Robustness Study of a Dynamic Inversion Control Law for a High Performance Aircraft

In the design of °ight control system modeling uncertainties in the form of param-eter variations is one of the major problems. It is even more critical for high performance aircrafts,since such aircrafts are purposefully designed unstable to enhance their performance (especially ma-neuverability). Hence the °ight control system needs to be quite e®ective in both assuring accurate tracking of pilot commands, while simultaneously assuring overall stability of the aircraft. In addi-tion, the control system must also be su±ciently robust to cater for possible parameter variations and inaccuracies . The primary aim of this paper is to carry out a robustness study of a dynamic inversion based nonlinear control design for a high performance aircraft, which has been developed recently [1].

Ultrasonic performance of the PVDF thin film sensors under thermal fatigue

In the present work, the ultrasonic strain sensing performance of the large area PVDF thin film subjected to the thermal fatigue is studied. The PVDF thin film is prepared using hot press and the piezoelectric phase (beta-phase) has been achieved by thermo-mechanical treatment and poling under DC field. The sensors used in aircrafts for structural health monitoring applications are likely to be subjected to a wide range of temperature fluctuations which may create thermal fatigue in both aircraft structures and in the sensors. Thus, the sensitivity of the PVDF sensors for thermal fatigue needs to be studied for its effective implementation in the structural health monitoring applications. In present work, the fabricated films have been subjected to certain number of thermal cycles which serve as thermal fatigue and are further tested for ultrasonic strain sensitivity at various different frequencies. The PVDF sensor is bonded on the beam specimen at one end and the ultrasonic guided waves are launched with a piezoelectric wafer bonded on another end of the beam. Sensitivity of PVDF sensor in terms of voltage is obtained for increasing number of thermal cycles. Sensitivity variation is studied at various different extent of thermal fatigue. The variation of the sensor sensitivity with frequency due to thermal fatigue at different temperatures is also investigated. The present investigation shows an appropriate temperature range for the application of the PVDF sensors in structural health monitoring.

Vibration spectrum analyzer using stretched membranes of polymer piezoelectrics for sensor networks

The key problem tackled in this paper is the development of a stand-alone self-powered sensor to directly sense the spectrum of mechanical vibrations. Such a sensor could be deployed in wide area sensor networks to monitor structural vibrations of large machines (e. g. aircrafts) and initiate corrective action if the structure approaches resonance. In this paper, we study the feasibility of using stretched membranes of polymer piezoelectric polyvinlidene fluoride for low-frequency vibration spectrum sensing. We design and evaluate a low-frequency vibration spectrum sensor that accepts an incoming vibration and directly provides the spectrum of the vibration as the output.

COMPUTATIONAL MODELING OF A MULTI-LAYERED PIEZO-COMPOSITE BEAM MADE UP OF MFC

The Variational Asymptotic Method (VAM) is used for modeling a coupled non-linear electromechanical problem finding applications in aircrafts and Micro Aerial Vehicle (MAV) development. VAM coupled with geometrically exact kinematics forms a powerful tool for analyzing a complex nonlinear phenomena as shown previously by many in the literature 3 - 7] for various challenging problems like modeling of an initially twisted helicopter rotor blades, matrix crack propagation in a composite, modeling of hyper elastic plates and various multi-physics problems. The problem consists of design and analysis of a piezocomposite laminate applied with electrical voltage(s) which can induce direct and planar distributed shear stresses and strains in the structure. The deformations are large and conventional beam theories are inappropriate for the analysis. The behavior of an elastic body is completely understood by its energy. This energy must be integrated over the cross-sectional area to obtain the 1-D behavior as is typical in a beam analysis. VAM can be used efficiently to approximate 3-D strain energy as closely as possible. To perform this simplification, VAM makes use of thickness to width, width to length, width multiplied by initial twist and strain as small parameters embedded in the problem definition and provides a way to approach the exact solution asymptotically. In this work, above mentioned electromechanical problem is modeled using VAM which breaks down the 3-D elasticity problem into two parts, namely a 2-D non-linear cross-sectional analysis and a 1-D non-linear analysis, along the reference curve. The recovery relations obtained as a by-product in the cross-sectional analysis earlier are used to obtain 3-D stresses, displacements and velocity contours. The piezo-composite laminate which is chosen for an initial phase of computational modeling is made up of commercially available Macro Fiber Composites (MFCs) stacked together in an arbitrary lay-up and applied with electrical voltages for actuation. The expressions of sectional forces and moments as obtained from cross-sectional analysis in closed-form show the electro-mechanical coupling and relative contribution of electric field in individual layers of the piezo-composite laminate. The spatial and temporal constitutive law as obtained from the cross-sectional analysis are substituted into 1-D fully intrinsic, geometrically exact equilibrium equations of motion and 1-D intrinsic kinematical equations to solve for all 1-D generalized variables as function of time and an along the reference curve co-ordinate, x(1).

