Parametric Identification of a Return Space Vehicle during Vertical Landing
- Авторы: Afanas’ev V.A.1, Degtyarev G.L.2, Meshchanov A.S.2
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Учреждения:
- South Ural State University (National Research University)
- Tupolev Kazan National Research Technical University
- Выпуск: Том 61, № 1 (2018)
- Страницы: 23-31
- Раздел: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230386
- DOI: https://doi.org/10.3103/S106879981801004X
- ID: 230386
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Аннотация
Real values of parameters for a space vehicle and its steering devices are specified by using the motion parameters measured in flight based on solving the differential equations of motion.
Об авторах
V. Afanas’ev
South Ural State University (National Research University)
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
A. Meshchanov
Tupolev Kazan National Research Technical University
Автор, ответственный за переписку.
Email: mas41@list.ru
Россия, ul. Karla Marksa 10, Kazan Tatarstan, 420111
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