Systematic vectored thrust calibration method for satellite mome

Aeronautics and astronautics – Spacecraft – Attitude control

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244168, 244169, 244164, B64G 128

Patent

active

057657807

ABSTRACT:
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.

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patent: 4230294 (1980-10-01), Pistiner
patent: 5133518 (1992-07-01), Flament
patent: 5337981 (1994-08-01), Bender
patent: 5349532 (1994-09-01), Tilley et al.
patent: 5443231 (1995-08-01), Anzel
patent: 5571953 (1996-11-01), Wu

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