基于SPC的电源故障预测系统研究

本文结合飞行器电源系统故障维护特点,利用统计过程控制理论,从数理统计的角度对电源系统测试数据进行分析,设计了电源故障预测系统。文中阐述了系统的工作原理和利用LabView软件的实现过程。实验结果表明此预测系统可以发现故障征兆及时维护,提高系统安全性。最后阐述了进一步研究可能会遇到的问题。

HTS Motors in Aircraft Propulsion: Design Considerations

Current high temperature superconducting (HTS) wires exhibit high current densities enabling their use in electrical rotating machinery. The possibility of designing high power density superconducting motors operating at reasonable temperatures allows for new applications in mobile systems in which size and weight represent key design parameters. Thus, all-electric aircrafts represent a promising application for HTS motors. The design of such a complex system as an aircraft consists of a multi-variable optimization that requires computer models and advanced design procedures. This paper presents a specific sizing model of superconducting propulsion motors to be used in aircraft design. The model also takes into account the cooling system. The requirements for this application are presented in terms of power and dynamics as well as a load profile corresponding to a typical mission. We discuss the design implications of using a superconducting motor on an aircraft as well as the integration of the electrical propulsion in the aircraft, and the scaling laws derived from physics-based modeling of HTS motors.

Active corrosion protection of AA2024 by sol-gel coatings with corrosion inhibitors

A indústria aeronáutica utiliza ligas de alumínio de alta resistência para o fabrico dos elementos estruturais dos aviões. As ligas usadas possuem excelentes propriedades mecânicas mas apresentam simultaneamente uma grande tendência para a corrosão. Por esta razão essas ligas necessitam de protecção anticorrosiva eficaz para poderem ser utilizadas com segurança. Até à data, os sistemas anticorrosivos mais eficazes para ligas de alumínio contêm crómio hexavalente na sua composição, sejam pré-tratamentos, camadas de conversão ou pigmentos anticorrosivos. O reconhecimento dos efeitos carcinogénicos do crómio hexavalente levou ao aparecimento de legislação banindo o uso desta forma de crómio pela indústria. Esta decisão trouxe a necessidade de encontrar alternativas ambientalmente inócuas mas igualmente eficazes. O principal objectivo do presente trabalho é o desenvolvimento de prétratamentos anticorrosivos activos para a liga de alumínio 2024, baseados em revestimentos híbridos produzidos pelo método sol-gel. Estes revestimentos deverão possuir boa aderência ao substrato metálico, boas propriedades barreira e capacidade anticorrosiva activa. A protecção activa pode ser alcançada através da incorporação de inibidores anticorrosivos no prétratamento. O objectivo foi atingido através de uma sucessão de etapas. Primeiro investigou-se em detalhe a corrosão localizada (por picada) da liga de alumínio 2024. Os resultados obtidos permitiram uma melhor compreensão da susceptibilidade desta liga a processos de corrosão localizada. Estudaram-se também vários possíveis inibidores de corrosão usando técnicas electroquímicas e microestruturais. Numa segunda etapa desenvolveram-se revestimentos anticorrosivos híbridos orgânico-inorgânico baseados no método sol-gel. Compostos derivados de titania e zirconia foram combinados com siloxanos organofuncionais a fim de obter-se boa aderência entre o revestimento e o substrato metálico assim como boas propriedades barreira. Testes industriais mostraram que estes novos revestimentos são compatíveis com os esquemas de pintura convencionais actualmente em uso. A estabilidade e o prazo de validade das formulações foram optimizados modificando a temperatura de armazenamento e a quantidade de água usada durante a síntese. As formulações sol-gel foram dopadas com os inibidores seleccionados durante a primeira etapa e as propriedades anticorrosivas passivas e activas dos revestimentos obtidos foram estudadas numa terceira etapa do trabalho. Os resultados comprovam a influência dos inibidores nas propriedades anticorrosivas dos revestimentos sol-gel. Em alguns casos a acção activa dos inibidores combinou-se com a protecção passiva dada pelo revestimento mas noutros casos terá ocorrido interacção química entre o inibidor e a matriz de sol-gel, de onde resultou a perda de propriedades protectoras do sistema combinado. Atendendo aos problemas provocados pela adição directa dos inibidores na formulação sol-gel procurou-se, numa quarta etapa, formas alternativas de incorporação. Na primeira, produziu-se uma camada de titania nanoporosa na superfície da liga metálica que serviu de reservatório para os inibidores. O revestimento sol-gel foi aplicado por cima da camada nanoporosa. Os inibidores armazenados nos poros actuam quando o substrato fica exposto ao ambiente agressivo. Numa segunda, os inibidores foram armazenados em nano-reservatórios de sílica ou em nanoargilas (halloysite), os quais foram revestidos por polielectrólitos montados camada a camada. A terceira alternativa consistiu no uso de nano-fios de molibdato de cério amorfo como inibidores anticorrosivos nanoparticulados. Os nano-reservatórios foram incorporados durante a síntese do sol-gel. Qualquer das abordagens permitiu eliminar o efeito negativo do inibidor sobre a estabilidade da matriz do sol-gel. Os revestimentos sol-gel desenvolvidos neste trabalho apresentaram protecção anticorrosiva activa e capacidade de auto-reparação. Os resultados obtidos mostraram o elevado potencial destes revestimentos para a protecção anticorrosiva da liga de alumínio 2024.

