1,908 research outputs found
System for monitoring and controlling unit operations that include distillation
Fluid sensor methods and systems adapted for monitoring and/or controlling distillation operations in fluidic systems, such as bath distillation operations or continuous distillation operations, are disclosed. Preferred embodiments are directed to process monitoring and/or process control for unit operations involving endpoint determination of a distillation, for example, as applied to a liquid-component-switching operation (e.g., a solvent switehing operation), a liquid-liquid separation operation, a solute concentration operation, a dispersed- phase concentration operation, among others
Systems and methods for monitoring solids using mechanical resonator
Multi-phase system monitoringmethods, systems and apparatus aredisclosed. Preferred embodiments comprise one or more mechanical resonator sensing elements. In preferred embodiments a sensor or a sensor subassembly is ported to a fluidized bed vessel such as a fluidized bed polymerization reactor
Digest of Russian Space Life Sciences, issue 33
This is the thirty-third issue of NASA's USSR Space Life Sciences Digest. It contains abstracts of 55 papers published in Russian journals. The abstracts in this issue have been identified as relevant to the following areas of space biology and medicine: biological rhythms, body fluids, botany, cardiovascular and respiratory systems, developmental biology, endocrinology, equipment and instrumentation, gastrointestinal system, genetics, hematology, human performance, metabolism, microbiology, musculoskeletal system, neurophysiology, nutrition, operational medicine, psychology, radiobiology, and reproductive system
Pioneer Venus large probe neutral mass spectrometer
The deuterium hydrogen abundance ratio in the Venus atmosphere was measured while the inlets to the Pioneer Venus large probe mass spectrometer were coated with sulfuric acid from Venus' clouds. The ratio is (1.6 + or - 0.2) x 10 to the minus two power. It was found that the 100 fold enrichment of deuterium means that Venus outgassed at least 0.3% of a terrestrial ocean and possibly more
The development of a novel on-line system for the monitoring and control of fermentation processes
A thesis submitted to the University of Luton for the degree of Doctor of PhilosophyThis thesis describes the development of a computer controlled on-line system for fermentation monitoring and control. The entire system consists of a laboratory fermenter, flow injection system (four channels), a newly designed on-line filter, biomass analysis channel, pH and oxygen controllers as well as a spectrophotometer. A new design of gas driven flow injection analysis (FIA) allows a large number of reagents to be handled. The computer-controlled four channel PIA system is well suited for sequential analysis, which is important for fermentation on-line mOnitoring. The system can change the wavelength of the spectrophotometer automatically for each PIA channel, which makes the system powerful and flexible. A high frequency, low energy ultrasonic filter was modified and applied to the system for on-line mammalian cell culture sampling without breaking the sterile barrier. The results show that this novel application of ultrasonic filter technology results in higher efficiency and reliability and a longer life cycle than other types of filter. All the operations of the analytical system are controlled by a Macintosh computer (Quadra 950). The control program was written in LabVIEW which is a graphical programming language and well applicable to fermentation control. The software communicates with detectors, data acquisition, data analysis and presentation. The system can programmatically control up to 50 devices. Mammalian cell batch culture was used as an example of the application of the system. The system consists of a laboratory fermenter with a continuous sample withdrawal filter and an analysis system where glucose, lactate and ammonia, lactate dehydrogenase and biomass were measured. Cell viability was estimated by microscopic assay with trypan blue. pH and Oxygen were also measured. The system response was fast and yields a large number of reliable and precise analytical results which can be of great importance in the monitoring and control of mammalian cell culture conditions
Aerospace medicine and biology: A continuing bibliography with indexes (supplement 335)
This bibliography lists 143 reports, articles and other documents introduced into the NASA Scientific and Technical Information System during March, 1990. Subject coverage includes: aerospace medicine and psychology, life support systems and controlled environments, safety equipment, exobiology and extraterrestrial life, and flight crew behavior and performance
Application of chemical kinetic modeling to improve design and performance criteria for a practical incineration system
In this study, detailed thermo-chemical kinetics with networked ideal reactor model were applied to simulate a practical combustion system -the Secondary Combustion Chamber (SCC) of the Rotary Kiln incineration Simulator (RKIS) at the EPA facility at Research Triangle Park, NC. The networked ideal model was developed using analysis of reactor geometry, temperature profile measurements, and SO2 tracer data provided by EPA. A computer simulation of the networked model was developed using the CHEMKIN H library. A parallel effort considered the effects of non-ideal mixing on detailed thermo-kinetic, simulations. Specifically, an alternate approach was developed to solve the Partially Stirred Reactor (PaSR) model that allowed the incorporation of large detailed mechanisms. Both ideal and non-ideal modeling approaches were compared with experimental data gathered on a Toroidal Jet Stirred Combustor (TJSQ and the SCC at EPA. SCC experiments measured Product of Incomplete Combustion (PIC) formation of surrogate chlorinated wastes (CCl4 and CH2Cl2)lwhile the TSJC experiments measured PIC formation in ethylene/air combustion for fuel-lean conditions near blowout and fuel-rich conditions.
