Email this article Roll control of a flight vehicle with the adjustable center of mass
- Authors: Afanas’ev V.A.1, Degtyarev G.L.2, Kiselev V.I.1, Meshchanov A.S.2
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Affiliations:
- South Ural State University (National Research University)
- Tupolev Kazan National Research Technical University
- Issue: Vol 60, No 1 (2017)
- Pages: 50-56
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229989
- DOI: https://doi.org/10.3103/S1068799817010081
- ID: 229989
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Abstract
We present the results of analytical research of flight dynamics for a flight vehicle that is controlled by the adjustable center of mass in the vertical symmetry plane. The roll oscillations, which appear perpendicular to the symmetry plane due to technological errors, are eliminated by means of control rocket engines, for which a control law is assigned.
About the authors
V. A. Afanas’ev
South Ural State University (National Research University)
Author for correspondence.
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
V. I. Kiselev
South Ural State University (National Research University)
Email: mas41@list.ru
Russian Federation, pr. Oktyabrya 16, Miass, 456318
A. S. Meshchanov
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
