| Autor: |
Pedrosa Reis, Francisco, Lustosa, Leandro R., Poussot-Vassal, Charles |
| Přispěvatelé: |
Institut Supérieur de l'Aéronautique et de l'Espace - ISAE-SUPAERO (FRANCE), Office National d'Etudes et Recherches Aérospatiales - ONERA (FRANCE) |
| Jazyk: |
angličtina |
| Rok vydání: |
2022 |
| Předmět: |
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| Popis: |
This paper proposes a new parametrization of very flexible aircraft structural elements to support geometric control studies. First, a sum of basis functions is used to calculate the torsion and curvature distributions of a beam-like structural element. Secondly, the modal functions are used to determine the attitude on SO(3) and the position of each point on the element, assuming constant curvatures. Finally, a simulator implementation of the method is described, along with numerical simplifying strategies. |
| Databáze: |
OpenAIRE |
| Externí odkaz: |
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