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Helicopter in virtual space
2008 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

This work explores two different approaches in the helicopter system (HUMUSOFT CE-150) identification. The obtained mathematical model of the helicopter is used for the control synthesis of PD, PID, LQG and MPC. The performances of controllers are mutually compared through the step responses with the standard amplitudes. The real time interconnection of the virtual reality helicopter model with the real helicopter system enhances the flight impression. The robustness of the control design is checked by the reaction of the system during the flight to the outside disturbances.

Place, publisher, year, edition, pages
2008.
Keyword [en]
Technology, Helicopter, Autopilot, Mathematical modeling, Control, PD, PID, LQG, Kalman filter, MPC, Virtual reality, Simulations, MATLAB, SIMULINK
Keyword [sv]
Teknik
Identifiers
URN: urn:nbn:se:ltu:diva-48802ISRN: LTU-PB-EX--08/087--SELocal ID: 639c73e4-8df8-433e-bede-588be72b1111OAI: oai:DiVA.org:ltu-48802DiVA: diva2:1022146
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

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