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Start Over Graduate Program Aerospace Engineering Year 2016 Committee Member Kenneth Steven Brentner Keyword dynamic inversion Keyword control systems

1. Rotorcraft Simulations with Coupled Flight Dynamics, Free Wake, and Acoustics

open_access
Open Access
Author:
Saetti, Umberto
Title:
Rotorcraft Simulations with Coupled Flight Dynamics, Free Wake, and Acoustics
Graduate Program:
Aerospace Engineering
Keywords:
rotorcraft
noise
control
control systems
dynamic inversion
feedback
flight dynamics
free wake
CHARM
PSUHeloSim
PSUWOPWOP
File:
Download UmbertoSaetti_Thesis_v9.pdf
Committee Members:
Joseph Francis Horn, Thesis Advisor/Co-Advisor
Kenneth Steven Brentner, Committee Member
George A Lesieutre, Committee Member

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