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Author:

Iyer, Venkatakrishnan

Title:

Nonlinear Yaw Control of a Compound Helicopter

Graduate Program:

Electrical Engineering

Keywords:

Dynamic Inversion
Helicopter Modeling
Automatic Flight Control System
Adaptive Control
Vectored Thrust Ducted propeller
Compound Helicopter
Pseudo Control Hedging
Feedback Linearization Using Neural Networks
Neural Networks
Feedback Linearization

File:

Download Nonlinear_Yaw_Control_of_a_Compound_Helicopter.pdf

Committee Members:

Minghui Zhu, Thesis Advisor/Co-Advisor
Constantino Manuel Lagoa, Committee Member
Eric Norman Johnson, Thesis Advisor/Co-Advisor
Kultegin Aydin, Program Head/Chair