| タイトル | Dynamic Control System Performance during Commissioning of the Space Technology 7-Disturbance Reduction System Experiment of LISA Pathfinder |
| 本文（外部サイト） | http://hdl.handle.net/2060/20170001465 |
| 著者（英） | Romero-Wolf, Andrew; Hsu, Oscar; Ziemer, John; Maghami, Peiman; O’Donnell, James R., Jr. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 2017-02-03 |
| 言語 | eng |
| 内容記述 | The Space Technology-7 Disturbance Reduction System (DRS) launched aboard the European Space Agency's LISA Pathfinder spacecraft on December 3, 2015, after more than a decade in development. DRS consists of three primary components: an Integrated Avionics Unit (IAU), Colloidal MicroNewton Thrusters, and Dynamic Control System (DCS) algorithms implemented on the IAU. During the portions of the mission in which the DRS was under control, the DCS was responsible for controlling the spacecraft and the free-floating test masses that were part of the LISA Test Package. The commissioning period was originally divided into two periods: before propulsion separation and after propulsion separation. A recommissioning period was added after an anomaly occurred in the thruster system. The paper will describe the activities used to commission DRS, present results from the commissioning of the DCS and the recommissioning activities per-formed after the thruster anomaly. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | AAS 17-166
GSFC-E-DAA-TN38831-1 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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