Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
In this paper the analysis of the fuel/time optimal control of the plane oscillations of the satellite on the elliptical orbit has been done. The numerical method of the sequential linearization of the boundary conditions for the optimal calculation of the switching moments has been proposed and its implementation has been presented. Examples for the different areas of the initial states and the different time-optimal values of hybridization coefficient γ have been calculated.
| Original language | English |
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| Title of host publication | International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2016 |
| Editors | Theodore E. Simos, Theodore E. Simos, Charalambos Tsitouras |
| Publisher | American Institute of Physics |
| ISBN (Electronic) | 9780735415386 |
| DOIs | |
| State | Published - 21 Jul 2017 |
| Event | International Conference of Numerical Analysis and Applied Mathematics 2016, ICNAAM 2016 - Rhodes, Greece Duration: 19 Sep 2016 → 25 Sep 2016 http://icnaam.org/ |
| Name | AIP Conference Proceedings |
|---|---|
| Volume | 1863 |
| ISSN (Print) | 0094-243X |
| ISSN (Electronic) | 1551-7616 |
| Conference | International Conference of Numerical Analysis and Applied Mathematics 2016, ICNAAM 2016 |
|---|---|
| Abbreviated title | ICNAAM 2016 |
| Country/Territory | Greece |
| City | Rhodes |
| Period | 19/09/16 → 25/09/16 |
| Internet address |
ID: 73212913