Email this article Control of flight vehicles 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
- Tupolev Kazan National Research Technical University
- Issue: Vol 59, No 3 (2016)
- Pages: 324-330
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229747
- DOI: https://doi.org/10.3103/S1068799816030053
- ID: 229747
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Abstract
We resolve a problem how to control the longitudinal angular motion of flight vehicles (FV) having a system to displace the center of mass in the transverse direction. A structure is determined and a control law is established to start up and shutdown the engines. Formulas to determine the control parameters are obtained.
About the authors
V. A. Afanas’ev
South Ural State University
Email: mas41@list.ru
Russian Federation, pr. Oktyabrya 16, Miass, Chelyabinskaya oblast, 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
Email: mas41@list.ru
Russian Federation, pr. Oktyabrya 16, Miass, Chelyabinskaya oblast, 456318
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
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