Analysis of the geometry and temperature profiles of the SCC suggested the existence of up to four distinct mixing zones. The RTDs, which were resolved from the tracer studies, further supported a multiple PSR model. A model was chosen based on the best fit to SO2, tracer data and consistency with physical geometry, resulting flow patterns, and temperature measurements. A thermo-kinetic mechanism developed by Chiang (1995) was applied to the model. The model results did not agree well with the experimental data. However, it followed many of the underlying trends revealed by the data. Sensitivity analysis of the parameters was used to further explore trends and recommend potential design improvements to reduce PIC formation.
An alternate solution technique was developed for the PaSR which approximated mean conditions and solved the deterministic model to refme the approximation and eventually converge on a solution. The approximation, direct integration, and convergence technique compared favorably with the published Monte Carlo modeling calculations, but used, on average, less than 1/200th of the CPU time. This new technique allowed use of considerably larger detailed mechanisms. Additionally, a generalized PaSR model was proposed to account for the effects of non-ideal macromixing
Error Detection and Diagnosis for System-on-Chip in Space Applications
Tesis por compendio de publicacionesLos componentes electrónicos comerciales, comúnmente llamados componentes
Commercial-Off-The-Shelf (COTS) están presentes en multitud de dispositivos habituales
en nuestro día a día. Particularmente, el uso de microprocesadores y sistemas en chip (SoC)
altamente integrados ha favorecido la aparición de dispositivos electrónicos cada vez más
inteligentes que sostienen el estilo de vida y el avance de la sociedad moderna. Su uso se
ha generalizado incluso en aquellos sistemas que se consideran críticos para la seguridad,
como vehículos, aviones, armamento, dispositivos médicos, implantes o centrales eléctricas.
En cualquiera de ellos, un fallo podría tener graves consecuencias humanas o económicas.
Sin embargo, todos los sistemas electrónicos conviven constantemente con factores internos
y externos que pueden provocar fallos en su funcionamiento. La capacidad de un sistema
para funcionar correctamente en presencia de fallos se denomina tolerancia a fallos, y es
un requisito en el diseño y operación de sistemas críticos.
Los vehículos espaciales como satélites o naves espaciales también hacen uso de
microprocesadores para operar de forma autónoma o semi autónoma durante su vida útil,
con la dificultad añadida de que no pueden ser reparados en órbita, por lo que se consideran
sistemas críticos. Además, las duras condiciones existentes en el espacio, y en particular
los efectos de la radiación, suponen un gran desafío para el correcto funcionamiento de los
dispositivos electrónicos. Concretamente, los fallos transitorios provocados por radiación
(conocidos como soft errors) tienen el potencial de ser una de las mayores amenazas para
la fiabilidad de un sistema en el espacio.
Las misiones espaciales de gran envergadura, típicamente financiadas públicamente
como en el caso de la NASA o la Agencia Espacial Europea (ESA), han tenido
históricamente como requisito evitar el riesgo a toda costa por encima de cualquier
restricción de coste o plazo. Por ello, la selección de componentes resistentes a la radiación
(rad-hard) específicamente diseñados para su uso en el espacio ha sido la metodología
imperante en el paradigma que hoy podemos denominar industria espacial tradicional, u
Old Space. Sin embargo, los componentes rad-hard tienen habitualmente un coste mucho
más alto y unas prestaciones mucho menores que otros componentes COTS equivalentes.
De hecho, los componentes COTS ya han sido utilizados satisfactoriamente en misiones
de la NASA o la ESA cuando las prestaciones requeridas por la misión no podían ser
cubiertas por ningún componente rad-hard existente.
