Postdigital interfaces and the aesthetics of recruitment

This paper analyses reconfigurations of play in emergent digital materialities of game design. It extends recent work examining dimensions of hybridity in playful products by turning attention to interfaces, practices and spaces, rather than devices. We argue that the concept of hybrid play relies on predefining clear and distinct digital or material entities that then enter into hybrid situations. Drawing on concepts of the ‘interface’ and ‘postdigital’, we argue the distribution of computing devices creates difficulties for such presuppositions. Instead, we propose thinking these situations through an ‘aesthetic of recruitment’ that is able to accommodate the intensive entanglements and inherent openness of both the social and technical in postdigital play.

Autonomous formation flying: unified control and collision avoidance methods for close manoeuvring spacecraft

The idea of spacecraft formations, flying in tight configurations with maximum baselines of a few hundred meters in low-Earth orbits, has generated widespread interest over the last several years. Nevertheless, controlling the movement of spacecraft in formation poses difficulties, such as in-orbit high-computing demand and collision avoidance capabilities, which escalate as the number of units in the formation is increased and complicated nonlinear effects are imposed to the dynamics, together with uncertainty which may arise from the lack of knowledge of system parameters. These requirements have led to the need of reliable linear and nonlinear controllers in terms of relative and absolute dynamics. The objective of this thesis is, therefore, to introduce new control methods to allow spacecraft in formation, with circular/elliptical reference orbits, to efficiently execute safe autonomous manoeuvres. These controllers distinguish from the bulk of literature in that they merge guidance laws never applied before to spacecraft formation flying and collision avoidance capacities into a single control strategy. For this purpose, three control schemes are presented: linear optimal regulation, linear optimal estimation and adaptive nonlinear control. In general terms, the proposed control approaches command the dynamical performance of one or several followers with respect to a leader to asymptotically track a time-varying nominal trajectory (TVNT), while the threat of collision between the followers is reduced by repelling accelerations obtained from the collision avoidance scheme during the periods of closest proximity. Linear optimal regulation is achieved through a Riccati-based tracking controller. Within this control strategy, the controller provides guidance and tracking toward a desired TVNT, optimizing fuel consumption by Riccati procedure using a non-infinite cost function defined in terms of the desired TVNT, while repelling accelerations generated from the CAS will ensure evasive actions between the elements of the formation. The relative dynamics model, suitable for circular and eccentric low-Earth reference orbits, is based on the Tschauner and Hempel equations, and includes a control input and a nonlinear term corresponding to the CAS repelling accelerations. Linear optimal estimation is built on the forward-in-time separation principle. This controller encompasses two stages: regulation and estimation. The first stage requires the design of a full state feedback controller using the state vector reconstructed by means of the estimator. The second stage requires the design of an additional dynamical system, the estimator, to obtain the states which cannot be measured in order to approximately reconstruct the full state vector. Then, the separation principle states that an observer built for a known input can also be used to estimate the state of the system and to generate the control input. This allows the design of the observer and the feedback independently, by exploiting the advantages of linear quadratic regulator theory, in order to estimate the states of a dynamical system with model and sensor uncertainty. The relative dynamics is described with the linear system used in the previous controller, with a control input and nonlinearities entering via the repelling accelerations from the CAS during collision avoidance events. Moreover, sensor uncertainty is added to the control process by considering carrier-phase differential GPS (CDGPS) velocity measurement error. An adaptive control law capable of delivering superior closed-loop performance when compared to the certainty-equivalence (CE) adaptive controllers is finally presented. A novel noncertainty-equivalence controller based on the Immersion and Invariance paradigm for close-manoeuvring spacecraft formation flying in both circular and elliptical low-Earth reference orbits is introduced. The proposed control scheme achieves stabilization by immersing the plant dynamics into a target dynamical system (or manifold) that captures the desired dynamical behaviour. They key feature of this methodology is the addition of a new term to the classical certainty-equivalence control approach that, in conjunction with the parameter update law, is designed to achieve adaptive stabilization. This parameter has the ultimate task of shaping the manifold into which the adaptive system is immersed. The performance of the controller is proven stable via a Lyapunov-based analysis and Barbalat’s lemma. In order to evaluate the design of the controllers, test cases based on the physical and orbital features of the Prototype Research Instruments and Space Mission Technology Advancement (PRISMA) are implemented, extending the number of elements in the formation into scenarios with reconfigurations and on-orbit position switching in elliptical low-Earth reference orbits. An extensive analysis and comparison of the performance of the controllers in terms of total Δv and fuel consumption, with and without the effects of the CAS, is presented. These results show that the three proposed controllers allow the followers to asymptotically track the desired nominal trajectory and, additionally, those simulations including CAS show an effective decrease of collision risk during the performance of the manoeuvre.

