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

DOI10.3103/S0025654422600787MaRDI QIDQ2699160

Yu. N. Chelnokov

Publication date: 26 April 2023

Published in: Mechanics of Solids (Search for Journal in Brave)

zbMATH Keywords

spacecraftnonholonomicEuler (Rodrigues-Hamilton) parametersHamilton rotation quaternionorbital and ideal coordinate systemsperturbed spatial restricted three-body problemregular quaternion models

Mathematics Subject Classification ID

Mechanics of deformable solids (74-XX)

Related Items

Quaternion methods and regular models of celestial mechanics and space flight mechanics: local regularization of the singularities of the equations of the perturbed spatial restricted three-body problem generated by gravitational forces

Cites Work

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