13 resultados para Aerodrome


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This article provides an overview of a novel prototype device that can be used to aid airports in monitoring their landing lighting. Known as Aerodrome Ground Lighting (AGL), the device is comprised of a camera that is capable of capturing images of landing lighting as aircraft approach the airport. AGL is designed to automatically examine landing lighting to assess if it is operating under uniform brightness standards (i.e., luminous intensity of luminares) that aviation governing bodies require. A detailed discussion of the hardware and software requirements of AGL -- currently under joint development by researchers at Queens University Belfast and Cobham Flight Inspection Limited -- is presented. Results from the research indicate that assessing the performance of both ground-based runway luminaries and elevated approach luminaries is possible, though further testing is needed for full validation.

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The Australian Civil Aviation Safety Authority (CASA) currently lists more than 100 separate entities or organisations which maintain a UAS Operator Certificate (UOC) [1]. Approved operations are overwhelmingly a permutation of aerial photography, surveillance, survey or spotting and predominantly, are restricted to Visual Line of Sight (VLOS) operations, below 400 feet, and not within 3 NM of an aerodrome. However, demand is increasing for a Remote Piloted Aerial System (RPAS) regulatory regime which facilitates more expansive operations, in particular unsegregated, Beyond Visual Line of Sight (BVLOS) operations. Despite this demand, there is national and international apprehension regarding the necessary levels of airworthiness and operational regulation required to maintain safety and minimise the risk associated with unsegregated operations. Fundamental to addressing these legitimate concerns will be the mechanisms that underpin safe separation and collision avoidance. Whilst a large body of research has been dedicated to investigating on-board, Sense and Avoid (SAA) technology necessary to meet this challenge, this paper focuses on the contribution of the NAS to separation assurance, and how it will support, as well as complicate RPAS integration. The paper collates and presents key, but historically disparate, threads of Australian RPAS and NAS related information, and distils it with a filter focused on minimising RPAS collision risk. Our ongoing effort is motivated by the need to better understand the separation assurance contribution provided by the NAS layers, in the first instance, and subsequently employ this information to identify scenarios where the coincident collision risk is demonstrably low, providing legitimate substantiation for concessions on equipage and airworthiness standards.

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The development of an automated system for the quality assessment of aerodrome ground lighting (AGL), in accordance with associated standards and recommendations, is presented. The system is composed of an image sensor, placed inside the cockpit of an aircraft to record images of the AGL during a normal descent to an aerodrome. A model-based methodology is used to ascertain the optimum match between a template of the AGL and the actual image data in order to calculate the position and orientation of the camera at the instant the image was acquired. The camera position and orientation data are used along with the pixel grey level for each imaged luminaire, to estimate a value for the luminous intensity of a given luminaire. This can then be compared with the expected brightness for that luminaire to ensure it is operating to the required standards. As such, a metric for the quality of the AGL pattern is determined. Experiments on real image data is presented to demonstrate the application and effectiveness of the system.

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Dissertação para obtenção do grau de Mestre em Engenharia Civil na Área de especialização de Vias de Comunicação e Transportes

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Per garantire la sicurezza di tutte le operazioni in volo (avvicinamento, decollo, holding, ecc..) il decreto legge del 15 marzo del 2006 n. 151 ha imposto la redazione di opportune cartografie basate sul Regolamento ENAC per la Costruzione e l’Esercizio degli Aeroporti e sulla normativa internazionale ICAO così da poterle annettere agli Strumenti Urbanistici del territorio e governare lo sviluppo delle costruzioni. La sicurezza delle operazioni in volo è garantita attraverso delle Superfici di Delimitazione Ostacoli che impongono dei vincoli plano-altimetrici nelle aree limitrofe agli Aeroporti, quindi costruzioni, alberi e lo stesso terreno non devono forare queste superfici altrimenti diventerebbero “Ostacoli” alla navigazione aerea. Per gli ostacoli già presenti sono definiti dei provvedimenti da adottarsi in funzione della superficie che questi forano: potranno essere abbattuti se ricadenti in aree critiche come in prossimità delle piste oppure essere segnalati in mappe in uso ai piloti e anche con segnali visivi posizionati sugli stessi. Per quanto riguarda le future costruzioni, queste non potranno mai diventare Ostacolo in quanto sarà obbligatorio rispettare i vincoli plano-altimetrici. La tesi di laurea in questione vuole illustrare come si è arrivati alla redazione delle sopraccitate mappe nel caso specifico dell'Aeroporto Guglielmo Marconi di Bologna; sono analizzate nel primo capitolo le caratteristiche fisiche degli Aeroporti per acquisire una certa padronanza su termini tecnici che compaiono nei capitoli successivi (è inoltre presente un glossario). Nel secondo capitolo è individuato il percorso normativo che ha portato alla redazione dell’ultima revisione al Codice della Navigazione. Il capitolo 3 introduce le superfici di delimitazione ostacoli secondo quanto esposto nel Regolamento per la Costruzione e l’Esercizio degli Aeroporti di ENAC; il capitolo 4 è dedicato al lay-out dell’Aeroporto Guglielmo Marconi di Bologna. Infine la tesi si conclude con il capitoli 5 nel quale sono esposte le fasi e le metodologie usate per la realizzazione delle planimetrie e con il capitolo 6 in cui si discute delle problematiche sorte a causa dell’orografia del territorio che deve tenersi nella giusta considerazione per la definizione dei suddetti vincoli aeronautici.

