Roll control of a flight vehicle with the adjustable center of mass
- 作者: Afanas’ev V.A.1, Degtyarev G.L.2, Kiselev V.I.1, Meshchanov A.S.2
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隶属关系:
- South Ural State University (National Research University)
- Tupolev Kazan National Research Technical University
- 期: 卷 60, 编号 1 (2017)
- 页面: 50-56
- 栏目: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229989
- DOI: https://doi.org/10.3103/S1068799817010081
- ID: 229989
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详细
We present the results of analytical research of flight dynamics for a flight vehicle that is controlled by the adjustable center of mass in the vertical symmetry plane. The roll oscillations, which appear perpendicular to the symmetry plane due to technological errors, are eliminated by means of control rocket engines, for which a control law is assigned.
作者简介
V. Afanas’ev
South Ural State University (National Research University)
编辑信件的主要联系方式.
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
V. Kiselev
South Ural State University (National Research University)
Email: mas41@list.ru
俄罗斯联邦, pr. Oktyabrya 16, Miass, 456318
A. Meshchanov
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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