Systematic vectored thrust calibration method for satellite momentum control

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

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Bibliographische Detailangaben
Hauptverfasser: YOCUM, JR., JOHN F, BARSKEY, MICHAEL F
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A method of simultaneously performing a translational maneuver of a spacecraft by a thruster and dumping momentum from the spacecraft during a time period P. The method entails aligning the thruster along a thrust vector which is fixed during the time period P, wherein the thrust vector is aligned with the center of mass of the spacecraft at a time P/2, and firing the thruster throughout the time period P.