Space trajectory optimization. Last stage of a launcher -- Space debris cleaning.

Max Cerf 1
Abstract : This work addresses two space trajectory optimization problems: the flight of a launcher upper stage and the collecting of space debris. For these two problems the goal is to develop solution methods and softwares usable in an industrial framework. The work consists of a theoretical part to formulate the problems and an applied part to develop numerical algorithms. The related fields are space mechanics, integer programming, nonlinear programming and optimal control.
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Submitted on : Saturday, September 29, 2012 - 11:04:34 AM
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  • HAL Id : tel-00736748, version 1

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Max Cerf. Space trajectory optimization. Last stage of a launcher -- Space debris cleaning.. Optimization and Control [math.OC]. Université Pierre et Marie Curie - Paris VI, 2012. English. ⟨tel-00736748⟩

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