Enviar artigo por via de e-mail A mathematical model of transforming the vertical takeoff and landing aircraft with a disk wing at maneuvering (on a deck)
- Autores: Pavlov V.V.1
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Afiliações:
- Tupolev Kazan National Research Technical University
- Edição: Volume 59, Nº 4 (2016)
- Páginas: 507-516
- Seção: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229873
- DOI: https://doi.org/10.3103/S1068799816040115
- ID: 229873
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Resumo
The motion of blades relative to the disk wing at the extension and retraction modes is defined. The general solution is obtained including the fuselage motion under the action of control or external disturbance.
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Sobre autores
V. Pavlov
Tupolev Kazan National Research Technical University
Autor responsável pela correspondência
Email: diskolet@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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