Nonlinear modeling and control design of active helicopter blades

Matthias Althoff, Mayuresh J. Patil, Johannes P. Traugott

Publikation: Beitrag in Buch/Bericht/KonferenzbandKonferenzbeitragBegutachtung

4 Zitate (Scopus)

Abstract

The paper presents the theoretical basis for the simulation of active helicopter blades. The analysis of active helicopter blades is based on models for the structure, aerodynamics, actuation and sensing. For simulation and analysis purposes, the blade structural model is discretized in space using a Galerkin approach. The effect of the integral actuation enters the beam model via an active beam cross-sectional analysis. A 2-D incompressible, inviscid, quasi-steady aerodynamic model is coupled to the active structural model. The resulting nonlinear model of high order is reduced using the aeroelastic modes of the blade. Finally, a nonlinear controller is obtained by cancelling the nonlinearities and applying an energy optimal LQR, design to the resulting linear plant.

OriginalspracheEnglisch
TitelCollection of Technical Papers - 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Untertitel14th AIAA/ASME/AHS Adaptive Structures Conference, 8th AIAA Non-deterministic App
Herausgeber (Verlag)American Institute of Aeronautics and Astronautics Inc.
Seiten5389-5406
Seitenumfang18
ISBN (Print)1563478080, 9781563478086
DOIs
PublikationsstatusVeröffentlicht - 2006
Veranstaltung47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Newport, RI, USA/Vereinigte Staaten
Dauer: 1 Mai 20064 Mai 2006

Publikationsreihe

NameCollection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Band8
ISSN (Print)0273-4508

Konferenz

Konferenz47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Land/GebietUSA/Vereinigte Staaten
OrtNewport, RI
Zeitraum1/05/064/05/06

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