Space Trajectories Optimization

[Introduction] - [Contacts] - [Research] - [Publications] - [Projects] - [Events] - [Teaching] - [The Giants].

We have tackled the space trajectory optimization problems proposed by the European Space Agency (ESA), which are reported in the Global Optimisation Trajectory Problems (GTOP) database.

Problem "TandEM-Atlas501" (MGA-1DSM - unconstrained continuous optimisation) and Solutions

Trajectories to Saturn: new optimal solutions found! Here is a list of the best solutions known for different fly-by sequences. Note that E = Earth, V = Venus, M = Mars, J = Jupiter, S = Saturn. The final mass is obtained from the objective function according to the expression: mass = (2 -objfun)*1000

Global Optimisation Trajectory Problems and Solutions


[Introduction] - [Contacts] - [Research] - [Publications] - [Projects] - [Events] - [Teaching] - [The Giants].

Copyright 2002-2010, Giuseppe Nicosia.
Giuseppe Nicosia, Optimization, Combinatorial Optimization, Numerical Optimization, Non Linear Optimization, Large Scale Optimization, Evolutionary Algorithms, Genetic Algorithms, Immune Algorithms, Artificial Immune Systems, Graph Coloring, String Folding, NP-complete problems, Circuit Optimization, Circuit Design, Design For Yield, Device Optimization, Bioinformatics, Structural Bioinformatics, Protein Folding, Protein Structure Prediction, HP model.