Numerical Optimization of Flight Trajectory for Rockets via Artificial Neural Networks

This research arise to optimize the flight trajectory for rockets, for this were applied hybrid techniques, based on the Finite Difference Method (FDM) to obtain the solution of the non-linear differential equations provided by the analytic modeling. So aiming at the optimizations were applied the A...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Revista IEEE América Latina 2017-01, Vol.15 (8), p.1556-1565
Hauptverfasser: do Nascimento, Eriberto Oliveira, de Oliveira, Lucas Nonato
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!