Optimal rotation of the orbit plane of a variable mass spacecraft in the central gravitational field by means of orthogonal thrust

DOI10.1134/S000511791908006XzbMath1431.93032OpenAlexW2969019024MaRDI QIDQ2289036

Ya. G. Sapunkov, Yu. N. Chelnokov

Publication date: 28 January 2020

Published in: Automation and Remote Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s000511791908006x

zbMATH Keywords

optimal controlspacecraftquaternionslimited thrustorientation of orbit and orbital planesmall thrust

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Application models in control theory (93C95) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (2)

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

Cites Work

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• Optimal reorientation of a Spacecraft's orbit using a jet thrust orthogonal to the orbital plane
• Optimal Reorientation Of Spacecraft Orbit
• Ideal frames for perturbed Keplerian motions

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