Coupled differential-algebraic equations framework for modeling six-degree-of-freedom flight dynamics of asymmetric fixed-wing aircraft
Crossref DOI link: https://doi.org/10.21833/ijaas.2025.01.004
Published Online: 2025-01
Published Print: 2025-01
Update policy: https://doi.org/10.21833/ijaas-crossmark
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Marzouk, Osama A. https://orcid.org/0000-0002-1435-5318
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