A mathematical model of transforming the vertical takeoff and landing aircraft with a disk wing at maneuvering (on a deck)
- Авторлар: Pavlov V.V.1
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Мекемелер:
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 59, № 4 (2016)
- Беттер: 507-516
- Бөлім: 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
Дәйексөз келтіру
Аннотация
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.
Негізгі сөздер
Авторлар туралы
V. Pavlov
Tupolev Kazan National Research Technical University
Хат алмасуға жауапты Автор.
Email: diskolet@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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