Search results for "Aerospace"

showing 10 items of 450 documents

Simulación de Plataformas Robóticas de Movimiento para Aplicaciones de Realidad Virtual Mediante Filtros Digitales

2017

[ES] El uso de plataformas robóticas de movimiento en simuladores de vehículos y aplicaciones de Realidad Virtual es relativamente habitual. Sin embargo, el ajuste de los algoritmos que controlan su funcionamiento, denominados algoritmos de washout, no es sencillo y requiere de numerosas pruebas hasta obtener una apropiada fidelidad de movimiento. Disponer de herramientas que permitan simular plataformas de movimiento puede permitir simplificar esta tarea. Es por ello que este trabajo presenta un método para la caracterización y simulación de manipuladores robóticos mediante filtros digitales de segundo orden, sencillo de implementar y ajustar a partir de una caracterización previa. El simu…

0209 industrial biotechnologyEngineeringGeneral Computer Sciencemedia_common.quotation_subjectTiempo reallcsh:Control engineering systems. Automatic machinery (General)Fidelity02 engineering and technologyVirtual realitySimulation systemMotion (physics)Filtros digitalesRealidad virtuallcsh:TJ212-225020901 industrial engineering & automation0203 mechanical engineeringSimulationmedia_commonMotion platforms020301 aerospace & aeronauticsbusiness.industryDigital filtersProcess (computing)Virtual RealityRoboticsReal timeControl and Systems EngineeringbusinessRobóticaSimuladoresSimulationPlataformas de movimientoRevista Iberoamericana de Automática e Informática Industrial RIAI
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Vibration reduction on city buses: Determination of optimal position of engine mounts

2010

International audience; This study is composed of three essential parts. The first part describes an indirect semi-experimental method which is used to reconstruct the excitation force of an operating diesel engine from the acceleration data measured at the mounting points. These internal forces can not be directly measured with force sensors; they have to be derived from the dynamic deformation of the engine support, so a theoretical analysis is carried out to derive the equations for the force re-construction.The second part deals with prevention of low frequency vibration of the powertrain from spreading to the rest of the vehicle. Three uncoupling techniques are used to minimize these v…

0209 industrial biotechnologyEngineeringPowertrainVibration controlAerospace EngineeringMechanical engineering02 engineering and technologylaw.invention[SPI]Engineering Sciences [physics]020901 industrial engineering & automation0203 mechanical engineeringControl theorylawTorqueCivil and Structural EngineeringStiffness matrixCrankshaftbusiness.industryMechanical EngineeringVibrationBusEngineMountCrankshaftComputer Science ApplicationsVibration020303 mechanical engineering & transportsInternal combustion engineControl and Systems EngineeringSignal ProcessingbusinessDecoupling (electronics)
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Flexible integration of robotics, ultrasonics and metrology for the inspection of aerospace components

2016

The performance of modern robotic manipulators has allowed research in recent years, for the development of fast automated non-destructive testing (NDT) of complex geometries. Contemporary robots are well suited for their accuracy and flexibility when adapting to new tasks. Several robotic inspection prototype systems and a number of commercial products have been created around the world. This paper describes the latest progress of a new phase of the research applied to a composite aerospace component of size 1 by 3 metres. A multi robot flexible inspection cell was used to take the fundamental research and the feasibility studies to higher technology readiness levels, all set for future in…

0209 industrial biotechnologyEngineeringTK02 engineering and technologyMetrologyPhased array ultrasonicsSettore ING-IND/14 - Progettazione Meccanica E Costruzione Di Macchine020901 industrial engineering & automationSoftwareData acquisitionUltrasonicsAerospaceSimulationSystem integrationbusiness.industryPayloadInspectionRoboticsControl engineeringRobotics021001 nanoscience & nanotechnologyRobot controlRobotArtificial intelligence0210 nano-technologybusinessAerospace componentsAIP Conference Proceedings
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Multi-band identification for enhancing bearing fault detection in variable speed conditions

