Trajectory optimization of a reusable launch vehicle

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

Riccardi, Annalisa ORCID: https://orcid.org/0000-0001-5305-9450

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• Item metadata

  Item type:	Conference or Workshop Item(Speech)
  ID code:	72574
  Dates:	Date Event 29 June 2019 Published
  Keywords:	optimal control, reusable launch vehicle, access to space, trajectory optimization, astronautics, Motor vehicles. Aeronautics. Astronautics, Aerospace Engineering
  Subjects:	Technology > Motor vehicles. Aeronautics. Astronautics
  Department:	Faculty of Engineering > Mechanical and Aerospace Engineering Strategic Research Themes > Ocean, Air and Space
  Depositing user:	Pure Administrator
  Date deposited:	04 Jun 2020 13:35
  Last modified:	31 Aug 2022 18:35
  Related URLs:	Event
  URI:	https://strathprints.strath.ac.uk/id/eprint/72574