6 Art�culos

On an approach to determining the orientation of the spacecraft orbit

Acceso

en l�nea

Ilia Pankratov P�g. 47 - 51

The paper is dedicated to a mathematical simulation of the motion of a spacecraft in an elliptical orbit. The acceleration vector is limited in modulo and orthogonal to the plane of spacecraft orbit during its motion. The spacecraft motion is described u... ver m�s

Revista: International Journal of Open Information Technologies Formato: Electr�nico

Tabla de contenido: Vol: 9 Num: 10 Par: 0 A�o: 2021

Quasi-optimal quaternion genetic algorithm for reorientation of the spacecraft orbit

Acceso

en l�nea

Ilia Pankratov P�g. 9 - 13

The problem of optimal reorientation of the spacecraft orbit is considered in quaternion formulation. Control (acceleration from jet thrust vector orthogonal to the plane of the orbit) is limited in magnitude. It is necessary to minimize the energy costs... ver m�s

Revista: International Journal of Open Information Technologies Formato: Electr�nico

Tabla de contenido: Vol: 7 Num: 8 Par: 0 A�o: 2019

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