2020

Abstract Rolling element bearings are crucial components in rotating machinery, and avoiding unexpected breakdowns using fault detection methods is an increased demand in industry today. Variable speed conditions render a challenge for vibration-based fault diagnosis due to the non-stationary impact frequency. Computed order tracking transforms the vibration signal from time domain to the shaft-angle domain, allowing order analysis with the envelope spectrum. To enhance fault detection, the bearing resonance frequency region is isolated in the raw signal prior to order tracking. Identification of this region is not trivial but may be estimated using kurtosis-based methods reported in the li…

0209 industrial biotechnologyNoise (signal processing)Computer scienceMechanical EngineeringAerospace EngineeringCondition monitoring02 engineering and technologyFault (power engineering)01 natural sciencesNoise floorFault detection and isolationComputer Science Applications020901 industrial engineering & automationControl and Systems Engineering0103 physical sciencesSignal ProcessingCepstrumTime domain010301 acousticsOrder trackingAlgorithmCivil and Structural EngineeringMechanical Systems and Signal Processing
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Clothoid-Based Three-Dimensional Curve for Attitude Planning

2019

Interest in flying robots, also known as unmanned aerial vehicles (UAVs), has grown during last years in both military and civil fields [1, 2]. The same happens to autonomous underwater vehicles (AUVs) [3]. These vehicles, UAVs and AUVs, offer a wide variety of possible applications and challenges, such as control, guidance or navigation [2, 3]. In this sense, heading and attitude control in UAVs is very important [4], particularly relevant in airplanes (fixed-wing flying vehicles), because they are strongly non-linear, coupled, and tend to be underactuated systems with non-holonomic constraints. Hence, designing a good attitude controller is a difficult task [5, 6, 7, 8, 9], where stabilit…

0209 industrial biotechnologyOperations researchFixed-wing planesAutonomous Navigation SystemComputer scienceEnginyeriaAerospace Engineering02 engineering and technologyUnmanned aerial vehicles020901 industrial engineering & automation0203 mechanical engineeringObstacle avoidancemedia_common.cataloged_instanceMotion planningElectrical and Electronic EngineeringEuropean unionmedia_common020301 aerospace & aeronauticsAeronàuticaApplied MathematicsMobile robotVehiclesINGENIERIA DE SISTEMAS Y AUTOMATICAClothoid 3DWork (electrical)Space and Planetary ScienceControl and Systems EngineeringChristian ministryRobotsSmooth path planning
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Buckling and post-buckling analysis of cracked stiffened panels via an X-Ritz method

2019

Abstract A multi-domain eXtended Ritz formulation, called X-Ritz, for the analysis of buckling and post-buckling of stiffened panels with cracks is presented. The theoretical framework is based on the First-order Shear Deformation Theory and accounts for von Karman's geometric nonlinearities. The structure is modeled as assembly of plate elements. Penalty techniques are used to fulfill the continuity condition along the edges of contiguous elements and to satisfy essential boundary conditions requirements. The use of an extended set of approximating functions allows to model through-the-thickness cracks and to capture the crack opening and tip singular fields as well as the structural behav…

0209 industrial biotechnologyPost-bucklingShear deformation theoryStructure (category theory)Aerospace Engineering02 engineering and technology01 natural sciences010305 fluids & plasmasRitz methodSet (abstract data type)020901 industrial engineering & automation0103 physical sciencesStiffened panelBoundary value problemSingle domainSettore ING-IND/04 - Costruzioni E Strutture AerospazialiMathematicsCrackbusiness.industryBucklingThin-walled structureX-Ritz methodStructural engineeringFinite element methodBucklingbusiness
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New results on stability analysis and stabilization of time-delay continuous Markovian jump systems with partially known rates matrix

