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Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits
- Authors: Fadeenkov P.V.1, Ishkov S.A.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 10, No 1 (2011)
- Pages: 31-37
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/974
- DOI: https://doi.org/10.18287/2541-7533-2011-0-1(25)-31-37
- ID: 974
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Abstract
The paper deals with the problem of creating an optimal program of controlling low-thrust spacecraft in the flight between noncoplanar elliptical and geostationary orbits. A scheme for the joint change of orbital elements within the simple structure of the thrust vector control on the orbit turn is suggested.
About the authors
P. V. Fadeenkov
Samara State Aerospace University
Author for correspondence.
Email: dinpol@ssau.ru
Assistant of the Department of Flight Dynamics and Control
Systems
S. A. Ishkov
Samara State Aerospace University
Email: ishkov@ssau.ru
Doctor of Technical Science
Professor
Head of the Institute of Supplementary Professional Education
Russian FederationReferences
- Lebedev, V. N. Calculation of motion of a low-thrustspace vehicle [Text] / V.N. Lebedev. - M.: Computer center of the Academy of Sciences, USSR, - p.
- Petukhov, V. G. Optimization of multiorbit transfers between noncoplanar elliptic orbits [Text] / V. G. Petukhov // Kosmicheskie issledovaniya. - - Vol.42, 3, - PP. 260-Salmin, V. V. Methods of solving variational problems of mechanics of low-thrust space flight [Text] / V. V. Salmin, S. A. Ishkov, O. L. Starinova. - Samara: Publishing house of the Samara center of science, RAS. - 164 p.
- Okhotsimsky, D. Ye. Basics of space flight mechanics [Text] / D. Ye. Okhotsimsky, Yu. G. Sikharulidze. - M.: Nauka. - p.
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