305 resultados para Gasolio propulsore motore drone velivolo
Resumo:
L’objectif principal de cette thèse de doctorat en composition consiste en la conceptualisation et création d’une oeuvre pour guitare électrique et dispositif électronique se situant à un point de rencontre stylistique entre le free jazz, la musique électro glitch et le drone métal. Le présent texte vise principalement à expliciter la démarche de création de cette oeuvre, intitulée feedback. À la suite du chapitre d'introduction qui décrit l'origine et les objectifs de ce projet de composition, le premier chapitre est consacré à une réflexion sur l'improvisation musicale. En partant d'une description générale de cette pratique et de ses origines, cinq manifestations de l'improvisation qui ont influencé l’oeuvre y sont décrites. Dans le deuxième chapitre est présentée l'hyperguitare qui a été développée pour la pièce ainsi que la description de ses composantes matérielles et logicielles. Dans le troisième chapitre sont décrits le contexte de création, le rôle de l’improvisation dans le processus de création et la description technique des quatre oeuvres composées en amont de feedback. Le quatrième chapitre est dédié à la pièce feedback inspirée de l'œuvre cinématographique et littéraire Fight Club et imprégnée, sur le plan stylistique, de la culture rock, du free jazz et de la musique électroacoustique glitch. En conclusion sont présentés les nouveaux objectifs que ces recherches ont engendrés.
Resumo:
In this brief essay I shall obviously draw from my reflections which I shared over the past three decades and to which I have provided some bibliographical references. It is clear from them that I had several opportunities to share my views beyond the Anglo-Saxon world, and some of them in events organized by K. Koschorke himself in the German academic circles as Munich-Freising Conferences. It is important that we do not get misled by words. We also need clarity of the concepts involved. Koschorke’s emphasis on “ploycentric structures” requires to be discussed and analysed critically to sort out its geographic components and its political-cultural implications, in order to be clear where lie the priorities. Without such exercise we will run the risk of hiding behind the ambiguity of words and concepts. My gut feelings make me believe that “polycentric structures” is just what the West needs in the postcolonial era to replace the control it has lost with decolonization.
Resumo:
Since the terrorist attacks of September 11, 2001, international law has had to grapple with the fundamental challenges that large-scale violence carried out by non-State actors poses to the traditional inter- State orientation of international law. Questions related to the “adequacy” and “effectiveness” of international humanitarian law, international human rights law and the law related to the use of force have been particularly pronounced. This paper focuses on the international humanitarian law implications of American drone attacks in northwest Pakistan. A highly-advanced modality of modern warfare, armed drones highlight the possibilities, problems, prospects and pitfalls of high-tech warfare. How is the battlefield to be defined and delineated geographically and temporally? Who can be targeted, and by whom? Ultimately, this paper concludes that American drone attacks in northwest Pakistan are not unlawful as such under international humanitarian law, though, like any tactical decision in the context of asymmetric warfare, they should be continuously and closely monitored according to the dictates of law with sensitivity to facts on the ground.
Resumo:
Drone strikes are becoming a key feature of the United States’ global military response to nonstate actors, and it has been widely adduced that these strikes have been carried out with the consent of the host states in which such non-state actors reside. This article examines the degree to which assertions of consent (or ‘intervention by invitation’), provided as a justification for drone strikes by the United States in Pakistan, Yemen and Somalia, can be said to accord with international law. First the article provides a broad sketch of the presence of consent in international law. It then analyses in detail the individual elements of consent as provided by Article 20 of the International Law Commission Draft Articles of State Responsibility. These require that consent should be ‘valid’, given by the legitimate government and expressed by an official empowered to do so. These elements will be dealt with individually, and each in turn will be applied to the cases of Pakistan, Yemen and Somalia. Finally, the article will examine the breadth of the exculpatory power of consent, and the extent to which it can preclude the wrongfulness of acts carried out in contravention of international law other than the prohibition of the use of force under Article 2(4) of the Charter of the United Nations.
Resumo:
There is growing concern amongst international lawyers that the United States’ use of unmanned armed vehicles to conduct lethal targeting operations against non-state actors is setting a dangerous precedent for the future and might lead to an erosion of important rules under international law. Taking seriously these concerns, this article examines in more detail the potential precedent created by the US through its lethal drone strikes and the provided justifications, for the purpose of the development of jus ad bellum. In identifying the claims made by the US under different theories of customary international law as qualified practice or expressions of opinio juris that can lead to an alteration of the law should they be accepted by the international community, this article takes a first step towards a more extensive debate on the potential effects of the US drone strikes on the development of international law.
Resumo:
O resultado do jogo entre Corinthians e Palmeiras, neste domingo (31), na Arena Corinthians não chamou tanto a atenção nas redes sociais durante a partida. Em quase 200 mil menções feitas ao clássico paulista as palavras "Guaraní", "drone" e "Valdivia" foram as mais citadas na web.
Resumo:
Bee males (drones) of stingless bees tend to congregate near entrances of conspecific nests, where they wait for virgin queens that initiate their nuptial flight. We observed that the Neotropical solitary wasp Trachypus boharti (Hymenoptera, Cabronidae) specifically preys on males of the stingless bee Scaptotrigona postica (Hymenoptera, Apidae); these wasps captured up to 50 males per day near the entrance of a single hive. Over 90% of the wasp attacks were unsuccessful; such erroneous attacks often involved conspecific wasps and worker bees. After the capture of non-male prey, wasps almost immediately released these individuals unharmed and continued hunting. A simple behavioral experiment showed that at short distances wasps were not specifically attracted to S. postica males nor were they repelled by workers of the same species. Likely, short-range prey detection near the bees' nest is achieved mainly by vision whereas close-range prey recognition is based principally on chemical and/or mechanical cues. We argue that the dependence on the wasp's visual perception during attack and the crowded and dynamic hunting conditions caused wasps to make many preying attempts that failed. Two wasp-density-related factors, wasp-prey distance and wasp-wasp encounters, may account for the fact that the highest male capture and unsuccessful wasp bee encounter rates occurred at intermediate wasp numbers.
