Optimal reorientation of a Spacecraft's orbit using a jet thrust orthogonal to the orbital plane

DOI10.1016/J.JAPPMATHMECH.2013.02.002zbMath1327.70018OpenAlexW1991358197MaRDI QIDQ900318

Yu. N. Chelnokov

Publication date: 22 December 2015

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jappmathmech.2013.02.002

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (4)

Optimal reorientation of a Spacecraft's orbit using a jet thrust orthogonal to the orbital plane ⋮ 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

Cites Work

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• The causes of the shimmy phenomenon
• Optimal reorientation of a Spacecraft's orbit using a jet thrust orthogonal to the orbital plane
• Ideal frames for perturbed Keplerian motions

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