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El estudio del comportamiento de la atmósfera ha resultado de especial importancia tanto en el programa SESAR como en NextGen, en los que la gestión actual del tránsito aéreo (ATM) está experimentando una profunda transformación hacia nuevos paradigmas tanto en Europa como en los EE.UU., respectivamente, para el guiado y seguimiento de las aeronaves en la realización de rutas más eficientes y con mayor precisión. La incertidumbre es una característica fundamental de los fenómenos meteorológicos que se transfiere a la separación de las aeronaves, las trayectorias de vuelo libres de conflictos y a la planificación de vuelos. En este sentido, el viento es un factor clave en cuanto a la predicción de la futura posición de la aeronave, por lo que tener un conocimiento más profundo y preciso de campo de viento reducirá las incertidumbres del ATC. El objetivo de esta tesis es el desarrollo de una nueva técnica operativa y útil destinada a proporcionar de forma adecuada y directa el campo de viento atmosférico en tiempo real, basada en datos de a bordo de la aeronave, con el fin de mejorar la predicción de las trayectorias de las aeronaves. Para lograr este objetivo se ha realizado el siguiente trabajo. Se han descrito y analizado los diferentes sistemas de la aeronave que proporcionan las variables necesarias para obtener la velocidad del viento, así como de las capacidades que permiten la presentación de esta información para sus aplicaciones en la gestión del tráfico aéreo. Se ha explorado el uso de aeronaves como los sensores de viento en un área terminal para la estimación del viento en tiempo real con el fin de mejorar la predicción de las trayectorias de aeronaves. Se han desarrollado métodos computacionalmente eficientes para estimar las componentes horizontales de la velocidad del viento a partir de las velocidades de las aeronaves (VGS, VCAS/VTAS), la presión y datos de temperatura. Estos datos de viento se han utilizado para estimar el campo de viento en tiempo real utilizando un sistema de procesamiento de datos a través de un método de mínima varianza. Por último, se ha evaluado la exactitud de este procedimiento para que esta información sea útil para el control del tráfico aéreo. La información inicial proviene de una muestra de datos de Registradores de Datos de Vuelo (FDR) de aviones que aterrizaron en el aeropuerto Madrid-Barajas. Se dispuso de datos de ciertas aeronaves durante un periodo de más de tres meses que se emplearon para calcular el vector viento en cada punto del espacio aéreo. Se utilizó un modelo matemático basado en diferentes métodos de interpolación para obtener los vectores de viento en áreas sin datos disponibles. Se han utilizado tres escenarios concretos para validar dos métodos de interpolación: uno de dos dimensiones que trabaja con ambas componentes horizontales de forma independiente, y otro basado en el uso de una variable compleja que relaciona ambas componentes. Esos métodos se han probado en diferentes escenarios con resultados dispares. Esta metodología se ha aplicado en un prototipo de herramienta en MATLAB © para analizar automáticamente los datos de FDR y determinar el campo vectorial del viento que encuentra la aeronave al volar en el espacio aéreo en estudio. Finalmente se han obtenido las condiciones requeridas y la precisión de los resultados para este modelo. El método desarrollado podría utilizar los datos de los aviones comerciales como inputs utilizando los datos actualmente disponibles y la capacidad computacional, para proporcionárselos a los sistemas ATM donde se podría ejecutar el método propuesto. Estas velocidades del viento calculadas, o bien la velocidad respecto al suelo y la velocidad verdadera, se podrían difundir, por ejemplo, a través del sistema de direccionamiento e informe para comunicaciones de aeronaves (ACARS), mensajes de ADS-B o Modo S. Esta nueva fuente ayudaría a actualizar la información del viento suministrada en los productos aeronáuticos meteorológicos (PAM), informes meteorológicos de aeródromos (AIRMET), e información meteorológica significativa (SIGMET). ABSTRACT The study of the atmosphere behaviour is been of particular importance both in SESAR and NextGen programs, where the current air traffic management (ATM) system is undergoing a profound transformation to the new paradigms both in Europe and the USA, respectively, to guide and track aircraft more precisely on more efficient routes. Uncertainty is a fundamental characteristic of weather phenomena which is transferred to separation assurance, flight path de-confliction and flight planning applications. In this respect, the wind is a key factor regarding the prediction of the future position of the aircraft, so that having a deeper and accurate knowledge of wind field will reduce ATC uncertainties. The purpose of this thesis is to develop a new and operationally useful technique intended to provide adequate and direct real-time atmospheric winds fields based on on-board aircraft data, in order to improve aircraft trajectory prediction. In order to achieve this objective the following work has been accomplished. The different sources in the aircraft systems that provide the variables needed to derivate the wind velocity have been described and analysed, as well as the capabilities which allow presenting this information for air traffic management applications. The use of aircraft as wind sensors in a terminal area for real-time wind estimation in order to improve aircraft trajectory prediction has been explored. Computationally efficient methods have been developed to estimate horizontal wind components from aircraft velocities (VGS, VCAS/VTAS), pressure, and temperature data. These wind data were utilized to estimate a real-time wind field using a data processing approach through a minimum variance method. Finally, the accuracy of this procedure has been evaluated for this information to be useful to air traffic control. The initial information comes from a Flight Data Recorder (FDR) sample of aircraft landing in Madrid-Barajas Airport. Data available for more than three months were exploited in order to derive the wind vector field in each point of the airspace. Mathematical model based on different interpolation methods were used in order to obtain wind vectors in void areas. Three particular scenarios were employed to test two interpolation methods: a two-dimensional one that works with both horizontal components in an independent way, and also a complex variable formulation that links both components. Those methods were tested using various scenarios with dissimilar results. This methodology has been implemented in a prototype tool in MATLAB © in order to automatically analyse FDR and determine the wind vector field that aircraft encounter when flying in the studied airspace. Required conditions and accuracy of the results were derived for this model. The method developed could be fed by commercial aircraft utilizing their currently available data sources and computational capabilities, and providing them to ATM system where the proposed method could be run. Computed wind velocities, or ground and true airspeeds, would then be broadcasted, for example, via the Aircraft Communication Addressing and Reporting System (ACARS), ADS-B out messages, or Mode S. This new source would help updating the wind information furnished in meteorological aeronautical products (PAM), meteorological aerodrome reports (AIRMET), and significant meteorological information (SIGMET).

