eVTOL Aircraft

Control Allocation, Hybrid-Automata, Path Planning, Contingency Planning, Flight Dynamics Modeling

Introduction

With the introduction of novel eVTOL aircraft and drones into air space, the complexity in aircraft design and air space management will drastically increase. Safety and efficiency concerns must be solved before successful commercial flight operations can begin. In my research related to eVTOL aircraft, the objective is to respond to these concerns by formulating and solving optimization problems that can help enabling these technologies.

Specifically, I focused on the following subjects for tandem tiltwing eVTOL aircraft with distirubted propulsion in my PhD thesis (Yilmaz, 2023):

  • Surrogate Modeling for Aeropropulsive Forces and Moments
  • Control Allocation Optimization for Over-Actuated eVTOL Aircraft (Yilmaz & German, 2024)
  • Hybrid Automaton-Based Planning
  • Distributed Electric Propulsion Concepts
  • Transition Corridors and Tilting Schedule Considerations
  • Multi-Disciplinary Design and Optimization Frameworks
VSPAERO Trailing Vortex Solution at Forward Flight Condition
VSPAERO Trailing Vortex Solutions

References

2024

  1. J3.AST
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    Control allocation optimization for an over-actuated tandem tiltwing eVTOL aircraft considering aerodynamic interactions
    Aerospace Science and Technology, 2024

2023

  1. PhD Dissertation
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    Hybrid Automaton Based Nominal and Contingency Planning for an Over-Actuated Tandem Tiltwing eVTOL Aircraft
    Georgia Institute of Technology, 2023