Trajectory optimization of a reusable launch vehicle
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Marchetti, Francesco and Minisci, Edmondo and Riccardi, Annalisa (2019) Trajectory optimization of a reusable launch vehicle. In: 17th Workshop on Advances in Continuous Optimization, 2019-06-28 - 2019-06-29, University of Strathclyde.
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Abstract
A comparison between different direct trajectory optimization methods for a Single Stage to Orbit Reusable Launch Vehicle is carried out and presented. Collocation and multiple-shooting approaches are compared in terms of accuracy, scalability, computational costs, and sensitivity to irregularities of models. The ascent trajectory optimization of the FESTIP-FSS5 Reusable Launch Vehicle is considered.
ORCID iDs
Marchetti, Francesco ORCID: https://orcid.org/0000-0003-4552-0467, Minisci, Edmondo ORCID: https://orcid.org/0000-0001-9951-8528 and Riccardi, Annalisa ORCID: https://orcid.org/0000-0001-5305-9450;-
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Item type: Conference or Workshop Item(Speech) ID code: 72574 Dates: DateEvent29 June 2019PublishedSubjects: Technology > Motor vehicles. Aeronautics. Astronautics Department: Faculty of Engineering > Mechanical and Aerospace Engineering
Strategic Research Themes > Ocean, Air and SpaceDepositing user: Pure Administrator Date deposited: 04 Jun 2020 13:35 Last modified: 15 Dec 2024 01:56 Related URLs: URI: https://strathprints.strath.ac.uk/id/eprint/72574
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