Nonlinear modeling and control design of active helicopter blades

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

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

4 Scopus citations

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.

Original languageEnglish
Title of host publicationCollection of Technical Papers - 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Subtitle of host publication14th AIAA/ASME/AHS Adaptive Structures Conference, 8th AIAA Non-deterministic App
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages5389-5406
Number of pages18
ISBN (Print)1563478080, 9781563478086
DOIs
StatePublished - 2006
Event47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Newport, RI, United States
Duration: 1 May 20064 May 2006

Publication series

NameCollection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Volume8
ISSN (Print)0273-4508

Conference

Conference47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Country/TerritoryUnited States
CityNewport, RI
Period1/05/064/05/06

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