scientific article; zbMATH DE number 6306327

zbMath1291.70045MaRDI QIDQ4979386

Ya. G. Sapunkov, Yu. N. Chelnokov, Il'Ya Alekseevich Pankratov

Publication date: 20 June 2014

Full work available at URL: http://mathnet.ru/eng/isu356

Title: zbMATH Open Web Interface contents unavailable due to conflicting licenses.

zbMATH Keywords

optimal controlorbitspacecraftquaternion

Mathematics Subject Classification ID

Celestial mechanics (70F15)

Related Items (3)

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 ⋮ Quaternion methods and regular models of celestial and space flight mechanic: using Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. II: Perturbed spatial restricted three-body problem ⋮ Optimal rotation of the orbit plane of a variable mass spacecraft in the central gravitational field by means of orthogonal thrust

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