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Design Considerations and Deployment Simulations of Spinning Space Webs
KTH, Skolan för teknikvetenskap (SCI), Mekanik.
KTH, Skolan för teknikvetenskap (SCI), Mekanik.ORCID-id: 0000-0001-6802-8331
Advanced Concepts Team, EUI-ACT, ESTEC, Keplerlaan.
2007 (engelsk)Inngår i: 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structual Dynamics and Materials Conrerence: Waikiki, HI; 23 April 2007 through 26 April 2007, 2007, s. 1503-1512Konferansepaper, Publicerat paper (Fagfellevurdert)
Abstract [en]

ESA Advanced Concepts Team (ACT) has proposed to construct large space antennas and solar power systems by deploying and stabilising a large web in space. The idea originates from the Japanese "Furoshiki Satellite". Since an overly complicated control system contributed to the partly chaotic deployment, ACT suggests to use centrifugal forces to deploy the space web. In this study the design and folding pattern of space webs are discussed. An analytical model and a finite element model used to describe the deployment, from the chosen folding, are presented. Free deployment of space webs is studied and a first control strategy that enables controlled and stable deployment is suggested.

sted, utgiver, år, opplag, sider
2007. s. 1503-1512
Serie
Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, ISSN 0273-4508
Emneord [en]
Finite element method; Mathematical models; Receiving antennas; Satellites; Solar cells; Solar power systems; Space web; Spinning space webs
HSV kategori
Identifikatorer
URN: urn:nbn:se:kth:diva-9645Scopus ID: 2-s2.0-34547497219ISBN: 978-1-56347-892-5 (tryckt)OAI: oai:DiVA.org:kth-9645DiVA, id: diva2:126803
Merknad
QC 20100729Tilgjengelig fra: 2008-11-21 Laget: 2008-11-21 Sist oppdatert: 2010-07-29bibliografisk kontrollert
Inngår i avhandling
1. Deployment Control of Spinning Space Webs and Membranes
Åpne denne publikasjonen i ny fane eller vindu >>Deployment Control of Spinning Space Webs and Membranes
2008 (engelsk)Doktoravhandling, med artikler (Annet vitenskapelig)
Abstract [en]

Future solar sail and solar power satellite missions require deployment of large and lightweight flexible structures in space. One option is to spin the assembly and use the centrifugal force for deployment, stiffening and stabilization. Some of the main advantages with spin deployment are that the significant forces are in the plane of rotation, a relatively simple control can be used and the tension in the membrane or web can be adjusted by the spin rate to meet the mission requirements. However, a successful deployment requires careful development of new control schemes. The deployment rate can be controlled by a torque, applied either to a satellite in the center or by thrusters in the corners, or by deployment rate control, obtained by tether, spool braking or folding properties.

Analytical models with only three degrees of freedom were here used to model the deployment of webs and membranes for various folding patterns and control schemes, with focus on space webs folded in star-like arms coiled around a center hub. The model was used to investigate control requirements and folding patterns and to obtain optimal control laws for centrifugal deployment. New control laws were derived from the optimal control results and previously presented control strategies. Analytical and finite element simulations indicate that the here developed control laws yield less oscillations, and most likely more robustness, than existing controls.

Rotation-free (RF) shell elements can be used to model inflation or centrifugal deployment of flexible memebrane structures by the finite element method. RF elements approximate the rotational degrees of freedom from the out-of-plane displacements of a patch of elements, and thus avoid common singularity problems for very thin shells. The performance of RF shell elements on unstructured grids is investigated in the last article of this thesis, and it is shown that a combination of existing RF elements performs well even for unstructured grids.

sted, utgiver, år, opplag, sider
Stockholm: KTH, 2008. s. x, 64
Serie
Trita-MEK, ISSN 0348-467X ; 2008:10
Emneord
Flexible structures, space webs, membranes, solar sails, solar power systems, deployment control, optimal control, centrifugal force deployment, spin deployment, rotation-free, shell elements
HSV kategori
Identifikatorer
urn:nbn:se:kth:diva-9574 (URN)
Disputas
2008-12-08, F3, KTH, Lindstedtsvägen 26, Stockholm, 10:00 (engelsk)
Opponent
Veileder
Merknad
QC 20100729Tilgjengelig fra: 2008-11-21 Laget: 2008-11-17 Sist oppdatert: 2010-07-29bibliografisk kontrollert

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