Solution algorithm of a quasi-Lambert's problem with fixed flight-direction angle constraint

DOI10.1007/S10569-011-9335-5zbMath1270.70070OpenAlexW1965421320MaRDI QIDQ362649

Chao Han, Qinqin Luo, Zhanfeng Meng

Publication date: 30 August 2013

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-011-9335-5

zbMATH Keywords

two-point boundary value problemiteration algorithmflight-direction anglequasi-Lambert's problemuniversal variable

Mathematics Subject Classification ID

Two-body problems (70F05) Orbital mechanics (70M20)

Related Items (1)

Revisiting Lambert's problem

Cites Work

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• Cooperative evolutionary algorithm for space trajectory optimization
• A procedure for the solution of Lambert's orbital boundary-value problem
• A new procedure for the solution of the classical problem of minimal orbit determination from three lines of sight
• An elegant Lambert algorithm
• Alternative approach to the solution of Lambert's problem
• A uniform solution of the Lambert problem

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