| タイトル | The Interplay Between Hardware and Control System Design in the Development of the Active Rack Isolation System |
| 本文（外部サイト） | http://hdl.handle.net/2060/20000032438 |
| 著者（英） | Thampi, Sreekumar; Fialho, Ian J. |
| 著者所属（英） | DYNACS Engineering Co., Inc. |
| 発行日 | 2000-01-01 |
| 言語 | eng |
| 内容記述 | A primary mission of the International Space Station (ISS) is to provide a premier microgravity laboratory environment for conducting acceleration sensitive scientific research. In order to accomplish this goal, vibroacoustic disturbances caused by station activities that occur during the microgravity mode of operation, must be controlled. In addition to source isolation and other passive isolation methods, the ISS uses active isolation at the receiver, through the use of an Active Rack Isolation System (ARIS), as part of its overall vibration isolation strategy. A schematic diagram of a typical ARIS payload rack is shown. The ARIS isolation control system senses rack acceleration via three triaxial accelerometer heads and uses eight pushrod actuators to perform active vibration attenuation. Position sensors housed in the actuator assembly are used to sense the relative position between the rack and the station. Electrical power, data and other essential resources are routed through a set of umbilicals that interface with a passthrough panel at the bottom of the rack. A representative umbilical set is shown. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| 権利 | No Copyright |
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