Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits

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

Russian Federation

Assistant of the Department of Flight Dynamics and Control
Systems

S. A. Ishkov

Samara State Aerospace University

Email: ishkov@ssau.ru

Russian Federation

Doctor of Technical Science

Professor

Head of the Institute of Supplementary Professional Education

References

  1. 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.
  2. 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.
  3. Okhotsimsky, D. Ye. Basics of space flight mechanics [Text] / D. Ye. Okhotsimsky, Yu. G. Sikharulidze. - M.: Nauka. - p.

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