Wetland maps including open water extent dynamics based on ENVISAT ASAR WS for Siberia, 2007 and 2008, links to GeoTIFFs

Wetlands store large amounts of carbon, and depending on their status and type, they release specific amounts of methane gas to the atmosphere. The connection between wetland type and methane emission has been investigated in various studies and utilized in climate change monitoring and modelling. For improved estimation of methane emissions, land surface models require information such as the wetland fraction and its dynamics over large areas. Existing datasets of wetland dynamics present the total amount of wetland (fraction) for each model grid cell, but do not discriminate the different wetland types like permanent lakes, periodically inundated areas or peatlands. Wetland types differently influence methane fluxes and thus their contribution to the total wetland fraction should be quantified. Especially wetlands of permafrost regions are expected to have a strong impact on future climate due to soil thawing. In this study ENIVSAT ASAR Wide Swath data was tested for operational monitoring of the distribution of areas with a long-term SW near 1 (hSW) in northern Russia (SW = degree of saturation with water, 1 = saturated), which is a specific characteristic of peatlands. For the whole northern Russia, areas with hSW were delineated and discriminated from dynamic and open water bodies for the years 2007 and 2008. The area identified with this method amounts to approximately 300,000 km**2 in northern Siberia in 2007. It overlaps with zones of high carbon storage. Comparison with a range of related datasets (static and dynamic) showed that hSW represents not only peatlands but also temporary wetlands associated with post-forest fire conditions in permafrost regions. Annual long-term monitoring of change in boreal and tundra environments is possible with the presented approach. Sentinel-1, the successor of ENVISAT ASAR, will provide data that may allow continuous monitoring of these wetland dynamics in the future complementing global observations of wetland fraction.

Comparisons of observed ice properties and Envisat Advanced Synthetic Aperture Radar (ASAR) data during Nathanial B. Palmer cruise NBP09-01 and Oden cruise OSO08/09

Envisat Advanced Synthetic Aperture Radar (ASAR) Wide Swath Mode (WSM) images are used to derive C-band HH-polarization normalized radar cross sections (NRCS). These are compared with ice-core analysis and visual ship-based observations of snow and ice properties observed according to the Antarctic Sea Ice Processes and Climate (ASPeCt) protocol during two International Polar Year summer cruises (Oden 2008 and Palmer 2009) in West Antarctica. Thick first-year (TFY) and multi-year (MY) ice were the dominant ice types. The NRCS value ranges between -16.3 ± 1.1 and -7.6 ± 1.0 dB for TFY ice, and is -12.6 ± 1.3 dB for MY ice; for TFY ice, NRCS values increase from ~-15 dB to -9 dB from December/January to mid-February. In situ and ASPeCt observations are not, however, detailed enough to interpret the observed NRCS change over time. Co-located Advanced Microwave Scanning Radiometer-Earth Observing System (AMSR-E) vertically polarized 37 GHz brightness temperatures (TB37V), 7 day and 1 day averages as well as the TB37V difference between ascending and descending AMSR-E overpasses suggest the low NRCS values (-15 dB) are associated with snowmelt being still in progress, while the change towards higher NRCS values (-9dB) is caused by commencement of melt-refreeze cycles after about mid-January.

Plume-top altitude time-series during May 2011 volcanic eruption of Grímsvötn, Iceland

Plume-top altitude time series of the volcanic plume during the eruption of Grímsvötn in Iceland 21-28 May 2011. The altitude was estimated from weather radar echo top data from two weather radars, Keflavik and Klaustur. Keflavik radar is a fixed position C-band weather radar close to Keflavik International Airport, at 64°01.583'N, 22°38.150'W. The height of the antenna is 47 m a.s.l. and the distance to Grímsvötn volcano is 257 km. Klaustur radar is a mobile X-band weather radar located close to Kirkjubaejarklaustur, at 63°46.500'N, 17°57.817'W. The height of the antenna is also 47 m a.s.l. and the distance to Grímsvötn volcano is 75 km.

