposed gradient-based optimization algorithm. Several comparative simulations are carried out and the obtained optimal results indicate that it is effective and feasible to use the proposed multi-phase optimal control design for achieving the aeroassisted vehicle orbital hopping mission." @default.
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• W2786483361 date "2018-04-01" @default.
• W2786483361 modified "2023-10-03" @default.
• W2786483361 title "Optimal fuel consumption finite-thrust orbital hopping of aeroassisted spacecraft" @default.
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• W2786483361 doi "https://doi.org/10.1016/j.ast.2017.12.026" @default.
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