4,417 research outputs found

    THE NEXT GENERATION OF WILDLAND FIREFIGHTING TOOLS: USING UAV SWARMS FOR FIRE ATTACK

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    Wildland fires pose a direct threat to homeland security because of the severe personal, economic, and social stress they cause to those affected. As unmanned aerial vehicle (UAV) swarms become more ubiquitous in use, they will likely find a place as a frontline firefighting aerial asset, increasing the operational pace of aerial suppression flights and consequently increasing the safety of firefighters. This thesis explored the concept of using UAV swarms as a method for fire attack by comparing theoretical swarms to a conventional aerial asset within a realistic fire scenario and then using a systems engineering approach to define pressure points for implementing UAV swarms in the wildland space. The findings of this research support continued development of UAV swarms and clearly define areas that must be addressed before implementing large-scale UAV swarm flights. The firefighting UAV swarm system shows great promise due to its relative portability and ability to provide an aerial firefighting option to areas without ready access to conventional firefighting aircraft. It will be critical, however, to address logistical and communications constraints of UAV swarm systems before implementation to ensure positive outcomes.Civilian, Portland Fire and RescueApproved for public release. Distribution is unlimited

    Aerospace medicine and biology: A continuing bibliography with indexes, supplement 190, February 1979

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    This bibliography lists 235 reports, articles, and other documents introduced into the NASA scientific and technical information system in January 1979

    Generation and Implementation of Virtual Landscapes for an Augmented Reality HMI-Laboratory

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    Three dimensional visualisation achieves tremendous savings in time and costs during the design process. Due to these circumstances this methods are gaining in importance. For example improvement in performance and the product security or enabling the operative optimization of a production sequence. By the virtual testing it is possible to validate a product in the whole developing process and product lifecycle. The flight simulator ATILa at Airbus Defence and Space in Friedrichshafen uses these advantages for own products. ATILa is used to test intelligent assistance systems for helicopter pilots. Here the graphic implementation of the virtual earth plays a key role when practicing realistical scenarios. This approach is implemented with the Common Database (CDB) which is enabled by the definition of specifications and standards. Different commercial software packages by Presagis are used to implement the aforementioned database. The software Terra Vista is used for the database generation, including the compilation. For the CDB implementation the software Vega Prime is used to prepare the data with the help of the RTP. The software Vega Prime is not able to display 3D models with LODs, due to a software error. Therefore a third software named Creator is used to modify them. The 3D models are available in the OpenFlight Format. This OpenFlight format consists of different kind of nodes with a complex hierarchical structure. Other software solutions, such as Autodesk or Blender, are not able to provide access to the specific structure. The edited models can be integrated in the virtual environment and have to defined by unambiguous indices. Various settings are used to implement the objects automatically. The compilation of the area of interest takes place by the definition of a geotile with a specific size depending on the latitude. The CDB ouput will be transferred by Vega Prime and with the help of the RTP into the simulator. In addition, there is the possibility to render various CDB databases in the simulator to enable a visualisation of the complete earth. Finally, any errors occurring will be described and methods of resolution explained. The complexity of the generation process of a CDB database could be represented with this thesis. However, the whole workflow of the visualisation of the earth is still in its initial stages, since among other things there are errors in the software. To sum up; the potential of the CDB can be evaluated as above average.Die 3D Visualisierung vereinfacht den Planungsprozess und geht somit mit einer Zeit- und Kosten- einsparung einher. Aufgrund dieser Sachverhalte gewinnt sie immer weiter an Bedeutung, um zum Beispiel eine verbesserte und sichere Benutzung eines Produktes oder einen optimierten Betrieb einer Produktionskette zu ermöglichen. Durch vorherige virtuelle Erprobung und Vali- dierung eines Produktes können Kosten für den gesamten Entwicklungsprozess und den Pro- duktlebenszyklus gering gehalten werden. Im Flugsimulator für Helikopter namens ATILa in Friedrichshafen (Airbus Defence and Space) versucht man die genannten Vorteile für die eigenen Produkte zu nutzen. Im ATILa werden Assistenzsysteme geprüft, welche die Helikopterpiloten während ihres Fluges unterstützen sollen. Hierbei spielt die grafische Umsetzung der virtuellen Erde in dem Simulator eine entscheidende Rolle, um die Szenarien realitätsnah durchführen zu können. Dies kann mit Hilfe einer sogenannten Common Database (CDB), die durch Spezi- fikationen und Standards definiert ist, umgesetzt werden. Mittels verschiedener kommerzieller Softwarepakete der Firma Presagis lässt sich die oben genannte Datenbank erstellen. Die Gener- ierung und Kompilierung wird mit dem Softwareprogramm Terra Vista vorgenommen. Die Imple- mentierung der CDB in den Flugsimulator erfolgt mit der Software Vega Prime, welche die Daten über einen RTP zur Verfügung stellt. Da dieses Programm durch einen Softwarefehler nicht in der Lage ist, 3D Modelle mit verschiedenen Detaillierungsgraden darzustellen, muss eine dritte Soft- ware namens Creator genutzt werden. Die 3D Modelle liegen im OpenFlight Format vor. Dieses OpenFlight Format weist eine komplexe hierarchische Struktur aus verschiedenen Knoten auf. Andere Softwarelösungen, wie Autodesk oder Blender, sind nicht in der Lage einen Einblick in die spezielle Struktur zu geben. Die bearbeiteten Modelle können dann in der virtuellen Umgebung eingebunden und müssen durch eindeutige Indizes definiert werden. Verschiedene Einstellun- gen werden genutzt, um Objekte automatisch einzubinden. Die Kompilierung des Interessenge- bietes erfolgt über die Definition einer Geokachel mit einer bestimmten Größe, die abhängig vom Breitengrad ist. Die ausgegebene CDB wird mit Vega Prime und mit Hilfe des RTPs in den Simu- lator übertragen. Des Weiteren gibt es die Möglichkeit verschiedene CDB Datenbanken im Sim- ulator simultan zu rendern, was eine vollständige Visualisierung der kompletten Erde ermöglicht. Abschließend werden aufgetretene Fehler näher beschrieben und Lösungsansätze erläutert. Mit der vorliegenden Arbeit konnte die Komplexität der Entstehung einer CDB Datenbank dargestellt werden. Dennoch befindet sich der gesamte Arbeitsablauf der Visualisierung der Erde noch am Anfang, da u.a. Softwarefehler zu bemängeln sind. Zusammenfassend kann das Potenzial einer CDB als überdurchschnittlich bewertet werden

