Vibration Isolation, Suppression and Steering (VISS)

Author:

Wada Ben K.,Rahman Zahidul,Kedikian Roland,Kuo C. -P.1

Affiliation:

1. Jet Propulsion Laboratory, 4800 Oak Grove Dr., Pasadena, CA 91109

Abstract

The opportunities for precision space instruments will increase if they can be accommodated on a non-precise spacecraft or platform. In order to meet the precision requirements of various space instruments, the objective was to develop a six degree of freedom Vibration Isolation, Suppression and Steering (VISS) subsystem that interfaces the instrument to the spacecraft or platform. This paper results from a study to design a flight experiment to validate the VISS subsystem for a Mid-Wave Infra Red (MWIR) Camera on top of a small spacecraft. One of the major challenges is to develop a long stroke PZT actuator that is redundant and compact, with low stiffness and power efficiency. The test performance of the actuator design and the predicted VISS performance of the design is included.

Publisher

SAGE Publications

Subject

Mechanical Engineering,General Materials Science

Reference4 articles.

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. An Active Vibration Isolator for the Space Optical Clock;Instruments and Experimental Techniques;2024-04

2. Vibration Reduction for Camera Systems Onboard Small Unmanned Aircraft;Sensors and Instrumentation, Aircraft/Aerospace, Energy Harvesting & Dynamic Environments Testing, Volume 7;2019-05-04

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