Email this article Parametric Identification of a Return Space Vehicle during Vertical Landing
- Authors: Afanas’ev V.A.1, Degtyarev G.L.2, Meshchanov A.S.2
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Affiliations:
- South Ural State University (National Research University)
- Tupolev Kazan National Research Technical University
- Issue: Vol 61, No 1 (2018)
- Pages: 23-31
- Section: 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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Abstract
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.
About the authors
V. A. Afanas’ev
South Ural State University (National Research University)
Email: mas41@list.ru
Russian Federation, pr. Oktyabrya 16, Miass, 456318
G. L. Degtyarev
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
Russian Federation, ul. Karla Marksa 10, Kazan Tatarstan, 420111
A. S. Meshchanov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: mas41@list.ru
Russian Federation, ul. Karla Marksa 10, Kazan Tatarstan, 420111
