TY - RPRT A1 - Büdenbender, Martin T1 - Entflechtung von Stromnetzen in Deutschland und Europa im Rahmen des dritten EU-Legislativpakets – Eine Problemdarstellung T2 - Arbeitspapiere des Instituts für Genossenschaftswesen der Westfälischen Wilhelms-Universität Münster, Nr. 91 Y1 - 2010 ER - TY - CHAP A1 - Borggräfe, Andreas A1 - Dachwald, Bernd T1 - Mission performance evaluation for solar sails using a refined SRP force model with variable optical coefficients T2 - 2nd International Symposium on Solar Sailing N2 - Solar sails provide ignificant advantages over other low-thrust propulsion systems because they produce thrust by the momentum exchange from solar radiation pressure (SRP) and thus do not consume any propellant.The force exerted on a very thin sail foil basically depends on the light incidence angle. Several analytical SRP force models that describe the SRP force acting on the sail have been established since the 1970s. All the widely used models use constant optical force coefficients of the reflecting sail material. In 2006,MENGALI et al. proposed a refined SRP force model that takes into account the dependancy of the force coefficients on the light incident angle,the sail’s distance from the sun (and thus the sail emperature) and the surface roughness of the sail material [1]. In this paper, the refined SRP force model is compared to the previous ones in order to identify the potential impact of the new model on the predicted capabilities of solar sails in performing low-cost interplanetary space missions. All force models have been implemented within InTrance, a global low-thrust trajectory optimization software utilizing evolutionary neurocontrol [2]. Two interplanetary rendezvous missions, to Mercury and the near-Earth asteroid 1996FG3, are investigated. Two solar sail performances in terms of characteristic acceleration are examined for both scenarios, 0.2 mm/s2 and 0.5 mm/s2, termed “low” and “medium” sail performance. In case of the refined SRP model, three different values of surface roughness are chosen, h = 0 nm, 10 nm and 25 nm. The results show that the refined SRP force model yields shorter transfer times than the standard model. Y1 - 2010 N1 - 2nd International Symposium on Solar Sailing, ISSS 2010, 2010-07-20 - 2010-07-22. New York City College of Technology of the City University of New York, USA SP - 1 EP - 6 ER - TY - CHAP A1 - Dachwald, Bernd T1 - Solar sail dynamics and control T2 - Encyclopedia of Aerospace Engineering N2 - Solar sails are large and lightweight reflective structures that are propelled by solar radiation pressure. This chapter covers their orbital and attitude dynamics and control. First, the advantages and limitations of solar sails are discussed and their history and development status is outlined. Because the dynamics of solar sails is governed by the (thermo-)optical properties of the sail film, the basic solar radiation pressure force models have to be described and compared before parameters to measure solar sail performance can be defined. The next part covers the orbital dynamics of solar sails for heliocentric motion, planetocentric motion, and motion at Lagrangian equilibrium points. Afterwards, some advanced solar radiation pressure force models are described, which allow to quantify the thrust force on solar sails of arbitrary shape, the effects of temperature, of light incidence angle, of surface roughness, and the effects of optical degradation of the sail film in the space environment. The orbital motion of a solar sail is strongly coupled to its rotational motion, so that the attitude control of these soft and flexible structures is very challenging, especially for planetocentric orbits that