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Design of hybrid-electric aircraft with fault-tolerance considerations

  • Published:2023-02 Issue:2 Volume:36 Page:160-178
  • ISSN:1000-9361
  • Container-title:Chinese Journal of Aeronautics
  • language:en
  • Short-container-title:Chinese Journal of Aeronautics

Author:

MARCIELLO Valerio,OREFICE Francesco,NICOLOSI Fabrizio,CILIBERTI Danilo,DELLA VECCHIA Pierluigi

Funder

Horizon 2020

Horizon 2020 Framework Programme

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference41 articles.

1. International Civil Aviation Organization. Safety management manual. 2018. Document No.: 9859.

2. Future propulsion systems and energy sources in sustainable aviation;Farokhi,2019

3. Energy-optimal off-design power management for hybrid-electric aircraft;Riboldi;Aerosp Sci Technol,2019

4. An optimal approach to the preliminary design of small hybrid-electric aircraft;Riboldi;Aerosp Sci Technol,2018

5. Clarke S, Redifer M, Papathakis K, et al. X-57 power and command system design. In: 2017 IEEE transportation electrification conference and expo; 2017 Jun 22-24; Chicago, USA. Piscataway: IEEE Press; 2017.p.393–400

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4. Failure Behavior and Control-Based Mitigation for a Parallel Hybrid Propulsion System;AIAA SCITECH 2024 Forum;2024-01-04

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