Multi-swingby optimization of mission to Saturn using global optimization algorithms

DOI10.1007/S10409-009-0299-6zbMath1269.70046OpenAlexW1968191735MaRDI QIDQ358717

Jun-Feng Li, He-Xi Baoyin, Kaijian Zhu

Publication date: 9 August 2013

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-009-0299-6

zbMATH Keywords

global optimizationhybrid algorithmmission designswingby trajectory

Mathematics Subject Classification ID

Numerical optimization and variational techniques (65K10) Computational methods for problems pertaining to mechanics of particles and systems (70-08) Orbital mechanics (70M20)

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Cites Work

• Formation reconfiguration in restricted three body problem
• The art and theory of dynamic programming
• Differential evolution -- a simple and efficient heuristic for global optimization over continuous spaces
• Very low-thrust trajectory optimization using a direct SQP method
• Search space pruning and global optimisation of multiple gravity assist spacecraft trajectories
• Optimization Procedure for Preliminary Design of Opposition-Class Mars Missions
• Powered swingby

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