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Reprinted from Smithsonian reports for 1897, 1900, 1901 and 1904.

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As Servidões Militares Aeronáuticas (SMA) pressupõem restrições que lhes são intrínsecas, suscetíveis de impactar na Economia Real Portuguesa (ERP). Na Força Aérea (FA) as SMA denotam especial importância, em razão das constantes evolução e atualização das Operações Aéreas e tramitação legal imposta, com vista a uma minimização dos encargos restritivos dos bens que, territorialmente, lhes estão associados. Assim, salienta-se a pertinência das SMA enquanto processo que tem reflexos na ERP, uma vez serem utilizadas pela FA no processo de Licenciamento Urbano. Desta feita, foi avaliada a importância das SMA na FA, através de estudo de caso, utilizando um raciocínio hipotético-dedutivo, o qual norteou as entrevistas semiestruturadas, conceptualizadas no respetivo mapa. Estas entrevistas permitiram verificar que: a FA elabora as SMA segundo pressupostos reais e atualizados; a FA emite pareceres positivos relativos aos pedidos de licenciamento que estejam de acordo com o preconizado nos Decreto-Lei das SMA vigentes e nas respetivas áreas territoriais de aplicação; os processos de emissão de pareceres na FA podem ser melhorados concluindo-se, assim, que o processo de conceção das SMA na FA influencia o desenvolvimento da ERP. Abstract: It is assumed that the Aeronautical Control of Obstacles (ACO) imposes certain inner limitations that are susceptible to cause impact on the Portuguese Real Economy (PRE). The ACO area is of special relevance for the Portuguese Air Force (PoAF) due to the permanent evolution and update of the Air Operations and the legal procedures aimed at the decrease of the property limitations associated to them. The ACO is, therefore, of the utmost importance, considering that its process has a significant impact on PRE because of its use by the PoAF within the Building Control process. The scope of this research lies on the importance of the ACO for the PoAF. The research is based on the case study method and the hypothetical-deductive reasoning which set the guidelines for the semi-structured interviews within the conceptual framework, which made possible to verify the PoAF: develops the ACO according to real and updated assumptions; issues positive official assessments to the requests for building licensing that comply with the ACO Legal Decrees within its territorial area of applicability; process of issuing official assessments may be improved, concluding that the development of the ACO within the PoAF influences the development of the PRE.