Roll control of a flight vehicle with the adjustable center of mass
- Авторы: Afanas’ev V.A.1, Degtyarev G.L.2, Kiselev V.I.1, Meshchanov A.S.2
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Учреждения:
- South Ural State University (National Research University)
- Tupolev Kazan National Research Technical University
- Выпуск: Том 60, № 1 (2017)
- Страницы: 50-56
- Раздел: 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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Аннотация
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.
Об авторах
V. Afanas’ev
South Ural State University (National Research University)
Автор, ответственный за переписку.
Email: mas41@list.ru
Россия, pr. Oktyabrya 16, Miass, 456318
G. Degtyarev
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Kiselev
South Ural State University (National Research University)
Email: mas41@list.ru
Россия, pr. Oktyabrya 16, Miass, 456318
A. Meshchanov
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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