Optimal skip entry trajectory for lunar return vehicle with trim-flaps

DOI10.1155/2017/3498350zbMath1426.70021OpenAlexW2586263621WikidataQ59147483 ScholiaQ59147483MaRDI QIDQ1992631

Yin Wang, Keming Yao

Publication date: 5 November 2018

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2017/3498350

Mathematics Subject Classification ID

Problems involving a system of particles with friction (70F40) Orbital mechanics (70M20)

Cites Work

• Variational solutions for the heat-rate-limited aeroassisted orbital transfer problem
• Global Optimization Approaches for Optimal Trajectory Planning

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