A universal approach for solving the multi-revolution Lambert’s problem

Lambert’s problem, a cornerstone of orbital mechanics, is crucial in the design and planning of space missions, from satellite rendezvous to deep-space trajectory optimization. This paper presents a universal approach (valid across all conics) to solving Lambert’s problem. By employing matrix expone...

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Vydané v:	Celestial mechanics and dynamical astronomy Ročník 137; číslo 4; s. 22
Hlavní autori:	McElreath, James, Down, Ian M., Majji, Manoranjan
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	Dordrecht Springer Nature B.V 01.08.2025
Predmet:	Accuracy Algorithms Complexity Computation Conics Convergence Deep space Efficiency Exponential functions Integrals Methods Numerical stability Orbital mechanics Orbital rendezvous Orbits Rendezvous trajectories Revolutions Satellites Space missions Time functions Trajectory optimization Trigonometric functions
ISSN:	0923-2958, 1572-9478
On-line prístup:	Získať plný text
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