NASA/TM-211063, Hampton*, R.D. and Beech, G.S. and Rao*, N.N.S. and Rupert*, J.K. and Kim, Y.K., A "Kane's Dynamics" Model for the Active Rack Isolation System, George C. Marshall Space Flight Center Marshall Space Flight Center, Alabama 35812, National Aeronautics and Space Administration Washington, DC 20546-0001, Prepared by Engineering Systems Department *University of Alabama in Huntsville, Huntsville, Alaba, June 2001, pp. 48, Format(s): PDF 11534k |
Many microgravity space science experiments require vibratory acceleration levels unachievable without active isolation. The Boeing Corporation's Active Rack Isolation System (ARIS) employs a novel combination of magnetic actuation and mechanical linkages to address these isolation requirements on the International Space Station (ISS). ARIS provides isolation at the rack (International Standard Payload Rack (ISPR)) level. Effective model-based vibration isolation requires (1) an appropriate isolation device, (2) an adequate dynamic (i.e., mathematical) model of that isolator, and (3) a suitable, corresponding controller. ARIS provides the ISS response to the first requirement. This paper presents one response to the second, in a state space framework intended to facilitate an optimal-controls approach to the third. The authors use "Kane's Dynamics" to develop a state-space, analytical (algebraic) set of linearized equations of motion for ARIS
| Keywords: | active rack isolation system, control, dynamics, international space station |
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| Subjects: | Engineering: Communications and Radar: Communication Systems |
| ID Code: | 566 |
| Deposited On: | 02 August 2002 |