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Senior Researcher

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 classical method to constrain maneuvers is mathematically modeling them using the Two Point Boundary Value Problem (TPBVP), defining spacecraft positions at the start and end of the trajectory. Find out our new paper led by Allan Kardec de Almeida Junior. #ENGAGE SKA #SST #cislunar #TFC!

Tangential velocity constraint for orbital maneuvers with Theory of Functional Connections - Scientific Reports

Tangential velocity constraint for orbital maneuvers with Theory of Functional Connections - Scientific Reports

nature.com

ATIQ AHMAD

Planet Born....Galaxy Tourist. Till today NASA, JAXA, ESA are Failed & Zero for the Space Science Studies. 100% Truth. My Leading RôLE in the Space Science Industry. If you keep Ability, Quality, Standards & Status.

8mo

Physically not True. And you NASA, JAXA, ESA, CNSA are cannot Prove & Proof it ? Because no Abilities at All.

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