(Table 1) Accumulation and ice discharge of West Antarctic glaciers draining into the Amundsen Sea between 1974 and 2007

The Advanced Land Observation System (ALOS) Phased-Array Synthetic-Aperture Radar (PALSAR) is an L-band frequency (1.27 GHz) radar capable of continental-scale interferometric observations of ice sheet motion. Here, we show that PALSAR data yield excellent measurements of ice motion compared to C-band (5.6 GHz) radar data because of greater temporal coherence over snow and firn. We compare PALSAR velocities from year 2006 in Pine Island Bay, West Antarctica with those spanning years 1974 to 2007. Between 1996 and 2007, Pine Island Glacier sped up 42% and ungrounded over most of its ice plain. Smith Glacier accelerated 83% and ungrounded as well. Their largest speed up are recorded in 2007. Thwaites Glacier is not accelerating but widening with time and its eastern ice shelf doubled its speed. Total ice discharge from these glaciers increased 30% in 12 yr and the net mass loss increased 170% from 39 ± 15 Gt/yr to 105 ± 27 Gt/yr. Longer-term velocity changes suggest only a moderate loss in the 1970s. As the glaciers unground into the deeper, smoother beds inland, the mass loss from this region will grow considerably larger in years to come.

Plume-top altitude time-series during 2010 volcanic eruption of Eyjafjallajökull

The eruption of Eyjafjallajökull volcano in 2010 lasted for 39 days, 14 April-23 May. The eruption had two explosive phases separated by a phase with lava formation and reduced explosive activity. The height of the plume was monitored every 5 min with a C-band weather radar located in Keflavík International Airport, 155 km distance from the volcano. Furthermore, several web cameras were mounted with a view of the volcano, and their images saved every five seconds. Time series of the plume-top altitude were constructed from the radar observations and images from a web camera located in the village Hvolsvöllur at 34 km distance from the volcano. This paper presents the independent radar and web camera time series and performs cross validation.

Diseño, implementación y verificación de una antena de microondas

A lo largo de este proyecto se han tratado las diferentes fases que tienen lugar durante el desarrollo del programa de Diseño y Verificación de una Bocina en Banda C destinada a un satélite comercial de comunicaciones. En un primer lugar, se introduce el proyecto en el mundo real realizando una pequeña aproximación a los satélites artificiales y su historia. Después, en una primera fase, se describen los diversos puntos de la etapa de diseño y los resultados de la simulación de nuestra Antena. Se estudian por separado los diferentes elementos que componen el equipo, y además, se realiza un análisis de los parámetros eléctricos que se deben tener en cuenta durante el diseño para adaptar el comportamiento de la Antena a los requisitos solicitados por el cliente. Antes de realizar la verificación de la Antena, se procede a la definición de los ensayos, que se debe realizar sobre el equipo con el fin de simular las condiciones a las que se verá sometido. Pruebas y medidas, niveles de test, etc. que nos ayudan a demostrar que nuestra Antena está preparada para realizar su misión en el espacio. Se hará una descripción sobre la forma de realizar de los ensayos y de las instalaciones donde se van a llevar a cabo, además del orden que llevaremos durante la campaña. Una vez determinados los test y con la Antena fabricada y lista, se procede a la Verificación de nuestro equipo mediante la Campaña de Ensayos con el objetivo de caracterizar por completo el funcionamiento de nuestra Antena en cualquier circunstancia. Se muestran los resultados obtenidos en los test siguiendo el orden establecido por el Test Plan. Medidas en Laboratorio y Radiación, los test de vibración y las pruebas ambientales en las Cámaras Térmicas de Vacío, y medidas eléctricas en condiciones extremas de temperatura y presión. Y una vez realizada la Campaña, se vuelve a medir la Antena para comprobar el funcionamiento tras soportar todos los ensayos. Se analizan los resultados obtenidos en cada una de las pruebas y se comparan con las simulaciones obtenidas durante la fase de diseño. Finalmente, se realiza un pequeño resumen de los valores más importantes obtenidos durante la Verificación y exponen las Conclusiones que se desprende de dicho proceso. Como último punto del proyecto, se estudian las correcciones y mejoras que se podrán llevar a cabo en futuros programas gracias a lo que hemos aprendido en este proyecto. Abstract This project presents a C Band Horn Antenna for a commercial communications satellite. All the different phases from Design to Verification are presented. First of all, an introduction to artificial satellites and their history is presented to put this project into perspective. Next, the electrical design of the Antenna is presented. Taking into account the theoretical fundamentals, each element that comprises this Antenna was designed. Their electrical performances, obtained from analysis using commercial software, are presented in the simulation results. In the design of each element of the antenna, some critical parameters are set and optimized in order to be compliant with the global requirements requested by the customer. After the design is completed, it is necessary to define the Test Campaign that has to be carried out in order to verify the validity of the designed and manufactured Antenna. Therefore, a Test Plan and the Electrical and Environmental Test Procedures are defined. This Test Campaign must be representative of the same conditions of the real space mission. Considering this, the following are defined: parameters for the network analyzer and radiation patterns measurements; test levels for the environmental test; definition of the RF measurements to be carried out and the temperatures to be applied in the thermal vacuum cycling. If the Antenna surpasses these tests, it will be ready to perform its mission in space over the entire satellite’s life cycle. The facilities where the tests are performed, as well as the sequence of the tests along the campaign are described too. After that, the Test Campaign is performed to fully characterize the Antenna in the space simulated conditions. Following the order established in the Test Plan, a radiation pattern and laboratory parameters are measured to correlate its electrical response with the simulations. Then, vibration and thermal vacuum tests are performed to verify its behavior in extreme environmental conditions. Last, if the final electrical results are the same as the initial ones, it can be stated that the antenna has successfully passed the Test Campaign. And finally, conclusions obtained from the data simulation design and Test Campaign results are presented. Status of Compliance with the specification is shown to demonstrate that the Antenna fulfills the requested requirements. Although the purpose of this project is to design and verify the response of C Band Horn Antenna, it is important to highlight improvements for future developments and the lessons learnt during this project.

