Estimation of the Microaccelerations on an Automatic Rotary Vibration Isolation Device

The paper investigates the field of microaccelerations inside the protected zone of a microgravity platform of the mechanical principle of action. The platform is a 2-stage gyroscope. A container with technological equipment is fixed on the inner frame. A model of the microacceleration field in the working area of the technological equipment during the implementation of the directed crystallization process is constructed. In a simulation, data from assessments of the parts of the angular velocity direction of the rotation of the small spacecraft “Aist-2D” were used. Using these data, a microacceleration model was constructed and a microgravity platform control law was developed. When implementing this control law, near-zero values of microaccelerations are obtained inside the protected zone of the microgravity platform. These results can be used for small spacecraft missions.

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Publication Details

Journal
Space Science & Technology
Published
2025-01-01
DOI
https://doi.org/10.34133/space.0292
Primary Topic
Magnetic and Electromagnetic Effects
Type
article
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article

Estimation of the Microaccelerations on an Automatic Rotary Vibration Isolation Device

A. V. Sedelnikov, A S Taneeva, L. A. Manukyan
Space Science & Technology
Magnetic and Electromagnetic Effects
article

Estimation of the Microaccelerations on an Automatic Rotary Vibration Isolation Device

A. V. Sedelnikov, A S Taneeva, L. A. Manukyan
article en

Abstract

The paper investigates the field of microaccelerations inside the protected zone of a microgravity platform of the mechanical principle of action. The platform is a 2-stage gyroscope. A container with technological equipment is fixed on the inner frame. A model of the microacceleration field in the working area of the technological equipment during the implementation of the directed crystallization process is constructed. In a simulation, data from assessments of the parts of the angular velocity direction of the rotation of the small spacecraft “Aist-2D” were used. Using these data, a microacceleration model was constructed and a microgravity platform control law was developed. When implementing this control law, near-zero values of microaccelerations are obtained inside the protected zone of the microgravity platform. These results can be used for small spacecraft missions.

Space Science & TechnologyVol. 5
Samara National Research University (RU)
Affordable and clean energy
Openalex Percentile: Top 88%
Magnetic and Electromagnetic Effects
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