Multi-Degree-of-Freedom Active Isolation Platform for Microvibrations

Author:

Lafarga Vicente1ORCID,Jamshidi Rasa2,Rodrigues Gonçalo3,Seiler René3,Collette Christophe1

Affiliation:

1. Université Libre de Bruxelles, 1050 Brussels, Belgium

2. Liège University, 4000 Liège, Belgium

3. European Space Agency, 2200 AG Noordwijk, The Netherlands

Abstract

Reaction wheels are widely used in the attitude control of spacecraft due to their capability of applying control torques, greatly reducing the propellant requirements and limiting its use to reaction wheel desaturation. However, the presence of unavoidable mechanical imperfections results in significant mechanical disturbances, being applied to the spacecraft, which can severely impact the operation of sensitive payloads. These microvibrations are broadband in nature, and therefore the effective mitigation of their effects requires a high isolation factor throughout a wide frequency range. This paper presents the development and experimental verification of a six-degree-of-freedom active isolation platform for a reaction wheel, integrating a soft suspension and active control using self-sensing actuators. A reduction in the transmitted forces of 65 dB at 270 Hz was experimentally demonstrated, while exhibiting negligible amplifications by its suspension resonance, which constitute very attractive performances.

Funder

European Space Agency

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

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