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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Bibliographic Details
Published in:	Celestial mechanics and dynamical astronomy Vol. 137; no. 4; p. 22
Main Authors:	McElreath, James, Down, Ian M., Majji, Manoranjan
Format:	Journal Article
Language:	English
Published:	Dordrecht Springer Nature B.V 01.08.2025
Subjects:	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
Online Access:	Get full text
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