Отправить статью по E-mail Control of flight vehicles with the adjustable center of mass
- Авторы: Afanas’ev V.1, Degtyarev G.2, Kiselev V.1, Meshchanov A.2
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Учреждения:
- South Ural State University
- Tupolev Kazan National Research Technical University
- Выпуск: Том 59, № 3 (2016)
- Страницы: 324-330
- Раздел: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229747
- DOI: https://doi.org/10.3103/S1068799816030053
- ID: 229747
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Аннотация
We resolve a problem how to control the longitudinal angular motion of flight vehicles (FV) having a system to displace the center of mass in the transverse direction. A structure is determined and a control law is established to start up and shutdown the engines. Formulas to determine the control parameters are obtained.
Об авторах
V. Afanas’ev
South Ural State University
Email: mas41@list.ru
Россия, pr. Oktyabrya 16, Miass, Chelyabinskaya oblast, 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
Email: mas41@list.ru
Россия, pr. Oktyabrya 16, Miass, Chelyabinskaya oblast, 456318
A. Meshchanov
Tupolev Kazan National Research Technical University
Автор, ответственный за переписку.
Email: mas41@list.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
