Pseudostate theory based iterative preliminary design method for powered gravity-assist interplanetary trajectories-Reference-Cited by-同舟云学术

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Pseudostate theory based iterative preliminary design method for powered gravity-assist interplanetary trajectories

Published:2019-12 Issue: Volume:165 Page:139-149
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Yang Bin,Yang Hongwei,Li Shuang

Funder

National Natural Science Foundation of China

Qing Lan Project

Shanghai Aerospace Science and Technology

Science and Technology on Space Intelligent Control Laboratory

NUAA

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Hybrid algorithm for multiple gravity-assist and impulsive delta-V maneuvers;Wagner;J. Guid. Control Dyn.,2015

2. The mariner 10 mission to Venus and Mercury;Shirley;Acta Astronaut.,2003

3. Graphical method for gravity-assist trajectory design;Strange;J. Spacecr. Rocket.,2002

4. Preliminary design of multiple gravity-assist trajectories;Vasile;J. Spacecr. Rocket.,2006

5. Gravity-assisted maneuvers applied in the multi-objective optimization of interplanetary trajectories;Venditti;Acta Astronaut.,2010

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1. Design of circumlunar emergency return trajectory based on two parameters;CHIN SPACE SCI TECHN;2023

2. Pseudo-Theory-Based Optimization Design Method for Lunar Gravity-Assisted Human Earth-Mars Transfer Trajectory;Journal of Physics: Conference Series;2023-05-01

3. OPTIMAL TWO-IMPULSE INTERPLANETARY TRAJECTORIES: EARTH-VENUS AND EARTH-MARS MISSIONS;Revista Mexicana de Astronomía y Astrofísica;2023-04-01

4. Parameterized design of abort trajectories with a lunar flyby for a crewed mission;Advances in Space Research;2023-03

5. Overview of Earth-Moon Transfer Trajectory Modeling and Design;Computer Modeling in Engineering & Sciences;2023

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