CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • 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
  • rtf
Networked Model Predictive Control for Satellite Formation Flying
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology. Nasa Ames Research Center.
2019 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

A novel continuous low-thrust fuel-efficient model predictive control strategy for multi-satellite formations flying in low earth orbit is presented. State prediction relies on a full nonlinear relative motion model, based on quasi-nonsingular relative orbital elements, including earth oblateness effects and, through state augmentation, differential drag. The optimal control problem is specically designed to incorporate latest theoretical results concerning maneuver optimality in the state-space, yielding to a sensible total delta-V reduction, while assuring feasibility and stability though imposition of a Lyapunov constraint. The controller is particularly suitable for networked architectures since it exploits the predictive strategy and the dynamics knowledge to provide robustness against feedback losses and delays. The Networked MPC is validated through real missions simulation scenarios using a high-fidelity orbital propagator which accounts for high-order geopotential, solar radiation pressure, atmospheric drag and third-body effects.

Place, publisher, year, edition, pages
2019. , p. 91
Keywords [en]
Satellite Formation Flying, Model Predictive Control
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:ltu:diva-75790OAI: oai:DiVA.org:ltu-75790DiVA, id: diva2:1347541
External cooperation
Stanford University; University of Wuerzburg
Subject / course
Student thesis, at least 30 credits
Educational program
Space Engineering, master's level (120 credits)
Presentation
2019-05-20, B202, sanderring 2, wuerzburg, 10:00 (English)
Supervisors
Examiners
Available from: 2019-09-02 Created: 2019-08-31 Last updated: 2019-09-02Bibliographically approved

Open Access in DiVA

fulltext(3675 kB)9 downloads
File information
File name FULLTEXT01.pdfFile size 3675 kBChecksum SHA-512
1ff5132ded69d005f9ec122cd5020f2ddc1087e4ae05cafc52960938177a26644402376cca24b579e8f4dea90bca5c54434eef4f37fc4ea331b63c704fdf9d29
Type fulltextMimetype application/pdf

By organisation
Space Technology
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar
Total: 9 downloads
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

urn-nbn

Altmetric score

urn-nbn
Total: 27 hits
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • 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
  • rtf