Journal article

Data-driven robust model predictive control of tiltwing vertical take-off and landing aircraft

Publication status:: Published

Peer review status:: Peer reviewed

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APA Style

Doff-Sotta, M., Cannon, M., & Bacic, M. (2024). Data-driven robust model predictive control of tiltwing vertical take-off and landing aircraft. Journal of Guidance, Control, and Dynamics.

MLA Style

Doff-Sotta, M., et al. “Data-Driven Robust Model Predictive Control of Tiltwing Vertical Take-off and Landing Aircraft.” Journal of Guidance, Control, and Dynamics, American Institute of Aeronautics and Astronautics, 2024.

Chicago Style

Doff-Sotta, M, M Cannon, and M Bacic. 2024. “Data-Driven Robust Model Predictive Control of Tiltwing Vertical Take-off and Landing Aircraft.” Journal of Guidance, Control, and Dynamics.
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Publisher copy:: 10.2514/1.G008315

Authors

+ Doff-Sotta, M More by this author

Institution:: University of Oxford
Division:: MPLS
Department:: Engineering Science
Role:: Author

+ Cannon, M More by this author

Institution:: University of Oxford
Division:: MPLS
Department:: Engineering Science
Oxford college:: St John's College
Role:: Author
ORCID:: 0000-0003-2189-7876

+ Bacic, M More by this author

Institution:: University of Oxford
Division:: MPLS
Department:: Engineering Science
Role:: Author

+ Engineering and Physical Sciences Research Council More from this funder

Funder identifier:: https://ror.org/0439y7842
Grant:: 2290940

Publisher:: American Institute of Aeronautics and Astronautics
Journal:: Journal of Guidance, Control, and Dynamics More from this journal
Publication date:: 2024-10-31
Acceptance date:: 2024-08-16
DOI:: 10.2514/1.G008315
EISSN:: 1533-3884
ISSN:: 0731-5090

Language:: English
Pubs id:: 2024467
Local pid:: pubs:2024467
Deposit date:: 2024-08-31

Terms of use

Copyright holder:: Rolls-Royce, plc.
Copyright date:: 2024
Rights statement:: © 2024 by Rolls-Royce, plc. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.
Notes:: This is the accepted manuscript version of the article. The final version is available online from American Institute of Aeronautics and Astronautics at: https://dx.doi.org/10.2514/1.G008315

Licence:: Terms and Conditions of Use for Oxford University Research Archive

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