Fleet Industries records, 1948, 1983-1989

The Fleet Aircraft of Canada Ltd. Company was founded in 1930 by Reuben Hollis Fleet in Fort Erie, Ontario. Within the first decade of operations, the company had gained an international reputation for excellence. With the outbreak of war in 1939, Fleet focused all of its efforts in the design and production of various training aircraft for the Royal Canadian Air Force and the refurbishment of British and Canadian fighter planes. Fleet ceased production of aircrafts in 1957 and was renamed Fleet Aerospace, a division of Magellan Aerospace. The manufacturing location in Fort Erie was known as Fleet Industries. Currently, the company is a Canadian Aerospace Sub-contractor that manufactures aerospace structures, component parts, and assemblies to approved design data. Fleet’s customers include Boeing, Bombardier, Viking Air and Erickson Air-Crane. In 2006, the Company became privately owned when 16 minority stakeholders took over operations. The Company was renamed Fleet Canada Inc.

De la réforme et de l'harmonisation du droit des sûretés dans un contexte de mondialisation de l'économie : vers un retour au paradigme de l'uniformisation du droit?

La réforme et l’harmonisation du droit des sûretés mobilières sont à l’ordre du jour de plusieurs organisations internationales, car il est admis qu’un régime de sûretés efficient favorise l’accès au crédit à de faibles coûts. L’harmonisation de ce droit comporte deux volets. D’une part, dans l’Occident industrialisé, les efforts d’harmonisation vont de la réforme des droits internes à l’établissement de régimes spéciaux relativement à des biens spécifiques (principalement les biens mobiles de grande valeur, tels les aéronefs, le matériel ferroviaire roulant et les satellites, et les biens incorporels, comprenant les créances, valeurs mobilières, actifs financiers et titres intermédiés). Ces efforts d’harmonisation démontrent que d’un point de vue systémique, malgré quelques différences notables, les régimes nord-américains et européens sont fondés sur des principes similaires et atteignent des résultats comparables. En résulte l’émergence d’un ordre juridique transnational en droit des sûretés mobilières, fondé sur les principes de la primauté de l’individu et la reconnaissance du droit de propriété de l’individu dans ses biens, mis en œuvre grâce à l’État de droit. D’autre part, les institutions financières internationales encouragent l’établissement de régimes de sûretés dans les pays en voie de développement qui obéissent aux mêmes critères que ceux de l’Occident, en insistant sur les réformes institutionnelles et juridiques visant l’établissement d’une bonne gouvernance et l’État de droit. Cependant, une transposition des régimes occidentaux ne peut se faire sans heurts dans les pays en voie de développement, notamment pour des raisons socio-culturelles et politiques. Lorsque les principes de la primauté de l’individu, de la propriété individuelle et de l’État de droit ne sont pas reconnus dans un pays donné, la réforme et l’harmonisation du droit des sûretés s’en trouvent compromis. La démonstration de l’état d’avancement de la réforme et de l’harmonisation du droit des sûretés dans les pays occidentaux industrialisés est faite grâce à une comparaison du Uniform Commercial Code, du Code civil du Québec, des Personal Property Security Acts des provinces canadiennes de common law, des principes des droits français et anglais, de l’influence du droit communautaire sur les pays membres de l’Union Européenne. Sont analysés, aussi, dans cette optique, les principaux instruments de l’harmonisation du droit émanant des organisations internationales. Par ailleurs, deux études de cas relatifs à la réforme du crédit foncier en Égypte et à la réforme de l’urbanisme et de l’habitat en République démocratique du Congo, viennent étayer les difficultés que rencontrent les institutions internationales, telles la Banque mondiale et l’ACDI, dans le cadre de projets de réformes visant la bonne gouvernance et l’instauration d’un véritable État de droit, en partie à cause d’un pluralisme des ordres juridiques de ces pays.

