Optimal reorientation of spacecraft orbit

• Autorzy: Chelnokov Yu. N. , Pankratov I. A. , Sapunkov Y. G.

Identyfikatory

DOI

10.2478/acsc-2014-0008

• Języki publikacji: EN

Abstrakty

EN

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.

Słowa kluczowe

EN

spacecraft; optimal control; quaternion

• Wydawca: Polish Academy of Sciences, Committee of Automatic Control and Robotics
• Czasopismo: Archives of Control Sciences
• Rocznik: 2014
• Tom: Vol. 24, no. 2
• Strony: 119--128
• Opis fizyczny: Bibliogr. 17 poz., rys., wzory

Twórcy

autor

Chelnokov Yu. N.

• Saratov State University and Institute of Precision Mechanics and Control Russian Academy of Sciences, Saratov, Russia

autor

Pankratov I. A.

• Saratov State University, Saratov, Russia

autor

Sapunkov Y. G.

• Saratov State University and Institute of Precision Mechanics and Control Russian Academy of Sciences, Saratov, Russia

Bibliografia

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