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Optimal guidance for space applications
2009 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

The first part of this study was focused on describe the state-of-art in optimization techniques for general space operations, and especially in landing operations. Numerous optimisation tools have been developed in the past years and may be profitably re-used in the frame of space operations. To take advantage of these developments, available software has to be compared, in terms of methods, performances and user-friendliness. Among the studied optimisation software, DIDO was selected for the second part of the study. In order to assess the performances of this Optimal Control Solver, tests have been performed on the asteroid landing scenario. Simulation results using the calculated optimal control profiles have shown the importance of the interpolation methods and the temporal resolution of the problem.

Place, publisher, year, edition, pages
2009.
Keyword [en]
Technology, GNC, DIDO, optimal control, guidance, optimization, asteroid, landing
Keyword [sv]
Teknik
Identifiers
URN: urn:nbn:se:ltu:diva-46801ISRN: LTU-PB-EX--09/115--SELocal ID: 46b26bfe-0023-4be8-aaef-352886087430OAI: oai:DiVA.org:ltu-46801DiVA: diva2:1020116
Subject / course
Student thesis, at least 30 credits
Educational program
Space Engineering, master's level
Examiners
Note
Validerat; 20101217 (root)Available from: 2016-10-04 Created: 2016-10-04Bibliographically approved

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CiteExportLink to record
Permanent link

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Citation style
  • apa
  • ieee
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  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
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