Email this article A mathematical model of transforming the vertical takeoff and landing aircraft with a disk wing at maneuvering (on a deck)
- Authors: Pavlov V.V.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 59, No 4 (2016)
- Pages: 507-516
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/229873
- DOI: https://doi.org/10.3103/S1068799816040115
- ID: 229873
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Abstract
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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About the authors
V. V. Pavlov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: diskolet@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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