    How Do Dangerous Goods Regulations Apply to Uncrewed Aerial Vehicles Transporting Medical Cargos?

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    Commercial operations of uncrewed aerial vehicles (UAVs or drones) are expanding, with medical logistics using UAVs as part of health service supply chains being targeted. The ability to transport cargos that include items classified as Dangerous Goods (DG) is a significant factor in enabling UAV logistics to assist medical supply chains, but DG regulations for air transport have developed from the perspective of crewed aircraft and not UAVs. This paper provides an important audit of the current DG regulations, best practice in their application and the development of much-needed new governance that will be required to fully exploit UAVs for the safe transport of DG in medical logistics. Findings from the audit provide a summary of the circumstances and potential challenges resulting from the application of DG regulations as they stand to UAV operations, particularly for medical logistics, and convenient guidance on the practical implications of DG regulations for UAV operators. The main conclusion is that this is an under-researched domain, not yet given full consideration in a holistic way by regulators, governments, industry bodies, practitioners or academia

    High Temperature Electronics Design for Aero Engine Controls and Health Monitoring

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    There is a growing desire to install electronic power and control systems in high temperature harsh environments to improve the accuracy of critical measurements, reduce the amount of cabling and to eliminate cooling systems. Typical target applications include electronics for energy exploration, power generation and control systems. Technical topics presented in this book include:• High temperature electronics market• High temperature devices, materials and assembly processes• Design, manufacture and testing of multi-sensor data acquisition system for aero-engine control• Future applications for high temperature electronicsHigh Temperature Electronics Design for Aero Engine Controls and Health Monitoring contains details of state of the art design and manufacture of electronics targeted towards a high temperature aero-engine application. High Temperature Electronics Design for Aero Engine Controls and Health Monitoring is ideal for design, manufacturing and test personnel in the aerospace and other harsh environment industries as well as academic staff and master/research students in electronics engineering, materials science and aerospace engineering

    NASA/FAA helicopter simulator workshop

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    A workshop was convened by the FAA and NASA for the purpose of providing a forum at which leading designers, manufacturers, and users of helicopter simulators could initiate and participate in a development process that would facilitate the formulation of qualification standards by the regulatory agency. Formal papers were presented, special topics were discussed in breakout sessions, and a draft FAA advisory circular defining specifications for helicopter simulators was presented and discussed. A working group of volunteers was formed to work with the National Simulator Program Office to develop a final version of the circular. The workshop attracted 90 individuals from a constituency of simulator manufacturers, training organizations, the military, civil regulators, research scientists, and five foreign countries

    U.S. Law of the Sea Cruise to Map the Foot of the Slope and 2500-m Isobath of the U.S. Arctic Ocean Margin

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    U.S. Law of the Sea cruise to map the foot of the slope and 2500-m isobath of the US Arctic Ocean margin CRUISE HEALY 1102 August 15 to September 28, 2011 Barrow, AK to Dutch Harbor, A

    U.S. Law of the Sea Cruise to Map and Sample the US Arctic Ocean Margin

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    U.S. Law of the Sea cruise to map and sample the US Arctic Ocean margin CRUISE HEALY 1202 August 25 to September 27, 2012 Barrow, AK to Dutch Harbor, A

    Bewertung des Rekuperatorpotenzials eines 300-kW-Turbowellen-Hubschraubermotors

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    In this thesis, an integrated rotorcraft multidisciplinary simulation framework has been developed to comprehensively evaluate the potential of the rotorcraft adopting a recuperator under various flight conditions as well as at mission levels. Through the execution of multi-objective genetic algorithm (GA) optimization, the Pareto front model is derived qualifying the associated interdependency and trade-off between the fuel saving potential and recuperator weight penalty. The proposed methodology proves to be a computationally efficient tool for the multidisciplinary design and optimization of the recuperated rotorcraft powerplant system.In dieser Arbeit wurde ein integriertes multidisziplinäres Simulationssystem für Drehflügler entwickelt, um das Potenzial des Drehflüglers für den Einsatz eines Rekuperators unter verschiedenen Flugbedingungen sowie auf Missionsebene umfassend zu bewerten. Durch die Ausführung einer Optimierung mit einem genetischen Algorithmus mit mehreren Zielsetzungen (GA) wird das Pareto-Frontmodell abgeleitet, das die damit verbundene Abhängigkeit und den Kompromiss zwischen dem Kraftstoffeinsparpotenzial und der Gewichtsstrafe für den Rekuperator qualifiziert. Die vorgeschlagene Methodik erweist sich als rechnerisch effizientes Werkzeug für die multidisziplinäre Auslegung und Optimierung eines derart modifizierten Triebwerkssystems für Drehflügler
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