Literatura científica selecionada sobre o tema "Sloshing compensation"

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Artigos de revistas sobre o assunto "Sloshing compensation"

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Wang, Zhiyi, Tingyu Wang, Yongqiang Yang, Xiaotao Mi, and Jianli Wang. "Differential Confocal Optical Probes with Optimized Detection Efficiency and Pearson Correlation Coefficient Strategy Based on the Peak-Clustering Algorithm." Micromachines 14, no. 6 (2023): 1163. http://dx.doi.org/10.3390/mi14061163.

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Quantifying free-form surfaces using differential confocal microscopy can be challenging, as it requires balancing accuracy and efficiency. When the axial scanning mechanism involves sloshing and the measured surface has a finite slope, traditional linear fitting can introduce significant errors. This study introduces a compensation strategy based on Pearson’s correlation coefficient to effectively reduce measurement errors. Additionally, a fast-matching algorithm based on peak clustering was proposed to meet real-time requirements for non-contact probes. To validate the effectiveness of the c
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Limarchenko, O., C. Cattani, and V. Pilipchuk. "Structure of geometrical nonlinearities in problems of liquid sloshing in tanks of non-cylindrical shape." Mathematical Modeling and Computing 1, no. 2 (2014): 195–213. http://dx.doi.org/10.23939/mmc2014.02.195.

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Structure of geometrical nonlinearities in mathematical model of liquid sloshing in tanks of non-cylindrical shape is under consideration. In contrast to the case of cylindrical reservoir, some new types of nonlinearities occur in mathematical statement of the problem. They are connected with four main reasons. First, they are determined by new normal modes, which correspond to non-cylindrical shape of the tank and take into account some nonlinear properties of the problem (for example, they follow tank walls above level of a free surface). Second, determination of the potential energy of the
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Kimura, S., M. Hamaguchi, and T. Taniguchi. "Transfer Control of Liquid Container by a Autonomous Mobile Robot with Sloshing Compensator." Proceedings of JSME annual Conference on Robotics and Mechatronics (Robomec) 2002 (2002): 85. http://dx.doi.org/10.1299/jsmermd.2002.85_5.

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Liu, Feng, Baozeng Yue, Bole Ma, and Cong Feng. "Wave-based attitude control of in-orbit spacecraft with large-amplitude slosh." Journal of Vibration and Control, December 22, 2022, 107754632211473. http://dx.doi.org/10.1177/10775463221147339.

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This paper aims to reach high-quality attitude control and large-amplitude slosh suppression when a typical liquid-filled spacecraft executes three-axial large-angle maneuvers, by applying a wave-based attitude controller (WBAC). First, the sloshing dynamics is modeled by using a spherical pendulum, whose motion is expressed by splitting its coordinates. Thus, the large-amplitude lateral sloshing and the rotary sloshing as well as the over-all rigid motion of a liquid with respect to the tank in spacecraft can be approximately described. Second, the dynamics equations of system in terms of hyb
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Han, Lei. "Mechanism on the short-term variability of the Atlantic meridional overturning circulation in the subtropical and tropical regions." Journal of Physical Oceanography, July 6, 2023. http://dx.doi.org/10.1175/jpo-d-23-0027.1.

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Abstract The continuous, moored observation revealed significant variability in the strength of the Atlantic Meridional Overturning Circulation (AMOC). Cause of such AMOC variability is an extensively studied subject. This study focuses on the short-term variability, which ranges up to seasonal and interannual timescales. A mechanism is proposed from the perspective of ocean water redistribution by layers. By offering explanations for four phenomena of AMOC variability in the subtropical and tropical oceans (seasonality, meridional coherence, layered-transport compensation as observed at 26.5°
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Gandhi, Prasanna S., Keyur B. Joshi, and N. Ananthkrishnan. "Design and Development of a Novel 2DOF Actuation Slosh Rig." Journal of Dynamic Systems, Measurement, and Control 131, no. 1 (2008). http://dx.doi.org/10.1115/1.3023113.

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Sloshing of liquid in a tank is critical in several areas, including launch vehicles carrying liquid fuel, satellites, industrial packaging of liquids, systems handling molten metal, and so on. Hence modeling, characterization, and control of nonlinear slosh phenomena are important in these applications. To study slosh dynamics, develop useful identification schemes, and design and verify slosh control algorithms, a new 2DOF actuation slosh rig is reported in this paper considering the fact that most of the times these tanks are subjected to linear as well as pitching excitation/control inputs
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Teses / dissertações sobre o assunto "Sloshing compensation"

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Magnani, Guido. "Advanced satellite attitude control strategies under actuation constraints and multiple sources of disturbance." Electronic Thesis or Diss., Toulouse, ISAE, 2024. http://www.theses.fr/2024ESAE0046.

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Dans un scénario de satellites géostationnaires hautement autonomes, dotés de capacités d'auto-assemblage et d'auto-maintenance, les perturbations des bras manipulateurs couplées à la dynamique de ballotement du carburant représentent un risque significatif de dégradation des performances du système de contrôle d'attitude et d'orbite du satellite. Bien que des solutions passives existent pour amortir le ballotement du carburant et compenser les perturbations des bras manipulateurs, il manque une solution de contrôle actif unique capable de compenser ces perturbations tout en évitant de manière
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Trabalhos de conferências sobre o assunto "Sloshing compensation"

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Santilli, Francesco, Andrew Hyslop, Mariel Triggianese, et al. "The CIMR satellite– challenges and design solutions for AOCS system." In ESA 12th International Conference on Guidance Navigation and Control and 9th International Conference on Astrodynamics Tools and Techniques. ESA, 2023. http://dx.doi.org/10.5270/esa-gnc-icatt-2023-177.

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The Copernicus Imaging Microwave Radiometer (CIMR) is a European Earth Observation mission consisting of 2 satellites (with an option of the extension to the third one). It will provide high resolution global monitoring of the Earth surface emissions across various frequency bands, in particular floating sea ice parameters. The 3-axis stabilized spacecraft(s) will operate in a sun synchronous orbit with 817 km altitude. The instrument features a deployable mesh reflector with the diameter of 8 meters and its feed cluster, which rotates at 8 rpm to produce a 1900km wide ground swath. The CIMR m
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