require fast attitude maneuvers. Finally, some potential attitude control methods are sketched and selection criteria are given. KW - solar sail KW - sailcraft KW - orbital dynamics KW - orbit control KW - attitude dynamics Y1 - 2010 U6 - https://doi.org/10.1002/9780470686652.eae292 PB - Wiley CY - Hoboken ER - TY - RPRT A1 - Temiz Artmann, Aysegül T1 - Frühgeburtenrate mindern durch ein Prognoseverfahren für den vorzeitigen Blasensprung - PROMPT (Premature rupture of membranes prediction test) : Abschlussbericht ; Laufzeit des Vorhabens: 01.03.2007 - 31.12.2009 Y1 - 2010 U6 - https://doi.org/10.2314/GBV:644277858 N1 - Förderkennzeichen BMBF 1772X07 PB - Technische Informationsbibliothek u. Universitätsbibliothek CY - Aachen ER - TY - JOUR A1 - Grajewski, Matthias A1 - Köster, Michael A1 - Turek, Stefam T1 - Numerical analysis and implementational aspects of a new multilevel grid deformation method JF - Applied Numerical Mathematics N2 - Recently, we introduced and mathematically analysed a new method for grid deformation (Grajewski et al., 2009) [15] we call basic deformation method (BDM) here. It generalises the method proposed by Liao et al. (Bochev et al., 1996; Cai et al., 2004; Liao and Anderson, 1992) [4], [6], [20]. In this article, we employ the BDM as core of a new multilevel deformation method (MDM) which leads to vast improvements regarding robustness, accuracy and speed. We achieve this by splitting up the deformation process in a sequence of easier subproblems and by exploiting grid hierarchy. Being of optimal asymptotic complexity, we experience speed-ups up to a factor of 15 in our test cases compared to the BDM. This gives our MDM the potential for tackling large grids and time-dependent problems, where possibly the grid must be dynamically deformed once per time step according to the user's needs. Moreover, we elaborate on implementational aspects, in particular efficient grid searching, which is a key ingredient of the BDM. Y1 - 2010 U6 - https://doi.org/10.1016/j.apnum.2010.03.017 SN - 0168-9274 VL - 60 IS - 8 SP - 767 EP - 781 PB - Elsevier CY - Amsterdam ER - TY - CHAP A1 - Matcha, Heike A1 - Ljubas, Ante T1 - Parametric Origami: Adaptable temporary buildings T2 - Future cities: 28th eCAADe Conference Proceedings. eCAADe: Conferences. Zurich, Switzerland Y1 - 2010 SN - 978-0-9541183-7-2 SP - 243 EP - 251 ER - TY - BOOK A1 - Matcha, Heike T1 - Expo 15 : Experimental Parametric Object ; Realisierung des Messestandes "Digital Origami" für den Fachbereich Architektur der Technischen Universität Darmstadt Y1 - 2010 PB - Technische Universität Darmstadt CY - Darmstadt ER - TY - CHAP A1 - Matcha, Heike ED - Hauschild, Moritz ED - Karzel, Rüdiger T1 - Regelbasierte Planung - Parametrik T2 - Digitale Prozesse : Planung, Gestaltung, Fertigung Y1 - 2010 SN - 978-3-95553-022-8 U6 - https://doi.org/10.11129/detail.9783955530228 N1 - auch gedruckt in der Bereichsbibliothek Bayernallee unter der Signatur 11 WTP 101 SP - 24 EP - 24 PB - Detail CY - München ER - TY - CHAP A1 - Matcha, Heike ED - Hauschild, Moritz ED - Karzel, Rüdiger T1 - Regelbasierte Planung - Parametrik T2 - Digitale Prozesse: Planung, Gestaltung, Fertigung Y1 - 2010 SN - 978-3-920034-35-5 N1 - gedruckt in der Bereichsbibliothek Bayernallee unter der Signatur: 11 WTP 101 ; auch als Online-Ausgabe verfügbar SP - 24 EP - 24 PB - Ed. Detail CY - München ER - TY - BOOK A1 - Matcha, Heike A1 - Quasten, Gero A1 - Rabighomi, Hossein T1 - Qualitätssteigerung im verdichteten Wohnungsbau über Erzeugung größerer Vielfalt und Flexibilität durch individualisierte Massenfertigung am Beispiel gestapelter Reihenhäuser Y1 - 2010 SN - 978-3-8167-8216-2 PB - Fraunhofer IRB Verlag CY - Stuttgart ER -