Analysis of optimal motion control for a material point in a central field with application of quaternions

DOI10.1134/S1064230707050036zbMath1308.49016OpenAlexW2028059939MaRDI QIDQ2017485

Yu. N. Chelnokov

Publication date: 23 March 2015

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

Full work available at URL: https://doi.org/10.1134/s1064230707050036

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Optimality conditions for problems involving ordinary differential equations (49K15)

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Cites Work

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• Ideal frames for perturbed Keplerian motions
• Perturbation theory of Kepler motion based on spinor regularization.
• Constants of the motion for optimum thrust trajectories in a central force field