En los últimos años, el acceso al espacio se está facilitando debido en gran parte a la
entrada de empresas privadas en la industria espacial. Estas empresas no siempre buscan
evitar el riesgo a toda costa, sino que deben perseguir una rentabilidad económica, por
lo que hacen un balance entre riesgo, coste y plazo mediante gestión del riesgo en un
paradigma denominado Nuevo Espacio o New Space. Estas empresas a menudo están
interesadas en entregar servicios basados en el espacio con las máximas prestaciones y el mayor beneficio posibles, para lo cual los componentes rad-hard son menos atractivos
debido a su mayor coste y menores prestaciones que los componentes COTS existentes.
Sin embargo, los componentes COTS no han sido específicamente diseñados para su uso
en el espacio y típicamente no incluyen técnicas específicas para evitar que los efectos de
la radiación afecten su funcionamiento. Los componentes COTS se comercializan tal cual
son, y habitualmente no es posible modificarlos para mejorar su resistencia a la radiación.
Además, los elevados niveles de integración de los sistemas en chip (SoC) complejos
de altas prestaciones dificultan su observación y la aplicación de técnicas de tolerancia
a fallos. Este problema es especialmente relevante en el caso de los microprocesadores.
Por tanto, existe un gran interés en el desarrollo de técnicas que permitan conocer y
mejorar el comportamiento de los microprocesadores COTS bajo radiación sin modificar
su arquitectura y sin interferir en su funcionamiento para facilitar su uso en el espacio y
con ello maximizar las prestaciones de las misiones espaciales presentes y futuras.
En esta Tesis se han desarrollado técnicas novedosas para detectar, diagnosticar y
mitigar los errores producidos por radiación en microprocesadores y sistemas en chip
(SoC) comerciales, utilizando la interfaz de traza como punto de observación. La interfaz de
traza es un recurso habitual en los microprocesadores modernos, principalmente enfocado
a soportar las tareas de desarrollo y depuración del software durante la fase de diseño. Sin
embargo, una vez el desarrollo ha concluido, la interfaz de traza típicamente no se utiliza
durante la fase operativa del sistema, por lo que puede ser reutilizada sin coste. La interfaz
de traza constituye un punto de conexión viable para observar el comportamiento de un
microprocesador de forma no intrusiva y sin interferir en su funcionamiento.
Como resultado de esta Tesis se ha desarrollado un módulo IP capaz de recabar
y decodificar la información de traza de un microprocesador COTS moderno de altas
prestaciones. El IP es altamente configurable y personalizable para adaptarse a diferentes
aplicaciones y tipos de procesadores. Ha sido diseñado y validado utilizando el dispositivo
Zynq-7000 de Xilinx como plataforma de desarrollo, que constituye un dispositivo COTS
de interés en la industria espacial. Este dispositivo incluye un procesador ARM Cortex-A9
de doble núcleo, que es representativo del conjunto de microprocesadores hard-core
modernos de altas prestaciones. El IP resultante es compatible con la tecnología ARM
CoreSight, que proporciona acceso a información de traza en los microprocesadores ARM.
El IP incorpora técnicas para detectar errores en el flujo de ejecución y en los datos de la
aplicación ejecutada utilizando la información de traza, en tiempo real y con muy baja
latencia. El IP se ha validado en campañas de inyección de fallos y también en radiación con
protones y neutrones en instalaciones especializadas. También se ha combinado con otras
técnicas de tolerancia a fallos para construir técnicas híbridas de mitigación de errores.
Los resultados experimentales obtenidos demuestran su alta capacidad de detección y
potencialidad en el diagnóstico de errores producidos por radiación.
El resultado de esta Tesis, desarrollada en el marco de un Doctorado Industrial entre
la Universidad Carlos III de Madrid (UC3M) y la empresa Arquimea, se ha transferido satisfactoriamente al entorno empresarial en forma de un proyecto financiado por la
Agencia Espacial Europea para continuar su desarrollo y posterior explotación.Commercial electronic components, also known as Commercial-Off-The-Shelf (COTS),
are present in a wide variety of devices commonly used in our daily life. Particularly, the
use of microprocessors and highly integrated System-on-Chip (SoC) devices has fostered
the advent of increasingly intelligent electronic devices which sustain the lifestyles and the
progress of modern society. Microprocessors are present even in safety-critical systems,
such as vehicles, planes, weapons, medical devices, implants, or power plants. In any of
these cases, a fault could involve severe human or economic consequences. However, every
electronic system deals continuously with internal and external factors that could provoke
faults in its operation. The capacity of a system to operate correctly in presence of faults
is known as fault-tolerance, and it becomes a requirement in the design and operation of
critical systems.
Space vehicles such as satellites or spacecraft also incorporate microprocessors to
operate autonomously or semi-autonomously during their service life, with the additional
difficulty that they cannot be repaired once in-orbit, so they are considered critical systems.
