Email this article 
Application of differential evolution algorithm in the problem of aeroassisted orbital plane change maneuver
- Authors: Elisov N.A.1, Ishkov S.A.1, Khramov A.A.1
-
Affiliations:
- Samara National Research University
- Issue: Vol 18, No 4 (2019)
- Pages: 41-51
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/7610
- DOI: https://doi.org/10.18287/2541-7533-2019-18-4-41-51
- ID: 7610
Cite item
Full Text
Abstract
The paper deals with application of the differential evolution method in optimizing aeroassisted orbital plane change maneuver performed by an aerospace vehicle with a high lift-to-drag ratio. The vehicle’s motion relative to the Earth is described by a system of differential equations in the flight path axis system. The angle-of-attack and the air path bank angle control programs are presented in the form of Fourier series and thrust control has the form of flip-flop control. The results of solving problems without phase parameter constraints obtained by the differential evolution algorithm were compared with the results obtained using Pontryagin’s maximum principle. The solution of the optimization problem taking into account temperature limitations at the stagnation point was obtained on the basis of the differential evolution algorithm.
About the authors
N. A. Elisov
Samara National Research University
Author for correspondence.
Email: mr07th@gmail.com
Postgraduate Student of the Department of Space Engineering
Russian FederationS. A. Ishkov
Samara National Research University
Email: ishkov@ssau.ru
Doctor of Science (Engineering),
Professor of the Department of Space Engineering
A. A. Khramov
Samara National Research University
Email: khramov@ssau.ru
Candidate of Science (Engineering),
Associate Professor of the Department of Space Engineering
References
- London H.S. Change of satellite orbit plane by aerodynamic maneuvering. Journal of Aerospace Science. 1962. V. 29, Iss. 3. P. 323-332. doi: 10.2514/8.9416
- Gurman V.I., Salmin V.V., Shershnev V.M. Analytical estimation of approximately-optimal combined turns. Kosmicheskie Issledovaniya. 1969. V. 7, no. 6. P. 819-826. (In Russ.)
- Shkadov L.M., Bukhanova R.S., Illarionov V.F., Plokhikh V.P. Mekhanika optimal’nogo prostranstvennogo dvizheniya letatel’nykh apparatov v atmosfere [Mechanics of optimal spatial motion of flying vehicles in the atmosphere]. Moscow: Mashinostroenie Publ., 1972. 240 p.
- Lazarev Yu.N. Upravleniye trayektoriyami aerokosmicheskikh apparatov [Space trajectory control]. Samara: Samarskiy Nauchnyy Tsentr RAN Publ., 2007. 274 p.
- Khramov A.A. Optimization of space vehicle combined orbital plane change maneuver on the basis of Pontryagin’s maximum principle. Vestnik of Samara University. Aerospace and Mechanical Engineering. 2019. V. 18, no. 1. P. 140-153. doi: 10.18287/2541-7533-2019-18-1-140-153 (In Russ.)
- Storn R., Price K. Differential evolution – a simple and efficient adaptive scheme for global optimization over continuous spaces. Technical report. Berkeley: International Computer Science Institute, 1995. 15 p.
- Thangeda P., Bhattacharya A.K., Gopal R., Kumar R.G.A. Synthesis of optimal trajectories in aerial engagements using differential evolution. IFAC-PapersOnLine. 2018. V. 51, Iss. 1. P. 90-97. doi: 10.1016/j.ifacol.2018.05.016
- Belokonov I.V., Kramlikh A.V., Lomaka I.A., Nikolaev P.N. Reconstruction of a spacecraft’s attitude motion using the data on the current collected from solar panels. Journal of Computer and Systems Sciences International. 2019. V. 58, Iss. 2. P. 286-296. doi: 10.1134/S1064230719020047
- Wu C., Xu R., Zhu S., Cui P. Time-optimal spacecraft attitude maneuver path planning under boundary and pointing constraints. Acta Astronautica. 2017. V. 137. P. 128-137. doi: 10.1016/j.actaastro.2017.04.004
- Wang M., Luo J., Fang J., Yuan J. Optimal trajectory planning of free-floating space manipulator using differential evolution algorithm. Advances in Space Research. 2018. V. 61, Iss. 6. P. 1525-1536. doi: 10.1016/j.asr.2018.01.011
- Yaroshevskiy V.A. Vkhod v atmosferu kosmicheskikh letatel'nykh apparatov [Spacecraft atmospheric re-entry]. Moscow: Nauka Publ., 1988. 336 p.
Supplementary files
