2021
DOI: 10.1016/j.ast.2021.106903
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Trajectory optimization-based maneuverability assessment of eVTOL aircraft

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Cited by 21 publications
(4 citation statements)
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“…Particular focus will be on the extension of the model to capture the notable differences in manoeuvrability, guidance, path-planning and wake turbulence characteristics of Electric Vertical Take-Off and Landing (eVTOL) and various other emerging rotary-wing platforms compared to fixed-wing aircraft. This development will necessarily occur after the conclusion of various ongoing studies in the dynamics modelling and handling qualities of these new aircraft [52][53][54][55]. Future work will also address the application of the proposed collision risk model to tactical online ATM operations and online risk estimation performed onboard UAS platforms.…”
Section: Discussionmentioning
confidence: 99%
“…Particular focus will be on the extension of the model to capture the notable differences in manoeuvrability, guidance, path-planning and wake turbulence characteristics of Electric Vertical Take-Off and Landing (eVTOL) and various other emerging rotary-wing platforms compared to fixed-wing aircraft. This development will necessarily occur after the conclusion of various ongoing studies in the dynamics modelling and handling qualities of these new aircraft [52][53][54][55]. Future work will also address the application of the proposed collision risk model to tactical online ATM operations and online risk estimation performed onboard UAS platforms.…”
Section: Discussionmentioning
confidence: 99%
“…Most of the literature analyzes eVTOL feasibility from an engineering perspective, proving that eVTOL aircraft can operate under certain technical conditions [25][26][27][28][29][30][31]. However, economic feasibility relies on mathematical modeling [32][33][34][35][36][37][38].…”
Section: Engineering Application and Economic Feasibilitymentioning
confidence: 99%
“…Other similar studies also utilized simplified dynamic models [11,12]. Yet, only a handful of studies have undertaken trajectory optimization for VTOL aircraft based on 6DOF models [13][14][15]. Furthermore, only a few studies have considered airworthiness requirements for VTOL operations [15,16].…”
Section: Introductionmentioning
confidence: 99%