Enviar artigo por via de e-mail Parametric Identification of a Return Space Vehicle during Vertical Landing
- Autores: Afanas’ev V.A.1, Degtyarev G.L.2, Meshchanov A.S.2
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Afiliações:
- South Ural State University (National Research University)
- Tupolev Kazan National Research Technical University
- Edição: Volume 61, Nº 1 (2018)
- Páginas: 23-31
- Seção: 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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Resumo
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.
Sobre autores
V. Afanas’ev
South Ural State University (National Research University)
Email: mas41@list.ru
Rússia, pr. Oktyabrya 16, Miass, 456318
G. Degtyarev
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
Rússia, ul. Karla Marksa 10, Kazan Tatarstan, 420111
A. Meshchanov
Tupolev Kazan National Research Technical University
Autor responsável pela correspondência
Email: mas41@list.ru
Rússia, ul. Karla Marksa 10, Kazan Tatarstan, 420111
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