Heterogeneity and Photoinhibition of Photosystem II Studied with Thermoluminescence1

Thermoluminescence (TL) signals were recorded from grana stacks, margins, and stroma lamellae from fractionated, dark-adapted thylakoid membranes of spinach (Spinacia oleracea L.) in the absence and in the presence of 2,6-dichlorphenylindophenol (DCMU). In the absence of DCMU, the TL signal from grana fractions consisted of a homogenous B-band, which originates from recombination of the semi-quinone QB− with the S2 state of the water-splitting complex and reflects active photosystem II (PSII). In the presence of DCMU, the B-band was replaced by the Q-band, which originates from an S2QA− recombination. Margin fractions mainly showed two TL-bands, the B- and C-bands, at approximately 50°C in the absence of DCMU, and Q- and C-bands in the presence of DCMU. The C-band is ascribed to a TyrD+-QA− recombination. In the absence of DCMU, the fractions of stromal lamellae mainly gave rise to a TL emission at 42°C. The intensity of this band was independent of the number of excitation flashes and was shifted to higher temperatures (52°C) after the addition of DCMU. Based on these observations, this band was considered to be a C-band. After photoinhibitory light treatment of uncoupled thylakoid membranes, the TL intensities of the B- and Q-bands decreased, whereas the intensity at 45°C (C-band) slightly increased. It is proposed that the 42 to 52°C band that was observed in marginal and stromal lamellae and in photoinhibited thylakoid membranes reflects inactive PSII centers that are assumed to be equivalent to inactive PSII QB-nonreducing centers.

Desenvolvimento de materiais nanoestruturados à base de SiO2-Nb2O5 preparados por uma nova rota sol-gel com aplicações em fotônica