In addition, the harsh conditions in space, and specifically radiation effects, involve a big
challenge for the correct operation of electronic devices. In particular, radiation-induced
soft errors have the potential to become one of the major risks for the reliability of systems
in space.
Large space missions, typically publicly funded as in the case of NASA or European
Space Agency (ESA), have followed historically the requirement to avoid the risk at any
expense, regardless of any cost or schedule restriction. Because of that, the selection of
radiation-resistant components (known as rad-hard) specifically designed to be used in
space has been the dominant methodology in the paradigm of traditional space industry,
also known as “Old Space”. However, rad-hard components have commonly a much higher
associated cost and much lower performance that other equivalent COTS devices. In fact,
COTS components have already been used successfully by NASA and ESA in missions
that requested such high performance that could not be satisfied by any available rad-hard
component.
In the recent years, the access to space is being facilitated in part due to the irruption
of private companies in the space industry. Such companies do not always seek to avoid
the risk at any cost, but they must pursue profitability, so they perform a trade-off between
risk, cost, and schedule through risk management in a paradigm known as “New Space”.
Private companies are often interested in deliver space-based services with the maximum
performance and maximum benefit as possible. With such objective, rad-hard components
are less attractive than COTS due to their higher cost and lower performance.
However, COTS components have not been specifically designed to be used in space
and typically they do not include specific techniques to avoid or mitigate the radiation effects in their operation. COTS components are commercialized “as is”, so it is not
possible to modify them to improve their susceptibility to radiation effects. Moreover,
the high levels of integration of complex, high-performance SoC devices hinder their
observability and the application of fault-tolerance techniques. This problem is especially
relevant in the case of microprocessors. Thus, there is a growing interest in the development
of techniques allowing to understand and improve the behavior of COTS microprocessors
under radiation without modifying their architecture and without interfering with their
operation. Such techniques may facilitate the use of COTS components in space and
maximize the performance of present and future space missions.
In this Thesis, novel techniques have been developed to detect, diagnose, and
mitigate radiation-induced errors in COTS microprocessors and SoCs using the trace
interface as an observation point. The trace interface is a resource commonly found
in modern microprocessors, mainly intended to support software development and
debugging activities during the design phase. However, it is commonly left unused
during the operational phase of the system, so it can be reused with no cost. The trace
interface constitutes a feasible connection point to observe microprocessor behavior in a
non-intrusive manner and without disturbing processor operation.
As a result of this Thesis, an IP module has been developed capable to gather and
decode the trace information of a modern, high-end, COTS microprocessor. The IP is highly
configurable and customizable to support different applications and processor types. The
IP has been designed and validated using the Xilinx Zynq-7000 device as a development
platform, which is an interesting COTS device for the space industry. This device features a
dual-core ARM Cortex-A9 processor, which is a good representative of modern, high-end,
hard-core microprocessors. The resulting IP is compatible with the ARM CoreSight
technology, which enables access to trace information in ARM microprocessors. The IP is
able to detect errors in the execution flow of the microprocessor and in the application data
using trace information, in real time and with very low latency. The IP has been validated
in fault injection campaigns and also under proton and neutron irradiation campaigns in
specialized facilities. It has also been combined with other fault-tolerance techniques
to build hybrid error mitigation approaches. Experimental results demonstrate its high
detection capabilities and high potential for the diagnosis of radiation-induced errors.
The result of this Thesis, developed in the framework of an Industrial Ph.D. between the
University Carlos III of Madrid (UC3M) and the company Arquimea, has been successfully
transferred to the company business as a project sponsored by European Space Agency to
continue its development and subsequent commercialization.Programa de Doctorado en Ingeniería Eléctrica, Electrónica y Automática por la Universidad Carlos III de MadridPresidenta: María Luisa López Vallejo.- Secretario: Enrique San Millán Heredia.- Vocal: Luigi Di Lill
Microgravity Science and Applications
The report presents fifteen papers from a workshop on microgravity science and applications held at the Jet Propulsion Laboratory in Pasadena, California, on December 3 to 4, 1984. The workshop and panel were formed by the Solid State Sciences Committee of the Board on Physics and Astronomy of the National Research Council in response to a request from the Office of Science and Technology Policy. The goal was to review the microgravity science and applications (MSA) program of NASA and to evaluate the quality of the program. The topics for the papers are metals and alloys, electronic materials, ceramics and glasses, biotechnology, combustion science, and fluid dynamics
- …