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Abstract

Mass Spring Systems (MSS) are often used to simulate the behavior of deformable objects, for example in computer graphics (modeling clothes for virtual characters) or in medicine (surgical simulators that facilitate the planning of surgical operations) due to their simplicity and speed of calculation. This paper presents a new, two-parameter method (TP MSS) of determining the values of spring coefficients for this model. This approach can be distinguished by a constant parameter which is calculated once at the beginning of the simulation, and a variable parameter that must be updated at each simulation step. The value of this variable parameter depends on the shape changes of the elements forming the mesh of the simulated object. The considered mesh is built of elements in the shape of acute-angled triangles. The results obtained using the new model were compared to FEM simulations and the Van Gelder model. The simulation results for the new model were also compared with the results of the bubble inflation test.
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Bibliography

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[8] Y. Nimura, J. D. Qu, Y. Hayashi, M. Oda, T. Kitasaka, M. Hashizume, K. Misawa, and K. Mori. Pneumoperitoneum simulation based on mass-spring-damper models for laparoscopic surgical planning. Journal of Medical Imaging, 2(4):044004, 2015. doi: 10.1117/1.JMI.2.4.044004.
[9] H. Dehghani Ashkezari, A. Mirbagheri, S. Behzadipour, and F. Farahmand. A mass-spring-damper model for real time simulation of the frictional grasping interactions between surgical tools and large organs. Scientia Iranica, 22(5):1833–1841, 2015.
[10] B. Dong, J. Li, G. Yang, X. Cheng, and Q. Gang. A multi-component conical spring model of soft tissue in virtual surgery. IEEE Access, 8:146093–146104, 2020. doi: 10.1109/ACCESS.2020.3014730.
[11] X. Zhang, J. Duan, W. Sun, T. Xu, and S.K. Jha. A three-stage cutting simulation system based on mass-spring model. Computer Modeling in Engineering & Sciences, 127(1):117–133, 2021. doi: 10.32604/cmes.2021.012034.
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[21] W.P. Jackson. Characterization of Soft Polymers and Gels using the Pressure-Bulge Technique. Ph.D. Thesis, California Institute of Technology, Pasadena, USA, 2008.
[22] L. Wanigasooriya. Mechanical Characterisation and Ram Extrusion of Wheat Flour Dough. Ph.D. Thesis, Imperial College London, UK, 2006.
[23] P. Jaszak. Modelling of the rubber in Finite Element Method. Elastomery, 20(3):31–39, 2016. (in Polish).
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[26] P. Małkowski and Ł. Ostrowski. The methodology for the young modulus derivation for rocks and its value. Procedia Engineering, 191:134–141, 2017. doi: 10.1016/j.proeng.2017.05.164.
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Authors and Affiliations

Sylwester Tudruj
1
ORCID: ORCID
Krzysztof Kurec
2
ORCID: ORCID
Janusz Piechna
1
ORCID: ORCID
Konrad Kamieniecki
2
ORCID: ORCID

  1. Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics, Warsaw, Poland
  2. Warsaw University of Technology, Institute of Micromechanics and Photonics, Warsaw, Poland
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Abstract

Microvibrations are mechanical oscillations caused by components such as the reaction wheels of an attitude control system of a spacecraft. These microvibrations are transferred through the spacecraft structure onto important instruments (e.g., optical instruments), causing those to produce diminished results (e.g., reduced image quality, imprecise geolocation etc.). At the present state, microvibrations in spacecraft cannot be actively controlled because their very high frequencies of up to 1000 Hz are above the control bandwidth a current attitude control system can provide. However, being able to reduce the effects of microvibrations on a space mission is becoming increasingly more critical as the envelope of future optical satellite missions expands. Furthermore, the advancements made in the performance of small satellites as well as the growing interest in laser and quantum communication call for a cost-efficient solution for managing microvibrations. This paper describes how cheap MEMS-based measurement systems have already proven that they are a potential solution. Showing high sensitivity and low-noise performance while allowing fast and easy prototyping.
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Bibliography

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[9] A. Wiebe. Entwicklung eines Teststandes zur Messung von Mikrovibrationen inklusive Auslegung eines Datenaufnahmesystems. Technical report, 2021.
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Authors and Affiliations

Antonio Garcia
1
Tim Gust
1
Enes Basata
1
Tim Gersting
1
Michal Deka
1
Sven Thiele
1
Mohammad Salah
1
Matias Bestard Koerner
2
Torben Runte
3
Miguel Gonzalez
3

  1. City University of Applied Sciences Bremen, Institute of Aerospace Technologies, Bremen, Germany
  2. German Aerospace Center – DLR, Institute of Space Systems. Guidance, Navigation and Control Systems. Bremen, Germany
  3. OHB System AG, Bremen, Germany
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Abstract

The article aims at assessing the influence of the drill bit material on the bearing strength of holes made in glass fabric reinforced epoxy composite. Six twists made of widely used drill materials such as high speed steels and carbides in different configurations were selected to drill holes in the composite. In the first stage of the work, optimum drilling parameters were selected and then used for drilling holes in specimens tested in single lap shear experiments. For each tested specimen two different delamination factors, one based on the delamination area and another - on its diameter, were calculated in order to assess the quality of the holes and then compared to the results of the bearing strength experiments. The results of the bearing tests showed that the highest strength was achieved for the high speed steel drill with titanium coating while the lowest for the cemented carbide drill. This finding is in opposition to the majority of results reported in literature.
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Bibliography

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Authors and Affiliations

Anna Galińska
1
ORCID: ORCID

  1. Warsaw University of Technology, Faculty of Power and Aeronautical Engineering, Warsaw, Poland

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