电邮这篇文章 A mathematical model of transforming the vertical takeoff and landing aircraft with a disk wing at maneuvering (on a deck)
- 作者: Pavlov V.V.1
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隶属关系:
- Tupolev Kazan National Research Technical University
- 期: 卷 59, 编号 4 (2016)
- 页面: 507-516
- 栏目: 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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详细
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.
作者简介
V. Pavlov
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: diskolet@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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