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Non-Smooth Multi-Objective Controller Synthesis for Test-Mass Actuation in Gravitational-Wave Detectors

Research output: Contribution to JournalArticleAcademicpeer-review

Abstract

This paper proposes a non-smooth controller optimization method and shows the results of ongoing research on the implementation of this method for gravitational-wave applications. Typical performance requirements concerning these type of suspensions are defined in terms of both (Formula presented.) - and (Formula presented.) -type constraints. A non-smooth optimization approach is investigated, which allows the use of non-convex cost functions that are often a result of mixed (Formula presented.) optimization problems. Besides the controller, the distribution of the actuation is integrated with the optimization to investigate the feasibility of simultaneous controller and actuator optimization. The results demonstrate that the proposed non-smooth optimization method is able to find suitable solutions for the control and actuator distribution that satisfy all required performance and design constraints.

Original languageEnglish
Article number134
Pages (from-to)1-13
Number of pages13
JournalGalaxies
Volume13
Issue number6
Early online date9 Dec 2025
DOIs
Publication statusPublished - Dec 2025

Bibliographical note

Publisher Copyright:
© 2025 by the authors.

Funding

The authors thank M. Valentini for useful discussions and input. This project has received funding from the European Research Council (ERC) under the European Union’s Horizon 2020 research and innovation program (grant agreement No. 865816).

FundersFunder number
European Research Council
Horizon 2020 Framework Programme865816

    Keywords

    • Einstein telescope
    • gravitational waves
    • non-smooth controller optimization
    • optimal control
    • payload suspension
    • vibration isolation

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