Change search
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • 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
Fuzzy Modelling of Zero-pressure Balloon Ascent
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.ORCID iD: 0000-0003-4977-6339
2018 (English)In: 2018 Modeling and Simulation Technologies Conference, 2018Conference paper, Published paper (Refereed)
Abstract [en]

Zero-pressure balloon ascent prediction is a critical issue for Swedish Space Corporation(SSC) as targeted test ights are important part of SSC activities. This paper introducesa data-driven approach for estimating the balloon ascent. An output-constrained fuzzylogic approach is applied to the zero-pressure balloon data set from the past 10 years fromEsrange Space Center and rules are formulated that can express the balloon ascent. Theserules are veried by performing a root mean square analysis of estimated ascent againstthe real ascent trajectory. The result shows that the proposed fuzzy model is reliable andis able to estimate the balloon ascent with an acceptable accuracy.

Place, publisher, year, edition, pages
2018.
National Category
Other Electrical Engineering, Electronic Engineering, Information Engineering
Research subject
Onboard space systems
Identifiers
URN: urn:nbn:se:ltu:diva-73399DOI: 10.2514/6.2018-3753Scopus ID: 2-s2.0-85051630074OAI: oai:DiVA.org:ltu-73399DiVA, id: diva2:1301862
Conference
2018 Modeling and Simulation Technologies Conference, June 25-29 2018, Atlanta, Georgia.
Available from: 2019-04-03 Created: 2019-04-03 Last updated: 2022-03-14Bibliographically approved
In thesis
1. Autonomous Navigation System for High Altitude Balloons
Open this publication in new window or tab >>Autonomous Navigation System for High Altitude Balloons
2019 (English)Doctoral thesis, comprehensive summary (Other academic)
Place, publisher, year, edition, pages
Luleå tekniska universitet, 2019. p. 150
Series
Doctoral thesis / Luleå University of Technology 1 jan 1997 → …, ISSN 1402-1544
National Category
Aerospace Engineering
Research subject
Onboard space systems
Identifiers
urn:nbn:se:ltu:diva-76476 (URN)978-91-7790-486-1 (ISBN)978-91-7790-487-8 (ISBN)
Public defence
2020-01-24, IRF Aula, Kiruna, 09:00 (English)
Opponent
Supervisors
Available from: 2019-10-23 Created: 2019-10-22 Last updated: 2023-01-23Bibliographically approved

Open Access in DiVA

No full text in DiVA

Other links

Publisher's full textScopus

Authority records

Garg, KanikaEmami, Reza

Search in DiVA

By author/editor
Garg, KanikaEmami, Reza
By organisation
Space Technology
Other Electrical Engineering, Electronic Engineering, Information Engineering

Search outside of DiVA

GoogleGoogle Scholar

doi
urn-nbn

Altmetric score

doi
urn-nbn
Total: 136 hits
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • 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