A Fuzzy Controller for an Aeroload Simulator Using Phase Plane Method

The objective of this paper is to realize a fuzzy logic controller for an aeroload simulator, which simulates the aerodynamic load that a missile is subjected to on flight. In this paper, we propose a new fuzzy logic controller using the phase plane, in order to improve the overall performance of the aeroload simulator system. The design procedure and method of this controller are easy and simple such that performance evaluation of the aeroload simulator is carried out in a phase plane mapped from a decision rule table. The effectiveness of this control scheme is verified by comparison with a proportional integral derivative (PID) and a fixed fuzzy control through a series of simulation studies.
Publisher
IEEE-Inst Electrical Electronics Engineers Inc
Issue Date
2001-06
Language
ENG
Keywords

LOGIC CONTROLLER; CONTROL-SYSTEMS

Citation

IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, v.9, no.6, pp.791 - 801

ISSN
1063-6536
URI
http://hdl.handle.net/10203/898
Appears in Collection
ME-Journal Papers(저널논문)
Files in This Item
00960342.pdf(291.15 kB)Download
  • Hit : 917
  • Download : 779
  • Cited 0 times in thomson ci
This item is cited by other documents in WoS
⊙ Detail Information in WoSⓡClick to seewebofscience_button
⊙ Cited 6 items in WoSClick to see citing articles inrecords_button

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0