Extended analytical formulae for the perturbed Keplerian motion under low-thrust acceleration and orbital perturbations

M Di Carlo, S Graça Marto, M Vasile - Celestial Mechanics and Dynamical …, 2021 - Springer
This paper presents a collection of analytical formulae that can be used in the long-term
propagation of the motion of a spacecraft subject to low-thrust acceleration and orbital …

Low-thrust tour of the main belt asteroids

M Di Carlo, M Vasile, J Dunlop - Advances in Space Research, 2018 - Elsevier
This work presents some initial results on a possible low-thrust tour of the main asteroid belt.
The asteroids are visited through a series of fly-by's to be completed within a given time …

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 …

Spacecraft design of a multiple asteroid orbiter with re-docking lander

A Probst, R Förstner - Advances in Space Research, 2018 - Elsevier
Almost two years after the landing of Rosetta's Philae on the comet 67P/Churyumov-
Gerasimenko, the triggered enthusiasm for small planetary bodies has not stagnated …

Phase-matching homotopic method for indirect optimization of long-duration low-thrust trajectories

C Guo, J Zhang, Y Luo, L Yang - Advances in Space Research, 2018 - Elsevier
For low-thrust trajectory designs, indirect optimization methods remain attractive, as they can
guarantee optimality. Previous studies presented many effective ways to overcome the …

Multiple-Target Low-Thrust Interplanetary Trajectory of

O Çelik, DA Dei Tos, T Yamamoto, N Ozaki… - Journal of Spacecraft …, 2021 - arc.aiaa.org
DESTINY+ is a medium-class interplanetary mission, selected by the Japan Aerospace
Exploration Agency for potential launch windows in the first half of 2020s. The mission will …

A mission concept for the low-cost large-scale exploration and characterisation of near earth objects

L Walker, M Di Carlo, C Greco, M Vasile… - Advances in Space …, 2021 - Elsevier
This paper presents the preliminary mission and science analysis of a new mission concept
for the large scale, low-cost exploration of Near Earth Objects (NEOs). The concept is to …

Optimal trajectory planning for multiple asteroid tour mission by means of an incremental bio-inspired tree search algorithm

A Vroom, M Di Carlo, JMR Martin… - 2016 IEEE Symposium …, 2016 - ieeexplore.ieee.org
In this paper, a combinatorial optimisation algorithm inspired by the Physarum
Polycephalum mould is presented and applied to the optimal trajectory planning of a …

[HTML][HTML] Solar-sail mission design for multiple near-Earth asteroid rendezvous

A Peloni - 2018 - theses.gla.ac.uk
Solar sailing is the use of a thin and lightweight membrane to reflect sunlight and obtain a
thrust force on the spacecraft. That is, a sailcraft has a potentially-infinite specific impulse …

EP_DE II: A significant algorithm to search the optimal solution for global optimization of multi-gravity assist trajectory

M Zuo, G Dai, L Peng - Proceedings of the Institution of …, 2018 - journals.sagepub.com
The paper deals with the design of the optimal multiple gravity assist trajectories. An
improved search algorithm named EP_DE II with search space exploration, principal …