Performance Analysis of a Conceptual Urban Air Mobility Configuration Using High-Fidelity Rotorcraft Flight Dynamic Model

Author:

An Jun-YoungORCID,Choi Yoo-Seung,Lee Il-Ryeong,Lim Mingyu,Kim Chang-JooORCID

Funder

Ministry of Education

Ministry of Science and ICT, South Korea

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Reference33 articles.

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2. Cerbe TM, Reichert G (1987) Simulation models for optimization of helicopter takeoff and landing. 13th European Rotorcraft Forum

3. Deresz RA (2013) Flight simulation and validation of height-velocity characteristics of an attack helicopter. Annual Forum Proc AHS Int 1:411–420

4. Goulos I, Giannakakis P, Pachidis V, Pilidis P (2013) Mission performance simulation of integrated helicopter-engine systems using an aeroelastic rotor model. J Eng Gas Turbines Power 135(9):1–12. https://doi.org/10.1115/1.4024869

5. Enconniere J, Ortiz-Carretero J, Pachidis V (2017) Mission performance analysis of a conceptual coaxial rotorcraft for air taxi applications. Aerosp Sci Technol 69:1–14. https://doi.org/10.1016/j.ast.2017.06.015

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