Thesis Details

Beresheet Lunar Landing Simulation

Bachelor's Thesis Student: Karpíšek Jakub Academic Year: 2019/2020 Supervisor: Chudý Peter, doc. Ing., Ph.D. MBA
Czech title
Simulace přistání Beresheet na Měsíci
Language
English
Abstract

The goal of this bachelor's thesis was to compute the optimal lunar descent trajectory for the Beresheet spacecraft and develop a visualization environment for interpreting lunar descents. The optimal descent trajectory was computed using Bocop, an optimal control problem solver, and the environment was implemented in Java, using the LibGDX 3D engine. The optimal descent trajectory was found and it enables soft landing with 29.2 kg (6.8 %) of fuel left. Created environment enables users to see lunar descent trajectories in an intuitive way and to interact with the visualization.

Keywords

Beresheet, lunar landing, simulation, optimal descent trajectory, optimal control, bocop, libgdx

Department
Degree Programme
Information Technology
Files
Status
defended, grade A
Date
13 July 2020
Reviewer
Committee
Janoušek Vladimír, doc. Ing., Ph.D. (DITS FIT BUT), předseda
Chudý Peter, doc. Ing., Ph.D. MBA (DCGM FIT BUT), člen
Kořenek Jan, doc. Ing., Ph.D. (DCSY FIT BUT), člen
Rozman Jaroslav, Ing., Ph.D. (DITS FIT BUT), člen
Veselý Vladimír, Ing., Ph.D. (DIFS FIT BUT), člen
Citation
KARPÍŠEK, Jakub. Beresheet Lunar Landing Simulation. Brno, 2020. Bachelor's Thesis. Brno University of Technology, Faculty of Information Technology. 2020-07-13. Supervised by Chudý Peter. Available from: https://www.fit.vut.cz/study/thesis/22727/
BibTeX
@bachelorsthesis{FITBT22727,
    author = "Jakub Karp\'{i}\v{s}ek",
    type = "Bachelor's thesis",
    title = "Beresheet Lunar Landing Simulation",
    school = "Brno University of Technology, Faculty of Information Technology",
    year = 2020,
    location = "Brno, CZ",
    language = "english",
    url = "https://www.fit.vut.cz/study/thesis/22727/"
}
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