Mixture-Ratio Control to Improve Hydrogen-Fuel Rocket Performance

The rocket equation of motion, in the absence of gravitational and aerodynamic forces, is integrated by considering the propellant mixture ratio as the problem control variable. The theory of optimal control is applied to obtain the control law, which maximizes the payload for an assigned velocity i...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Journal of spacecraft and rockets 1997-03, Vol.34 (2), p.214-217
Hauptverfasser:	Colasurdo, Guido, Pastrone, Dario, Casalino, Lorenzo
Format:	Artikel
Sprache:	eng
Schlagworte:	Hydrogen fuels
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!