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Mechanics / Differential equations / Control theory / Multivariable calculus / Partial differential equation / Normal mode / Constitutive equation / Damping / Physics / Ordinary differential equations / Mathematical analysis


Nonlinear Modeling and Control Design of Active Helicopter Blades Matthias Althoff∗, Mayuresh J. Patil† Virginia Polytechnic Institute and State University, Blacksburg, VA[removed]and Johannes P. Traugott‡
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Document Date: 2013-10-23 12:01:49


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City

Blacksburg / /

Company

IPl / /

Country

Germany / /

Facility

Institute of Automatic Control / Mayuresh J. Patil† Virginia Polytechnic Institute / American Institute of Aeronautics / Institute of Flight Mechanics / State University / /

IndustryTerm

free vibration solution / known solution / energy conservation / energy balance / cross product / kinetic energy / simulation tool / potential energy / nonlinear dynamic solution / approximate energy balance / tilde operator / steady-state solution / Steady state solution / energy / /

NaturalFeature

Ocean Engineering / /

Organization

State University / American Institute of Aeronautics and Astronautics / American Institute of Aeronautics / Institute of Automatic Control / Department of Aerospace and Ocean Engineering / Institute of Flight Mechanics and Flight Control / Polytechnic Institute / /

Person

V T ZV V V / Johannes P. Traugott‡ Technische Universit / V T XV V V / Aki Tkt Tir / T YV V V / /

/

Position

nonlinear controller / Assistant Professor / model for control design / /

ProvinceOrState

Virginia / /

Technology

3-D / aero / Newton-Raphson algorithm / simulation / /

SocialTag