NASA/TM-209009, Nurre, G.S. and Whorton, M.S. and Kim*, Y.K., A TREETOPS Simulation of the STABLE Microgravity Vibration Isolation System, Structures and Dynamics Laboratory, Science and Engineering Directorate, NASA Marshall Space Flight Center, AL 35812, and *University of Alabama in Huntsville, January 1999, pp. 56, Format(s): PDF 926k |
As a research facility for microgravity science, the International Space Station(ISS) will be used for numerous experiments which require a quiescent acceleration environment across a broad spectrum of frequencies. For many microgravity science experiments, the ambient acceleration environment on ISS will significantly exceed desirable levels. The ubiquity of acceleration disturbance sources and the difficulty in characterization of these sources precludes source isolation, requiring vibration isolation to attenuate the disturbances to an acceptable level at the experiment. To provide a more quiescent acceleration environment, a vibration isolation system named STABLE (Suppression of Transient Accelerations By LEvitation) was developed. STABLE was the first successful flight test of an active isolation device for microgravity science payloads and was flown on STS-73/USML-2 in October 1995. This report documents the development of the high fidelity, nonlinear, multibody simulation developed using TREETOPS which was used to design the control laws and define the expected performance of the STABLE isolation system
| Keywords: | microgravity, vibration isolation, simulation, stable |
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| Subjects: | Astronautics: Spacecraft Design, Testing And Performance |
| ID Code: | 498 |
| Deposited On: | 24 July 2002 |