A Low-Complexity Algorithm to Determine Trajectories Within the Circular Restricted Three-Body Problem

With the growing volume of traffic within the Cislunar region, there is an increasing need for efficient techniques to propagate trajectories of spacecraft in the circular restricted three-body problem. A low-complexity algorithm utilizing interpolation and incorporating boundary conditions is intro...

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Vydané v:	The Journal of the astronautical sciences Ročník 70; číslo 6; s. 46
Hlavní autori:	Canales, David, Perera, Sirani M., Kurttisi, Atahan, Baker-McEvilly, Brian
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	New York Springer US 07.11.2023 Springer Nature B.V
Predmet:	Accuracy Aerospace Technology and Astronautics Algorithms Boundary conditions Complexity Cost control Engineering Equilibrium Iterative methods Mathematical Applications in the Physical Sciences Moon Numerical analysis Orbits Original Article Propagation Retrograde orbits Space Exploration and Astronautics Space Sciences (including Extraterrestrial Physics Spacecraft Three body problem Trajectories India Low-complexity algorithm Periodic orbits Navigation Cislunar realm Three-body problem
ISSN:	2195-0571, 0021-9142, 2195-0571
On-line prístup:	Získať plný text
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