Мақаланы E-mail арқылы жіберу Parametric Identification of a Return Space Vehicle during Vertical Landing
- Авторлар: Afanas’ev V.A.1, Degtyarev G.L.2, Meshchanov A.S.2
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Мекемелер:
- South Ural State University (National Research University)
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 61, № 1 (2018)
- Беттер: 23-31
- Бөлім: 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
Дәйексөз келтіру
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Рұқсат берілді
Тек жазылушылар үшін
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.
Авторлар туралы
V. Afanas’ev
South Ural State University (National Research University)
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
A. Meshchanov
Tupolev Kazan National Research Technical University
Хат алмасуға жауапты Автор.
Email: mas41@list.ru
Ресей, ul. Karla Marksa 10, Kazan Tatarstan, 420111
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