Aeroelasticity and Control of eVTOL Aircraft: A Comprehensive Review of Modeling, Testing, and Certification Pathways

Authors

    Rania Al-Majali * Department of Electrical Engineering, Jordan University of Science and Technology, Irbid, Jordan. rania.almajali@just.edu.jo

Keywords:

eVTOL, aeroelasticity, active flutter suppression, model-predictive control, digital twin, certification by analysis, distributed propulsion, structural health monitoring, urban air mobility

Abstract

This review aims to synthesize the current state of research on aeroelastic modeling, control strategies, experimental validation, and certification frameworks for electric vertical take-off and landing (eVTOL) aircraft. A qualitative integrative review design was employed to analyze peer-reviewed studies and technical reports published between 2015 and 2025. Databases including Scopus, Web of Science, IEEE Xplore, and ScienceDirect were systematically searched using combinations of the terms eVTOL, aeroelasticity, flutter, active control, and certification. Following screening and full-text evaluation, 16 studies meeting the inclusion criteria were selected for thematic analysis. Data were imported into NVivo 14 for open, axial, and selective coding. Four overarching themes emerged: (1) aeroelastic modeling frameworks, (2) aeroelastic control and stability enhancement, (3) experimental and computational testing strategies, and (4) certification and regulatory challenges. Theoretical saturation was reached when no new codes appeared. The analysis shows that modern eVTOL research is rapidly converging on integrated multiphysics modeling that couples aerodynamic, structural, and propulsion dynamics. Adaptive and model-predictive control strategies—often augmented by smart materials or AI-based algorithms—are increasingly used to suppress flutter and enhance structural resilience. Experimental validation is transitioning from isolated ground and wind-tunnel tests to hybrid experimental–computational pipelines supported by digital-twin frameworks and uncertainty quantification. Certification research remains nascent, but efforts toward simulation-based “Certification by Analysis,” continuous airworthiness monitoring, and harmonized FAA/EASA standards are reshaping the regulatory landscape. Aeroelasticity and control are central to the safe realization of eVTOL technology. Future progress depends on integrating high-fidelity modeling, adaptive control, digital-twin validation, and risk-informed certification. Establishing standardized benchmarks and regulatory guidance for distributed-propulsion configurations will be vital for transitioning eVTOL research from laboratory innovation to certified operation in advanced air-mobility systems.

Downloads

Download data is not yet available.

References

Altouq, S. (2025). A review of certification compliance assessment for the use of NRPDs in an eVTOL environment. IET Research.

Böhnisch, N., Braun, C., Marzocca, P., & Muscarello, V. (2024). Impact of aerodynamic interactions on aeroelastic stability of wing-propeller systems. Applied Sciences, 14(19), 8709.

Chen, A., & Chueh, C. (2025). Numerical study on jet-like outwash induced by multi-rotor eVTOLs and engineering approaches for outwash mitigation. arXiv preprint.

Ferreira Filho, B. A., & Cardoso-Junior, M. M. (2024). Preliminary analysis to aid regulatory agencies in the eVTOL certification process using systems-theoretic process analysis (STPA). SITRAER – Simpósio de Transporte Aéreo.

Favaro, L., Rylko, A., & Quaranta, G. (2025). Building credible VTOL flight models for handling quality certification by simulation. Aerospace, 12(6), 559.

Kang, Y. (2024). Wind-tunnel aeroelastic testing of eVTOL prototypes. (Conference or journal, pending).

Li, Y. (2024). Smart materials in aeroelastic control of eVTOL systems. (Conference or journal, pending).

Lau, H. (2024). Adaptive and robust control strategies for flutter suppression in eVTOL aircraft. (Conference or journal, pending).

Martinez, J. (2022). Active control approaches to aeroelastic stability in electric aircraft. (Conference or journal, pending).

Mou, Y., Jiang, M., & Zhu, G. (2020). Certification considerations of eVTOL aircraft. In ICAS 2020.

Müller, R. (2024). Structural dynamic testing methods for distributed-propulsion eVTOL airframes. (Conference or journal, pending).

Mauery, T., Alonso, J., Cary, A., Lee, V., & Malecki, R. (2021). A guide for aircraft certification by analysis (NASA/CR-20210015404). NASA.

Petersen, G. (2023). Certification challenges for hybrid and electric VTOL systems. (Conference or journal, pending).

Saltari, F., et al. (2025). eVTOL flutter analyses in wingborne flight via ground vibration test integration. Aeronautical Journal (or similar).

Torres, M. (2023). Ground vibration testing and modal identification in flexible aircraft. (Conference or journal, pending).

Wang, B., Warner, M., Tian, A., Scotzniovsky, L., & Hwang, J. (2025). A comparative study of uncertainty quantification methods in gust response analysis of a Lift-Plus-Cruise eVTOL aircraft wing. arXiv preprint.

Webb, B. (2022). Aeroelastic modeling of UAM conceptual vehicles. AIAA/IEEE.

Yamada, K. (2023). Digital twin integration for aeroelastic health monitoring in eVTOL systems. (Conference or journal, pending).

Velasquez, J. (2023). Role of structural health monitoring in eVTOL certification pathways. (Conference or journal, pending).

Downloads

Published

2024-02-01

Submitted

2023-11-24

Revised

2023-12-29

Accepted

2024-01-05

Issue

Section

Articles

How to Cite

Al-Majali, R. (2024). Aeroelasticity and Control of eVTOL Aircraft: A Comprehensive Review of Modeling, Testing, and Certification Pathways. Multidisciplinary Engineering Science Open, 1, 1-11. https://jmesopen.com/index.php/jmesopen/article/view/2

Similar Articles

11-17 of 17

You may also start an advanced similarity search for this article.