Investigation & simulation of an intelligent lateral flight controller for a blimp system

Sayedmehranmirsafaie Rizi*, Ali Khalili Mobarakeh, Mina Mirsafaie, Saba Nazari, Mohd Rizal Bin Arshad

*Corresponding author for this work

Research output: Chapter in Book or Report/Conference proceedingConference Proceedingpeer-review

Abstract

This research work elaborates the investigation of lateral flight control system as point of unmanned aerial vehicle control.To evaluate our work, we have used rigid flying object model that is 10 meters in lengthand studythe effects of number of forces were consideredsuch as inertia, fin force and wind to design the heading controller, Fuzzy logic controller more specifically Proportional Integral Derivative (PID) controller is used, wherepros and cons of fuzzy logic controller is considered. To justify our proposed work, simulation is been implemented to model controller designs and dynamics of the airship.Furthermore comparative study have been done between the outcome of the system to be design and the latest research literature. Experimentalresultsillustrate that our method is efficient, is more reliable and effective.

Original languageEnglish
Title of host publicationManufacturing Engineering and Technology for Manufacturing Growth
Pages420-426
Number of pages7
DOIs
Publication statusPublished - 2013
Externally publishedYes
Event2012 International Conference on Manufacturing Engineering and Technology for Manufacturing Growth, METMG 2012 - San Diego, CA, United States
Duration: 1 Nov 20122 Nov 2012

Publication series

NameAdvanced Materials Research
Volume628
ISSN (Print)1022-6680

Conference

Conference2012 International Conference on Manufacturing Engineering and Technology for Manufacturing Growth, METMG 2012
Country/TerritoryUnited States
CitySan Diego, CA
Period1/11/122/11/12

Keywords

  • Fuzzy logic
  • Lateral flight
  • PID controller
  • Simulink

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