Optimal rendezvous trajectory between Sample Return Orbiter and Orbiting Sample Container in a Mars Sample Return mission-Reference-Cited by-同舟云学术

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Optimal rendezvous trajectory between Sample Return Orbiter and Orbiting Sample Container in a Mars Sample Return mission

Published:2020-06 Issue: Volume:171 Page:31-41
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Fossà Alberto,Bettanini Carlo^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference19 articles.

1. The Global Exploration Roadmap;Group,2013

2. Roadmap to a human Mars mission;Salotti;Acta Astronaut.,2014

3. Global Human Mars System Missions Exploration, Goals, Requirements and Technologies;Genta,2016

4. Trade space evaluation of ascent and return architectures for a Mars Sample Return mission;Alibay,2014

5. A Mars Ascent Vehicle for potential mars sample return;Shotwell,2017

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Trajectory optimization of space vehicle in rendezvous proximity operation with evolutionary feasibility conserving techniques;Engineering Applications of Artificial Intelligence;2023-01

2. Conceptual design and assessment of a mars orbital logistics node for sustainable human exploration;Acta Astronautica;2021-12

3. Fast optimization of impulsive perturbed orbit rendezvous using simplified parametric model;Astrodynamics;2021-12

4. Air traffic control with prognosticated flight trajectory;Journal of Physics: Conference Series;2020-11-01

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