Optimization of the Spacecraft Transfer Maneuver from a Point of the Elliptical Orbit to Another Point of the Same Orbit-Reference-Cited by-同舟云学术

Optimization of the Spacecraft Transfer Maneuver from a Point of the Elliptical Orbit to Another Point of the Same Orbit

Published:2023-09-16 Issue:5 Volume:61 Page:431-448
ISSN:0010-9525
Container-title:Cosmic Research
language:en
Short-container-title:Cosmic Res

Author:

Konstantinov M. S.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Link

https://link.springer.com/content/pdf/10.1134/S001095252370034X.pdf

Reference11 articles.

1. Konstantinov, M.S., Obukhov, V.A., Petukhov, V.G., et al., Spacecraft station keeping in the Molniya orbit using electric propulsion, Proc. 56th Int. Astronautical Congress, Fukuoka, Japan, October 17–21, 2005, p. IAC-05-C1.1.01. https://doi.org/10.2514/6.IAC-05-C1.1.01

2. Petukhov, V., Ivanyukhin, A., Popov, G., et al., Optimization of finite-thrust trajectories with fixed angular distance, Acta Astronaut., 2022, vol. 197, pp. 354–367. https://doi.org/10.1016/j.actaastro.2021.03.012

3. Petukhov, V., Application of the angular independent variable and its regularizing transformation in the problems of optimizing low-thrust trajectories, Cosmic Res., 2019, vol. 57, no. 5, pp. 351–363. https://doi.org/10.1134/S001095251905006X

4. Ivanyukhin, A. and Petukhov, V., Optimization of multi-revolution limited power trajectories using angular independent variable, J. Optim. Theory Appl., 2021, vol. 191, no. 2, pp. 575–599. https://doi.org/10.1007/s10957-021-01853-8

5. Konstantinov, M.S., Petukhov, V.G., and Thein, M., Optimizatsiya traektorii geliotsentricheskikh pereletov (Optimization of Trajectories of Heliocentric Transfers), Moscow: Izd. Mosk. Aviats. Inst., 2015.