Multi-objective hidden genes genetic algorithm for multigravity-assist trajectory optimization
A Ellithy, O Abdelkhalik, J Englander - Journal of Guidance, Control …, 2022 - arc.aiaa.org
In multigravity-assist trajectory optimization, the size of the design space is a variable itself.
The objective functions are usually replete with local minima. This paper presents a multi …
The objective functions are usually replete with local minima. This paper presents a multi …
Multiobjective design of gravity-assist trajectories via graph transcription and dynamic programming
Multiple gravity-assist (MGA) trajectory design requires the solution of a mixed-integer
programming problem to find the best sequence among all possible combinations of …
programming problem to find the best sequence among all possible combinations of …
Deep-space trajectory optimizations using differential evolution with self-learning
JH Choi, J Lee, C Park - Acta Astronautica, 2022 - Elsevier
This paper presents spacecraft trajectory optimizations for deep-space missions requiring
multiple gravity-assists (MGA). The main algorithm is based on a self-adaptive/self-learning …
multiple gravity-assists (MGA). The main algorithm is based on a self-adaptive/self-learning …
Automatic trajectory planning for low-thrust active removal mission in low-earth orbit
M Di Carlo, JMR Martin, M Vasile - Advances in Space Research, 2017 - Elsevier
In this paper two strategies are proposed to de-orbit up to 10 non-cooperative objects per
year from the region within 800 and 1400 km altitude in Low Earth Orbit (LEO). The …
year from the region within 800 and 1400 km altitude in Low Earth Orbit (LEO). The …
Multiple near-earth asteroid rendezvous mission: Solar-sailing options
The scientific interest in near-Earth asteroids (NEAs) and the classification of some of those
as potentially hazardous for the Earth stimulated the interest in their exploration. Close-up …
as potentially hazardous for the Earth stimulated the interest in their exploration. Close-up …
[HTML][HTML] CAMELOT: computational-analytical multi-fidElity low-thrust optimisation toolbox
M Di Carlo, JM Romero Martin, M Vasile - CEAS Space Journal, 2018 - Springer
Abstract Computational-Analytical Multi-fidElity Low-thrust Optimisation Toolbox (CAMELOT)
is a toolbox for the fast preliminary design and optimisation of low-thrust trajectories. It solves …
is a toolbox for the fast preliminary design and optimisation of low-thrust trajectories. It solves …
Baseline trajectory design for solar polar detection using gravity assists
Solar polar detection can greatly enrich human understanding of the solar magnetic field.
However, accurate polar flybys are rarely involved in previous trajectory designs due to the …
However, accurate polar flybys are rarely involved in previous trajectory designs due to the …
Multiple gravity assist spacecraft trajectories design based on BFS and EP_DE algorithm
M Zuo, G Dai, L Peng, M Wang… - International Journal of …, 2016 - Wiley Online Library
The paper deals with the multiple gravity assist trajectories design. In order to improve the
performance of the heuristic algorithms, such as differential evolution algorithm, in multiple …
performance of the heuristic algorithms, such as differential evolution algorithm, in multiple …
[HTML][HTML] 多目标空间探测智能轨迹优化方案综述
李海洋, 周晓东, 张旭光 - 2022 - dlxykzxb.cnjournals.net
摘要多目标空间探测是经济理性的太空探索与开发方案, 它能以较低的花费获取巨大的收益.
多目标空间探测轨迹优化的优化空间巨大, 优化难度高, 始终是航天动力学中的研究热点 …
多目标空间探测轨迹优化的优化空间巨大, 优化难度高, 始终是航天动力学中的研究热点 …
Semi-Analytical Assessment of Multiple Gravity-Assist Opportunities Based on Feasibility Domains
Z Cao, X Li, Y Qi - Journal of Guidance, Control, and Dynamics, 2024 - arc.aiaa.org
This paper proposes a semi-analytical method for multiple gravity-assist (MGA) opportunity
assessment, which can judge the feasibility of MGA sequences and predict corresponding …
assessment, which can judge the feasibility of MGA sequences and predict corresponding …