Roll control of a flight vehicle with the adjustable center of mass
- Авторлар: Afanas’ev V.A.1, Degtyarev G.L.2, Kiselev V.I.1, Meshchanov A.S.2
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Мекемелер:
- South Ural State University (National Research University)
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 60, № 1 (2017)
- Беттер: 50-56
- Бөлім: 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
Дәйексөз келтіру
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.
Авторлар туралы
V. Afanas’ev
South Ural State University (National Research University)
Хат алмасуға жауапты Автор.
Email: mas41@list.ru
Ресей, pr. Oktyabrya 16, Miass, 456318
G. Degtyarev
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Kiselev
South Ural State University (National Research University)
Email: mas41@list.ru
Ресей, pr. Oktyabrya 16, Miass, 456318
A. Meshchanov
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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