电邮这篇文章 Parametric Identification of a Return Space Vehicle during Vertical Landing
- 作者: Afanas’ev V.A.1, Degtyarev G.L.2, Meshchanov A.S.2
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隶属关系:
- South Ural State University (National Research University)
- Tupolev Kazan National Research Technical University
- 期: 卷 61, 编号 1 (2018)
- 页面: 23-31
- 栏目: 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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详细
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.
作者简介
V. Afanas’ev
South Ural State University (National Research University)
Email: mas41@list.ru
俄罗斯联邦, pr. Oktyabrya 16, Miass, 456318
G. Degtyarev
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan Tatarstan, 420111
A. Meshchanov
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: mas41@list.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan Tatarstan, 420111
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