Systematic vectored thrust calibration method for satellite momentum control

A method of simultaneously performing a translational maneuver of a spacecraft (20) by a thruster (36) and dumping momentum from the spacecraft (20) during a time period P. The method entails aligning the thruster (36) along a thrust vector (V) which is fixed during the time period P, wherein the th...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: YOCUM, JOHN F., JR, BARSKY, MICHAEL F
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:A method of simultaneously performing a translational maneuver of a spacecraft (20) by a thruster (36) and dumping momentum from the spacecraft (20) during a time period P. The method entails aligning the thruster (36) along a thrust vector (V) which is fixed during the time period P, wherein the thrust vector (V) is aligned with the center of mass (46) of the spacecraft (20) at a time P/2 and firing the thruster (36) throughout the time period P.