2015

Summary In this note, the problems of stability analysis and controller synthesis of Markovian jump systems with time-varying delay and partially known transition rates are investigated via an input–output approach. First, the system under consideration is transformed into an interconnected system, and new results on stochastic scaled small-gain condition for stochastic interconnected systems are established, which are crucial for the problems considered in this paper. Based on the system transformation and the stochastic scaled small-gain theorem, stochastic stability of the original system is examined via the stochastic version of the bounded realness of the transformed forward system. Th…

0209 industrial biotechnologyStochastic stabilityMechanical EngineeringGeneral Chemical EngineeringBiomedical EngineeringRegular polygonStability (learning theory)Aerospace Engineering02 engineering and technologyIndustrial and Manufacturing EngineeringMarkovian jumpMatrix (mathematics)020901 industrial engineering & automationControl and Systems EngineeringSystem transformationControl theoryBounded function0202 electrical engineering electronic engineering information engineering020201 artificial intelligence & image processingElectrical and Electronic EngineeringMathematicsInternational Journal of Robust and Nonlinear Control
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Wind component estimation for UAS flying in turbulent air

2019

One of the most important problem of autonomous flight for UAS is the wind identification, especially for small scale vehicles. This research focusses on an identification methodology based on the Extended Kalman Filter (EKF). In particular authors focus their attention on.the filter tuning problem. The proposed procedure requires low computational power, so it is very useful for UAS. Besides it allows a robust wind component identification even when, as it is usually, the measurement data set is affected by noticeable noises. (C) 2019 Elsevier Masson SAS. All rights reserved.

0209 industrial biotechnologyTurbulenceComputer scienceAuto-tuningWind estimationSettore ING-IND/03 - Meccanica Del VoloAerospace EngineeringScale (descriptive set theory)02 engineering and technology01 natural sciences010305 fluids & plasmasPower (physics)Data setExtended Kalman filterIdentification (information)020901 industrial engineering & automationEKFControl theory0103 physical sciencesWind componentUASFocus (optics)Aerospace Science and Technology
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Measurement and Prediction of Centrifugal Compressor Axial Forces During Surge—Part II: Dynamic Surge Model

2017

The force acting on centrifugal compressors is an important parameter to be considered throughout the operating life of these turbomachines. When the compressor is operating in surge conditions, these forces can become highly dangerous for the mechanical and aerodynamic structures. This instability is usually avoided in industrial applications, but the antisurge system may not react in time when emergency shutdowns or power failures take place. During these rapid transients, surge can develop, generating unsteady forces which can harm the close clearance components of the compressor. Therefore, the capability to predict the characteristics and the dynamics of these surge forces would allow …

021103 operations researchFuel TechnologyNuclear Energy and EngineeringMechanical Engineering0211 other engineering and technologies0202 electrical engineering electronic engineering information engineeringEnergy Engineering and Power TechnologyAerospace EngineeringNuclear Energy and Engineering; Fuel Technology; Aerospace Engineering; Energy Engineering and Power Technology; Mechanical Engineering020201 artificial intelligence & image processing02 engineering and technologyNOJournal of Engineering for Gas Turbines and Power
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Survey of Cyber Threats in Air Traffic Control and Aircraft Communications Systems

2018

Air traffic control systems based on the ADS-B standard have been widely adopted in civil aviation to the point that they are now considered the de facto standard. ADS-B provides major benefits to airports and airlines by increasing the safety of air traffic management and control and allowing more flights to travel near busy airports. However, the ADS-B technology lacks sufficient security measures. The ADS-B system is vulnerable and exposed to cyberattacks. We survey the potential known threats and attacks against ADS-B and assess the potential cybersecurity threats to air traffic management and control. The widespread use of ADS-B and the lack of security features in it, i.e., all the AD…

021110 strategic defence & security studies020301 aerospace & aeronauticsComputer sciencebusiness.industryAir traffic managementControl (management)0211 other engineering and technologiesCivil aviationComputerApplications_COMPUTERSINOTHERSYSTEMSJamming02 engineering and technologyAir traffic controlCommunications systemComputer securitycomputer.software_genre0203 mechanical engineeringWirelessbusinesscomputerDe facto standard
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