The problem of rendezvous of a controlled space vehicle with an uncontrolled space vehicle moving along an elliptical keplerian orbit in the central Newtonian gravitational field

DOI10.1134/S106423070703015XzbMath1301.70014OpenAlexW1997280023MaRDI QIDQ465323

Yu. V. Afanas'eva, Yu. N. Chelnokov

Publication date: 31 October 2014

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

Full work available at URL: https://doi.org/10.1134/s106423070703015x

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (1)

Quaternion methods and regular models of celestial mechanics and space flight mechanics: the use of Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. I: Review and analysis of methods and models and their applications

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