Este trabalho concentra-se na preparação e caracterizações estrutural e espectroscópica de materiais nanoestruturados à base de SiO2-Nb2O5 dopados e codopados com íons Er3+, Yb3+ e Eu3+ na forma de pós e guias de onda planares. Os nanocompósitos foram preparados através de uma nova rota sol-gel utilizando óxido de nióbio como precursor em substituição ao alcóxido de nióbio. A correlação estrutura propriedades luminescentes foi estudada por difração de raios X, microscopia eletrônica de transmissão, espectroscopia vibracional de absorção no infravermelho, espectroscopia vibracional de espalhamento Raman, análise térmica, reflectância difusa e especular, espectroscopia de fotoluminescência e acoplamento M-line. Inicialmente foi avaliado a influência da concentração de nióbio nas propriedades estruturais e luminescentes de nanocompósitos (100-x)Si-xNb dopados e codopados com íons Er3+, Yb3+ e Eu3+ tratados termicamente a 900 °C por 3h. A cristalização do Nb2O5 foi dependente da concentração de Nb na matriz, com a distribuição dos íons lantanídeos preferencialmente no Nb2O5, afetando as propriedades luminescentes. Para os nanocompósitos codopados com íons Er3+ e Yb3+ foram obtidos valores de largura de banda a meia altura (FWHM) da ordem de 70 nm na região de 1550 nm e tempos de vida de até 5,2 ms. A emissão na região do visível, decorrente de processos de conversão ascendente, revelou-se dependente da concentração de nióbio. Foi verificada emissão preferencial na região do verde para menores concentrações de Nb. Enquanto que, para as maiores concentrações, processos de relaxação cruzada levaram a um aumento relativo na intensidade de emissão na região do vermelho. A eficiência quântica de emissão dos nanocompósitos (100-x)Si-xNb dopados com Eu3+ variou com o comprimento de onda de excitação, refletindo os diferentes sítios de simetria ocupados por este íons nesta estrutura complexa. A influência da temperatura de tratamento térmico no processo de cristalização do Nb2O5 em nanocompósitos 70Si:30Nb codopados com íons Er3+ e Yb3+ foi avaliada. Material amorfo foi obtido a 700 °C enquanto que a 900 e 1100 °C foram identificas as fases ortorrômbica (fase T) e monoclínica (fase M) do Nb2O5. Intensa emissão na região de 1550 nm com valores de FWHM de 52 e 67 nm e tempos de vida de 5,6 e 5,4 ms foram verificados a 700 e 900 °C sob excitação em 977 nm, respectivamente. Por fim, foram obtidos guias de onda planares com excelentes propriedades ópticas e com grande potencial de aplicação em dispositivos de amplificação óptica. Especificamente, materiais fotônicos com banda larga de emissão na região do infravermelho foram preparados, indicando fortemente a potencialidade para a aplicação em telecomunicações envolvendo não somente a banda C como também as bandas L e S em materiais contendo somente íons Er3+ como centros emissores.

Agricultural co-operation in Germany and in Ireland. 1913.

Cover title.

On the old plantation; reminiscences of his childhood,

Mode of access: Internet.

First year qualifying report: neural networks for extracting wind vectors from satellite scatterometer data

The ERS-1 Satellite was launched in July 1991 by the European Space Agency into a polar orbit at about km800, carrying a C-band scatterometer. A scatterometer measures the amount of radar back scatter generated by small ripples on the ocean surface induced by instantaneous local winds. Operational methods that extract wind vectors from satellite scatterometer data are based on the local inversion of a forward model, mapping scatterometer observations to wind vectors, by the minimisation of a cost function in the scatterometer measurement space.par This report uses mixture density networks, a principled method for modelling conditional probability density functions, to model the joint probability distribution of the wind vectors given the satellite scatterometer measurements in a single cell (the `inverse' problem). The complexity of the mapping and the structure of the conditional probability density function are investigated by varying the number of units in the hidden layer of the multi-layer perceptron and the number of kernels in the Gaussian mixture model of the mixture density network respectively. The optimal model for networks trained per trace has twenty hidden units and four kernels. Further investigation shows that models trained with incidence angle as an input have results comparable to those models trained by trace. A hybrid mixture density network that incorporates geophysical knowledge of the problem confirms other results that the conditional probability distribution is dominantly bimodal.par The wind retrieval results improve on previous work at Aston, but do not match other neural network techniques that use spatial information in the inputs, which is to be expected given the ambiguity of the inverse problem. Current work uses the local inverse model for autonomous ambiguity removal in a principled Bayesian framework. Future directions in which these models may be improved are given.