Impact of Self-generation of Priorities and Non-preemptive Service in Single/Multiserver Queues

In this thesis we have studied a few models involving self-generation of priorities. Priority queues have been extensively discussed in literature. However, these are situations involving priority assigned to (or possessed by) customers at the time of their arrival. Nevertheless, customers generating into priority is a common phenomena. Such situations especially arise at a physicians clinic, aircrafts hovering over airport running out of fuel but waiting for clearance to land and in several communication systems. Quantification of these are very little seen in literature except for those cited in some of the work indicated in the introduction. Our attempt is to quantify a few of such problems. In doing so, we have also generalized the classical priority queues by introducing priority generation ( going to higher priorities and during waiting). Systematically we have proceeded from single server queue to multi server queue. We also introduced customers with repeated attempts (retrial) generating priorities. All models that were analyzed in this thesis involve nonpreemptive service. Since the models are not analytically tractable, a large number of numerical illustrations were produced in each chapter to get a feel about the working of the systems.

Die aeroelastische Stabilitätsanalyse – ein praxisnaher Ansatz zur intervalltheoretischen Betrachtung von Modellierungsunsicherheiten am Flugzeug

Die Untersuchung des dynamischen aeroelastischen Stabilitätsverhaltens von Flugzeugen erfordert sehr komplexe Rechenmodelle, welche die wesentlichen elastomechanischen und instationären aerodynamischen Eigenschaften der Konstruktion wiedergeben sollen. Bei der Modellbildung müssen einerseits Vereinfachungen und Idealisierungen im Rahmen der Anwendung der Finite Elemente Methode und der aerodynamischen Theorie vorgenommen werden, deren Auswirkungen auf das Simulationsergebnis zu bewerten sind. Andererseits können die strukturdynamischen Kenngrößen durch den Standschwingungsversuch identifiziert werden, wobei die Ergebnisse Messungenauigkeiten enthalten. Für eine robuste Flatteruntersuchung müssen die identifizierten Unwägbarkeiten in allen Prozessschritten über die Festlegung von unteren und oberen Schranken konservativ ermittelt werden, um für alle Flugzustände eine ausreichende Flatterstabilität sicherzustellen. Zu diesem Zweck wird in der vorliegenden Arbeit ein Rechenverfahren entwickelt, welches die klassische Flatteranalyse mit den Methoden der Fuzzy- und Intervallarithmetik verbindet. Dabei werden die Flatterbewegungsgleichungen als parameterabhängiges nichtlineares Eigenwertproblem formuliert. Die Änderung der komplexen Eigenlösung infolge eines veränderlichen Einflussparameters wird mit der Methode der numerischen Fortsetzung ausgehend von der nominalen Startlösung verfolgt. Ein modifizierter Newton-Iterations-Algorithmus kommt zur Anwendung. Als Ergebnis liegen die berechneten aeroelastischen Dämpfungs- und Frequenzverläufe in Abhängigkeit von der Fluggeschwindigkeit mit Unschärfebändern vor.

Air cargo economics

Air Cargo Economics - Outline - Air cargo participants - Air cargo pricing, rates & yields - Cargo related costs - Freighter aircraft operating costs - Methods of cost allocation - Pax/combi vs freighter services - Lufthansa’s cargo strategy - Quick change aircraft - Aircraft wet leasing - Conclusions

Peroxy radical partitioning during the AMMA radical intercomparison exercise

Peroxy radicals were measured onboard two scientific aircrafts during the AMMA (African Monsoon Multidisciplinary Analysis) campaign in summer 2006. This paper reports results from the flight on 16 August 2006 during which measurements of HO2 by laser induced fluorescence spectroscopy at low pressure (LIF-FAGE) and total peroxy radicals (RO2* = HO2+ΣRO2, R = organic chain) by two similar instruments based on the peroxy radical chemical amplification (PeRCA) technique were subject of a blind intercomparison. The German DLR-Falcon and the British FAAM-BAe-146 flew wing tip to wing tip for about 30 min making concurrent measurements on 2 horizontal level runs at 697 and 485 hPa over the same geographical area in Burkina Faso. A full set of supporting measurements comprising photolysis frequencies, and relevant trace gases like CO, NO, NO2, NOy, O3 and a wider range of VOCs were collected simultaneously. Results are discussed on the basis of the characteristics and limitations of the different instruments used. Generally, no data bias are identified and the RO2* data available agree quite reasonably within the instrumental errors. The [RO2*]/[HO2] ratios, which vary between 1:1 and 3:1, as well as the peroxy radical variability, concur with variations in photolysis rates and in other potential radical precursors. Model results provide additional information about dominant radical formation and loss processes.

