Tangent Velocity constraint for orbital maneuvers with Theory of Functional Connections

Maneuvering a spacecraft in the cislunar space is a complex problem, since it is highly perturbed by the gravitational influence of both the Earth and the Moon, and possibly also the Sun. Trajectories minimizing the needed fuel are generally preferred in order to decrease the mass of the payload. A...

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Veröffentlicht in:	arXiv.org 2024-01
Hauptverfasser:	A K de Almeida Jr, Vaillant, T, de Oliveira, V M, Barbosa, D, Maia, D, Aljbaae, S, Coelho, B, Bergano, M, Pandeirada, J, A F B A Prado, Guerman, A, Correia, A C M
Format:	Artikel
Sprache:	eng
Schlagworte:	Boundary value problems Cislunar space Computing time Gravitational effects Moon Optimization techniques Orbital maneuvers Physics - Earth and Planetary Astrophysics Physics - Instrumentation and Methods for Astrophysics Space rendezvous Spacecraft Trajectories
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