- Tytuł:
- Optimal reorientation of spacecraft orbit
- Autorzy:
-
Chelnokov, Yu. N.
Pankratov, I. A.
Sapunkov, Y. G. - Powiązania:
- https://bibliotekanauki.pl/articles/229458.pdf
- Data publikacji:
- 2014
- Wydawca:
- Polska Akademia Nauk. Czytelnia Czasopism PAN
- Tematy:
-
spacecraft
optimal control
quaternion - Opis:
- The problem of optimal reorientation of the spacecraft orbit is considered. For solving the problem we used quaternion equations of motion written in rotating coordinate system. The use of quaternion variables makes this consideration more efficient. The problem of optimal control is solved on the basis of the maximum principle. An example of numerical solution of the problem is given.
- Źródło:
-
Archives of Control Sciences; 2014, 24, 2; 119-128
1230-2384 - Pojawia się w:
- Archives of Control Sciences
- Dostawca treści:
- Biblioteka Nauki
Artykuł