... MEMORANDUM . Parameters of the Moon-perturbed orbit . Astro Space Center . ... of the Spacecraft only perturbations from external gravitating bodies (the Moon, the Sun) were taken into account, as well as ...
... MEMORANDUM . OPTIMIZATION OF THE MOON PERTURBED ORBIT . Astro Space Center . ... medium for near the 28 hours orbit altitudes , and high up to the Moon distances and higher) was fined a new class orbits [1 ...
... 30 degrees for Sun; . 20 degrees for Moon; . 25 degrees for Earth (nearest edge). ... An angle between direction to the Moon center and +X axis must exceed 5 degrees. ...
... around the Earth of about 9.5 days, which evolves as a result of weak gravitational perturbations from the Moon and the Sun ... km), by additional spacecraft maneuver using gravitational force of the Moon, and using 64-70 m antennas for the spacecraft ...
... around the Earth of about 9.5 days, which evolves as a result of weak gravitational perturbations from the Moon and the Sun ... km), by additional spacecraft maneuver using gravitational force of the Moon, and using 64-70 m antennas for the spacecraft ...
... with evolution due to gravitational pertur bations produced by the Moon and the Sun ... a high apogee orbit that strongly evolves under the action of the Moon and the Sun ...
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Ссылки http://www.asc.rssi.ru/RadioAstron/publications/articles/cr_2014,52,332.pdf -- 673.7 Кб -- 07.10.2014 Похожие документы
... the studied source, the Sun, and the Moon are trans formed to the coordinate system ... determine how the positions of the Sun and Moon on the celes tial sphere at the time ...
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Ссылки http://www.asc.rssi.ru/RadioAstron/publications/articles/cr_2014,52,373.pdf -- 295.3 Кб -- 07.10.2014 Похожие документы