Synthesis of robust flight control system for lift/cruise fan aircraft

Hisashi Hiraoka, Yasuhiro Osa, Shigeru Uchikado, Kanya Tanaka

Research output: Contribution to conferencePaperpeer-review

Abstract

In this paper, we propose a new type of lift/cruise fan aircraft and attempt to apply a robust adaptive control method for its maneuver. First, the longitudinal equations of aircraft motion for a lift/cruise fan aircraft on hovering and small advancing are shown. Where the small variations of the front duct fan angle, the total thrust and the rear duct fan angle are given as the inputs, and forward velocity, vertical velocity and pitch angle are given as the outputs. Next, the construction of robust adaptive flight control system via polynomial algebraic method is shown. At the end of paper, the proposed control approach is applied to the lift/cruise fan aircraft and numerical simulations are shown to prove the feasibility.

Original languageEnglish
Pages170-175
Number of pages6
Publication statusPublished - 1 Dec 2002
EventProceedings of the 2002 IEEE International Symposium on Intelligent Control - Vancouver, Canada
Duration: 27 Oct 200230 Oct 2002

Conference

ConferenceProceedings of the 2002 IEEE International Symposium on Intelligent Control
Country/TerritoryCanada
CityVancouver
Period27/10/0230/10/02

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