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Space debris represent a true risk for current and future activities in the circumterrestrial space, and remediation activities must be set out to guarantee the access to space in the future. For active debris removal, the development of an effective capturing mechanism remains an open issue. Among several proposals, cable nets are light, easily packable, scalable, and versatile. Nonetheless, guidance, navigation, and control aspects are especially critical in both the capture and post-capture phases. We present a finite element model of a deployable cable net. We consider a lumped mass/cable net system taking into account non-linearities arising both from large displacements and deformations, and from the different response of cables when subject to tension and compression. The problem is stated by using the nodal coordinates as Lagrangian coordinates. Lastly, the nonlinear governing equations of the system are obtained in a form ready for numerical integration.
Słowa kluczowe
Rocznik
Tom
Strony
21--25
Opis fizyczny
Bibliogr. 14 poz., fig.
Twórcy
autor
- University of Pisa (Italy)
autor
- University of Pisa (Italy)
autor
- University of Pisa (Italy)
Bibliografia
- [1] Inter-Agency Space Debris Coordination Committee, IADC space debris mitigation guidelines, IADC-02-01, Revision 3 ed., 2021.
- [2] Inter-Agency Space Debris Coordination Committee, Support to the IADC space debris mitigation guidelines, IADC-04-06, Revision 5.8 ed., 2021.
- [3] A. A. Baranov, D. A. Grishko, G. A. Shcheglov, A. S. Sholmin, M. V. Stognii and N. D. Kamenev, “Feasibility analysis of LEO and GEO large space debris de/re-orbiting taking into account launch mass of spacecraft-collector and its configuration layout,” Adv. Space Res., vol. 67, pp. 371-383, 2021.
- [4] C. Pardini and L. Anselmo, “Evaluating the impact of space activities in low earth orbit,” Acta Astronaut., vol. 184, pp. 11-22, 2021.
- [5] J. Virgili-Llop and M. Romano, “Simultaneous capture and detumble of a resident space object by a free-flying spacecraft-manipulator system,” Front. Robot. AI, vol. 6, p. 14, 2019.
- [6] M. Shan, J. Guo and E. Gill, “Review and comparison of active space debris capturing and removal methods,” Prog. Aerosp. Sci., vol. 80, pp. 18-32, 2016.
- [7] R. Benvenuto, S. Salvi and M. Lavagna, “Dynamics analysis and GNC design of flexible systems for space debris active removal,” Acta Astronaut., vol. 110, pp. 247-265, 2015.
- [8] E. M. Botta, I. Sharf and A. K. Misra, “Energy and momentum analysis of the deployment dynamics of nets in space,” Acta Astronaut., vol. 140, pp. 554-564, 2017.
- [9] M. Shan, J. Guo and E. Gill, “Deployment dynamics of tethered-net for space debris removal,” Acta Astronaut., vol. 132, pp. 293-302, 2017.
- [10] A. A. Shabana, “Computer implementation of the absolute nodal coordinate formulation for flexible multibody dynamics,” Nonlin. Dyn., vol. 16, pp. 293-306, 1998.
- [11] J. Gerstmayr and A. A. Shabana, “Analysis of thin beams and cables using the absolute nodal co-ordinate formulation,” Nonlin. Dyn., vol. 45, pp. 109-130, 2006.
- [12] P. S. Valvo, “Derivation of symmetric secant stiffness matrices for nonlinear finite element analysis,” Adv. Sci. Technol. Res. J., vol. 22, 2022.
- [13] R. W. Ogden, Non-linear Elastic Deformations, Chichester: Ellis Horwood, 1984.
- [14] R. W. Clough and J. Penzien, Dynamics of Structures, 3rd ed., Berkeley: Computers & Structures, 2033.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-07f9ed05-ef2a-4148-b815-8d207ca3f80b
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