| Autor: |
Alesova, I. M., Babadzanjanz, L. K., Bregman, A. M., Bregman, K. M., Pototskaya, I. Yu., Pupysheva, Yu. Yu., Saakyan, A. T. |
| Předmět: |
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| Zdroj: |
AIP Conference Proceedings; 2018, Vol. 1978 Issue 1, p1-4, 4p |
| Abstrakt: |
In this paper the analysis of the fuel optimal control of the plane oscillations of the satellite on the circular orbit subject to the aerodynamic moment variations has been done. On basis of necessary conditions of optimality the problem was reduced to the task of nonlinear programming. The numerical method of the sequential linearization of the boundary conditions for calculation of the switching moments has been proposed and its implementation has been presented. Examples for the different areas of the initial states have been calculated. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
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