Contribuições da Sociologia para a Análise sobre o Espaço

RESUMO: O espaço tem sido considerado como uma matéria-prima de interesse para uma pluralidade de ciências. A sua abordagem vai da Física à Geometria, da Economia à Sociologia e assume várias e diversas reflexões teóricas sobre as diferentes temáticas de que é detentor. Se nos primórdios da Sociologia não havia um interesse particular sobre o espaço e, em particular, sobre o fenómeno urbano e pelas suas reconfigurações resultantes da Revolução Industrial, não é menos verdade que a influência exercida hoje sobre a Sociologia e os sociólogos foi, e continua a ser exercida, por parte dos autores que estão na base do edifício da teoria sociológica. E essa influência foi a grande responsável pelo desenvolvimento dos saberes específicos de que são detentoras a Sociologia Espacial, Sociologia Urbana e a Sociologia Rural e a atual Sociologia do Território, que para além das teorias produzidas são ainda responsáveis pelos debates em torno de velhas e de novas questões que a Sociologia procura resolver. ABSTRACT: Space has been considered as a raw material of interest to a plurality of sciences. His approach goes from Physics to Geometry, from Economics to Sociology and assumes several and diverse theoretical reflections on the different themes of which he holds. If in the early days of Sociology there was no particular interest in space and in particular in the urban phenomenon and its reconfigurations resulting from the Industrial Revolution, it is no less true that the influence exerted today on sociology and sociologists was, and continues To be exercised, on the part of the authors who are at the base of the building of the sociological theory. And this influence was the great responsibility for the development of the specific knowledge that holds Space Sociology, Urban Sociology and Rural Sociology and the current Sociology of the Territory, which in addition to the theories produced are still responsible for the debates around old and New questions that Sociology seeks to solve.

Italian GenZ Celebrity. Le celebrita teen nella produzione audiovisiva italiana contemporanea: riconfigurazioni, modelli comunicativi, classificazioni.

La ricerca si pone l’obiettivo di comprendere in che modo sia strutturato lo stardom italiano della Generazione Z e quale ruolo svolgano i media nei processi di celebrification delle figure attoriali in esame, nonché l'impatto che queste hanno sulla società stessa. Si intende fornire una maggiore comprensione dei meccanismi alla base del funzionamento dello star system in un contesto storico, culturale e generazionale specifico. Inoltre, il confronto tra il panorama italiano e il landscape internazionale contribuisce a una maggiore comprensione dell’evoluzione e della trasformazione del concetto di celebrità nel contesto globale, oltre che delle modalità attraverso le quali la dimensione italiana si inserisce in questa evoluzione.

Ship performance modelling for least-CO2 emission routes

Decarbonization of maritime transport requires immediate action. In the short term, ship weather routing can provide greenhouse gas emission reductions, even for existing ships and without retrofitting them. Weather routing is based on making optimal use of both envi- ronmental information and knowledge about vessel seakeeping and performance. Combining them at a state-of-the-art level and making use of path planning in realistic conditions can be challenging. To address these topics in an open-source framework, this thesis led to the development of a new module called bateau , and to its combination with the ship routing model VISIR. bateau includes both hull geometry and propulsion modelling for various vessel types. It has two objectives: to predict the sustained speed in a seaway and to estimate the CO2 emission rate during the voyage. Various semi-empirical approaches were used in bateau to predict the ship hydro- and aerodynamical resistance in both head and oblique seas. Assuming that the ship sails at a constant engine load, the involuntary speed loss due to waves was estimated. This thesis also attempted to clarify the role played by the actual representation of the sea state. In particular, the influence of the wave steepness parameter was assessed. For dealing with ships with a greater superstructure, the wind added resistance was also estimated. Numerical experiments via bateau were conducted for both a medium and a large-size container ships, a bulk-carrier, and a tanker. The simulations of optimal routes were carried out for a feeder containership during voyages in the North Indian Ocean and in the South China Sea. Least-CO2 routes were compared to the least-distance ones, assessing the relative CO2 savings. Analysis fields from the Copernicus Marine Service were used in the numerical experiments.