Analytical Design of the Law for Control of the Center of Mass Motion for an Unmanned Aerial Vehicle
- 作者: Afanas’ev V.1, Degtyarev G.2, Meshchanov A.2
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隶属关系:
- South Ural State University (National Research University)
- Tupolev Kazan National Research Technical University
- 期: 卷 62, 编号 2 (2019)
- 页面: 206-212
- 栏目: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230918
- DOI: https://doi.org/10.3103/S1068799819020053
- ID: 230918
如何引用文章
详细
The control of the lift direction in space is considered. We synthesized the control of the mechanism of the center of mass motion in the longitudinal direction for regulating the static margin and in the transverse direction for creating the balancing equilibrium at the angle of attack and air-path bank angle. The structure of the law to control the angular acceleration is chosen, formulas to calculate the control parameters are obtained.
作者简介
V. Afanas’ev
South Ural State University (National Research University)
Email: mas41@list.ru
俄罗斯联邦, pr. Oktyabrya 16, Miass, 456318
G. Degtyarev
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
A. Meshchanov
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: mas41@list.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111