1) La descarga del recurso depende de la página de origen
2) Para poder descargar el recurso, es necesario ser usuario registrado en Universia


Opción 1: Descargar recurso

Opción 2: Descargar recurso

Detalles del recurso

Descripción

A methodology and a corresponding set of simulation tools for testing and evaluating turbulence detection sensors has been presented. The tool set is available to industry and the FAA for certification of radar based airborne turbulence detection systems. The tool set consists of simulated data sets representing convectively induced turbulence, an airborne radar simulation system, hazard tables to convert the radar observable to an aircraft load, documentation, a hazard metric "truth" algorithm, and criteria for scoring the predictions. Analysis indicates that flight test data supports spatial buffers for scoring detections. Also, flight data and demonstrations with the tool set suggest the need for a magnitude buffer.

Pertenece a

NASA Technical Reports Server (NTRS)  

Autor(es)

Hamilton, David W. -  Proctor, Fred H. - 

Id.: 69635584

Versión: 1.0

Estado: Final

Tipo:  application/pdf - 

Palabras claveAircraft Design, Testing and Performance - 

Cobertura:  Unclassified, Unlimited, Publicly available - 

Tipo de recurso: NF1676L-2267  -  AIAA Paper 2006-0075  -  AIAA Aerospace Sciences Meeting and Exhibit; 9-12 Jan. 2006; Reno, NV; United States  - 

Tipo de Interactividad: Expositivo

Nivel de Interactividad: muy bajo

Audiencia: Estudiante  -  Profesor  -  Autor  - 

Estructura: Atomic

Coste: no

Copyright: sí

: No Copyright

Formatos:  application/pdf - 

Requerimientos técnicos:  Browser: Any - 

Relación: [IsBasedOn] CASI

Fecha de contribución: 12-feb-2017

Contacto:

Localización:

Otros recursos del mismo autor(es)

  1. Numerical Simulation of HIWC Conditions with the Terminal Area Simulation System Three-dimensional, numerical simulation of a mesoconvective system is conducted in order to better u...
  2. Numerical Study of a Long-Lived, Isolated Wake Vortex in Ground Effect This paper examines a case observed during the 1990 Idaho Falls Test program, in which a wake vortex...
  3. Numerical Simulation of the Aircraft Wake Vortex Flowfield The near wake vortex flowfield from a NACA0012 half-wing was simulated using a fully unstructured Na...
  4. Terminal Area Simulation System User's Guide - Version 10.0 The Terminal Area Simulation System (TASS) is a three-dimensional, time-dependent, large eddy simula...
  5. Review of Idealized Aircraft Wake Vortex Models Properties of three aircraft wake vortex models, Lamb-Oseen, Burnham-Hallock, and Proctor are review...

Otros recursos de la mismacolección

  1. Launch Control System Master Console Event Message Reduction System monitoring and control (SMC) message browsers receive so many messages daily that operators d...
  2. System Testing of Ground Cooling System Components This internship focused primarily upon software unit testing of Ground Cooling System (GCS) componen...
  3. Small Payload Launch Integrated Testing Services (SPLITS) - SPSDL My experience working on the Small Payload Launch Integrated Testing Services project has been both ...
  4. Spaceport Processing System Development Lab The Spaceport Processing System Development Lab (SPSDL), developed and maintained by the Systems Har...
  5. Launch Control System Message Reduction System Monitoring and Control (SMC) message browsers receive many messages daily that operators do n...

Aviso de cookies: Usamos cookies propias y de terceros para mejorar nuestros servicios, para análisis estadístico y para mostrarle publicidad. Si continua navegando consideramos que acepta su uso en los términos establecidos en la Política de cookies.