Resumo:
We used light and transmission electron microscopy to examine the morphology of the accessory glands of immature and mature adult males of Apis mellifera L. We also made an electrophoretic analysis of the protein content of the mature gland. The glands of the immature male actively secrete a mucous substance that can be seen in the lumen of the gland of the mature male. This secretion stains with mercury bromophenol blue and with periodic acid-Schiff reaction, which stain glyconjugates. The protein content was higher in the lumen secretion than in the gland wall extracts. The electrophoresis patterns of the wall extracts were different from those of the secretion found in the gland lumen.
Resumo:
Durante il periodo di dottorato, l’attività di ricerca di cui mi sono occupato è stata finalizzata allo sviluppo di metodologie per la diagnostica e l’analisi delle prestazioni di un motore automobilistico. Un primo filone di ricerca è relativo allo sviluppo di strategie per l’identificazione delle mancate combustioni (misfires) in un motore a benzina. La sperimentazione si è svolta nella sala prove della Facoltà di Ingegneria dell’Università di Bologna, nei quali è presente un motore Fiat 1.200 Fire, accoppiato ad un freno a correnti parassite, e comandato da una centralina virtuale, creata mediante un modello Simulink, ed interfacciata al motore tramite una scheda di input/output dSpace. Per quanto riguarda la campagna sperimentale, sono stati realizzati delle prove al banco in diverse condizioni di funzionamento (sia stazionarie, che transitorie), durante le quali sono stati indotti dei misfires, sia singoli che multipli. Durante tali test sono stati registrati i segnali provenienti sia dalla ruota fonica usata per il controllo motore (che, nel caso in esame, era affacciata al volano), sia da quella collegata al freno a correnti parassite. Partendo da tali segnali, ed utilizzando un modello torsionale del sistema motoregiunto-freno, è possibile ottenere una stima sia della coppia motrice erogata dal motore, sia della coppia resistente dissipata dal freno. La prontezza di risposta di tali osservatori è tale da garantirci la possibilità di effettuare una diagnosi misfire. In particolare, si è visto che l’indice meglio correlato ala mancata combustione risultaessere la differenza fra la coppia motrice e la coppia resistente; tale indice risulta inoltre essere quello più semplice da calibrare sperimentalmente, in quanto non dipende dalle caratteristiche del giunto, ma solamente dalle inerzie del sistema. Una seconda attività della quale mi sono occupato è relativa alla stima della coppia indicata in un motore diesel automobilistico. A tale scopo, è stata realizzata una campagna sperimentale presso i laboratori della Magneti Marelli Powertrain (Bologna), nella quale sono state effettuati test in molteplici punti motori, sia in condizioni di funzionamento “nominale”, sia variando artificiosamente alcuni dei fattori di controllo (quali Start of Injection, pressione nel rail e, nei punti ove è stato possibile, tasso di EGR e pressione di sovralimentazione), sia effettuando degli sbilanciamenti di combustibile fra un cilindro e l’altro. Utilizzando il solo segnale proveniente da una ruota fonica posta sul lato motore, e sfruttando un modello torsionale simile a quello utilizzato nella campagna di prove relativa alla diagnosi del misfire, è possibile correlare la componente armonica con frequenza di combustione della velocità all’armonica di pari ordine della coppia indicata; una volta stimata tale componente in frequenza, mediante un’analisi di tipo statistico, è possibile eseguire una stima della coppia indicata erogata dal motore. A completamento dell’algoritmo, sfruttando l’analisi delle altre componenti armoniche presenti nel segnale, è possibile avere una stima dello sbilanciamento di coppia fra i vari cilindri. Per la verifica dei risultati ottenuti, sono stati acquisiti i segnali di pressione provenienti da tutti e quattro i cilindri del motore in esame.
Resumo:
This PhD thesis presents the results, achieved at the Aerospace Engineering Department Laboratories of the University of Bologna, concerning the development of a small scale Rotary wing UAVs (RUAVs). In the first part of the work, a mission simulation environment for rotary wing UAVs was developed, as main outcome of the University of Bologna partnership in the CAPECON program (an EU funded research program aimed at studying the UAVs civil applications and economic effectiveness of the potential configuration solutions). The results achieved in cooperation with DLR (German Aerospace Centre) and with an helicopter industrial partners will be described. In the second part of the work, the set-up of a real small scale rotary wing platform was performed. The work was carried out following a series of subsequent logical steps from hardware selection and set-up to final autonomous flight tests. This thesis will focus mainly on the RUAV avionics package set-up, on the onboard software development and final experimental tests. The setup of the electronic package allowed recording of helicopter responses to pilot commands and provided deep insight into the small scale rotorcraft dynamics, facilitating the development of helicopter models and control systems in a Hardware In the Loop (HIL) simulator. A neested PI velocity controller1 was implemented on the onboard computer and autonomous flight tests were performed. Comparison between HIL simulation and experimental results showed good agreement.