Formation of high inclined orbits to the ecliptic by multiple gravity assist maneuvers

DOI10.1134/S1064230717020083zbMath1384.93103MaRDI QIDQ1745814

Yu. F. Golubev, V. V. Koryanov, A. V. Grushevskii, D. A. Tuchin, A. G. Tuchin

Publication date: 18 April 2018

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

zbMATH Keywords

chains of multiple GAMsenergy-efficient gravity assist maneuversinclination of orbitstrajectories of spacecraft

Mathematics Subject Classification ID

Application models in control theory (93C95) Variable mass, rockets (70P05)

Related Items (5)

Generalization of the Rutherford formula and synthesis of trajectories with gravity assist maneuvers ⋮ Formation of high inclined orbits to the ecliptic by multiple gravity assist maneuvers ⋮ Gravity assist maneuvers of a spacecraft in Jupiter system ⋮ Mission design of multipurpose flights to Venus ⋮ Using a three-impulse maneuvering scheme for returning from the lunar orbit to the reentry point of the Earth's atmosphere

Cites Work

• Low-cost flights in the Jovian system using tisserand coordinates
• Formation of high inclined orbits to the ecliptic by multiple gravity assist maneuvers
• Gravity assist maneuvers of a spacecraft in Jupiter system

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