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Muhammad Nadeem

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2026

Integrated Active Vibration Control and Structural Health Monitoring of Flexible Spacecraft Panels

Abstract. This paper presents an integrated active vibration control (AVC) and structural health monitoring (SHM) framework for flexible spacecraft panels using offset piezoelectric stack actuators (OPSA). A three-dimensional ANSYS finite-element model of a hub–panel assembly with eccentric OPSA mounting is reduced to...

Muhammad Nadeem · 0 citations

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