Contratos relacionais na indústria aeronáutica brasileira : um estudo empírico do modelo de parcerias de risco da Embraer

O presente trabalho é um estudo empírico das práticas contratuais adotadas pela EMBRAER posteriormente ao seu processo de privatização em 1994, e do arranjo contratual empregado para viabilizar a realização dos projetos de aeronaves responsáveis pelo ressurgimento da empresa ao final da década 1990. Aspecto fundamental da engenharia contratual empreendida foi a formação das chamadas Parcerias de Risco entre a Embraer e um grupo selecionado de fornecedores-chave visando o co-desenvolvimento das aeronaves. A análise das informações obtidas na pesquisa aponta a importância epistemológica de se utilizar novos instrumentos de análise que permitam compreender melhor as práticas contratuais empregadas e seu papel no desenvolvimento. Assim, utilizamos a teoria relacional dos contratos como lente teórica para analisar o modelo de parcerias de risco e, por meio dela, investigar qual o papel exercido pelos elementos relacionais no sucesso dos programas ERJ 145 e EMBRAER 170/190. A hipótese central que norteia o trabalho é a de que, no inovador arranjo contratual que envolveu a Embraer, fornecedores estrangeiros e o BNDES, a relação contratual foi construída por meio de mecanismos promissórios e não-promissórios de projeção de trocas, e os padrões de normatividade estabelecidos entre as partes transcenderam o contrato escrito. A contribuição da teoria relacional dos contratos para a análise de tais práticas possui duplo caráter. A primeiro contribuição é eminentemente descritiva, ao fornecer um instrumental teórico mais abrangente e poderoso para compreender a real dinâmica das práticas contratuais em análise. A segunda contribuição, de natureza normativa, consiste em explicitar aspectos relacionais que compõem, juntamente com os elementos promissórios, uma certa normatividade interna ao contrato que informa a conduta dos agentes ao longo da relação. Nos programas ERJ 145 e EMBRAER 170/90, procuramos demonstrar como a formulação de um arranjo contratual mais relacional em substituição ao tradicional conjunto de relações contratuais de fornecimento descontínuas, foi fundamental para o sucesso dos projetos e até mesmo para a sua própria viabilização. Nesse sentido, a teoria relacional dos contratos fornece categorias de análise que não apenas oferecem um ferramental teórico mais adequado para descrever relações como a do caso em estudo, mas também fornece, por meio de uma descrição mais rica e abrangente, lições sobre como desenhar contratos. Isto é importante para demonstrar como a problemática das dimensões implícitas do contratos transcende o campo da teoria contratual e da justiça contratual e apresenta-se de grande relevância para a agenda de pesquisa em Direito e Desenvolvimento.

Sistema híbrido para detecção e diagnóstico de falhas em sistemas dinâmicos

The industries are getting more and more rigorous, when security is in question, no matter is to avoid financial damages due to accidents and low productivity, or when it s related to the environment protection. It was thinking about great world accidents around the world involving aircrafts and industrial process (nuclear, petrochemical and so on) that we decided to invest in systems that could detect fault and diagnosis (FDD) them. The FDD systems can avoid eventual fault helping man on the maintenance and exchange of defective equipments. Nowadays, the issues that involve detection, isolation, diagnose and the controlling of tolerance fault are gathering strength in the academic and industrial environment. It is based on this fact, in this work, we discuss the importance of techniques that can assist in the development of systems for Fault Detection and Diagnosis (FDD) and propose a hybrid method for FDD in dynamic systems. We present a brief history to contextualize the techniques used in working environments. The detection of fault in the proposed system is based on state observers in conjunction with other statistical techniques. The principal idea is to use the observer himself, in addition to serving as an analytical redundancy, in allowing the creation of a residue. This residue is used in FDD. A signature database assists in the identification of system faults, which based on the signatures derived from trend analysis of the residue signal and its difference, performs the classification of the faults based purely on a decision tree. This FDD system is tested and validated in two plants: a simulated plant with coupled tanks and didactic plant with industrial instrumentation. All collected results of those tests will be discussed