Open Access
Omkar Chendwankar,
Shraddha Pawar,
Siddesh Pardesi,
Nayan kamble,
Amol Bhagat,
- Student, Department of Mechanical Engineering, Saraswati College of Engineering, Kharghar, Mumbai, India
- Student, Department of Mechanical Engineering, Saraswati College of Engineering, Kharghar, Mumbai, India
- Student, Department of Mechanical Engineering, Saraswati College of Engineering, Kharghar, Mumbai, India
- Student, Department of Mechanical Engineering, Saraswati College of Engineering, Kharghar, Mumbai, India
- Assitant Professor, Department of Mechanical Engineering, Saraswati College of Engineering, Kharghar, Mumbai, India
Abstract
eVTOL (electric vertical take-off and landing) for urban mobility is currently evolving and many concepts of configurations with which vertical take-off and landing could be made possible are discussed like a multi-copter, lift and cruise, and tilt-wing. All these concepts have different behavior from the flight dynamics perspective. The one which is predominantly discussed here is the proposed model Cityhawk by Urban Aeronautics with a ducted fan vane control system. Urban Aeronautics has very high levels of aerospace experience on its team (including experts from Boeing and military development) and has completed flights of Cormorant drones which prove the concept for the passenger CityHawk. This project aims to conceptually design and building a nonlinear 6 DOF dynamic model of an eVTOL with a proposed configuration on a MATLAB Simulink.
Keywords: eVTOL, Urban Air Mobility, Simulink, MATLAB, Urban Aeronautics
Omkar Chendwankar, Shraddha Pawar, Siddesh Pardesi, Nayan kamble, Amol Bhagat. Conceptual design of eVTOL A Nonlinear Dynamic Model of an eVTOL on Simulink-MATLAB. International Journal of Structural Mechanics and finite elements. 2023; ():-.
Omkar Chendwankar, Shraddha Pawar, Siddesh Pardesi, Nayan kamble, Amol Bhagat. Conceptual design of eVTOL A Nonlinear Dynamic Model of an eVTOL on Simulink-MATLAB. International Journal of Structural Mechanics and finite elements. 2023; ():-. Available from: https://journals.stmjournals.com/ijsmfe/article=2023/view=91619
References
1. Borer, N.K.; Patterson, M.D.; Viken, J.K.; Moore, M.; Bevirt, J.; Stoll, A.M.; Gibson, A.R. Design and Performance of the NASA SCEPTOR Distributed Electric Propulsion Flight Demonstrator. In Proceedings of the 16th AIAA Aviation Technology, Integration, and Operations Conference (AIAA AVIATION Forum), Washington, DC, USA, 13–17 June 2016.
2. Xinhua Wang and Lilong Cai “Mathematical modeling and control of a tilt-rotor aircraft”. Aerospace Science and Technology, 2015. 47(12), Pp473-492.
3. Max skuhersky “A First principle power and energy model for evtol Vehicles”. Conference: AIAA Scitech 2020 Forum. January 2020.
4. Shannon Ackert “Aircraft payload-range analysis for financiers”
5. Rafi Yoeli “Ducted fan vehicles particularly useful as vtol aircraft” US patent US7918416B2
6. Rafi Yoeli “Flight control system especially suited for vtol vehicles”” US patent US 7946528 B2
7. Hao Cheng and Hua Wang“Prediction of lift coefficient for tandem wing configuration or multiple- lifting-surface system using prandtl’s lifting-line theory”. International Journal of Aerospace Engineering.
8. Bernard etkins “Dynamics of atmospheric flight.”
9. Michael V Cook “Flight Dynamics Principles””. A Linear Systems Approach to Aircraft Stability and Control Book • Third Edition • 2013.
10. Venkateshan C “Fundamentals of helicopter dynamics.” 1st Edition.
Volume | |
Received | 28/10/2021 |
Accepted | 14/12/2021 |
Published | 14/01/2023 |