New methods to reduce leakage errors in planar near-field measurements

This paper describes two methods to cancel the effect of two kinds of leakage signals which may be presented when an antenna is measured in a planar near-field range. One method tries to reduce leakage bias errors from the receiver¿s quadrature detector and it is based on estimating the bias constant added to every near-field data sample. Then, that constant is subtracted from the data, removing its undesired effect on the far-field pattern. The estimation is performed by back-propagating the field from the scan plane to the antenna under test plane (AUT) and averaging all the data located outside the AUT aperture. The second method is able to cancel the effect of the leakage from faulty transmission lines, connectors or rotary joints. The basis of this method is also a reconstruction process to determine the field distribution on the AUT plane. Once this distribution is known, a spatial filtering is applied to cancel the contribution due to those faulty elements. After that, a near-field-to-far-field transformation is applied, obtaining a new radiation pattern where the leakage effects have disappeared. To verify the effectiveness of both methods, several examples are presented.

3D Object following based on visual information for Unmanned Aerial Vehicles

This article presents a novel system and a control strategy for visual following of a 3D moving object by an Unmanned Aerial Vehicle UAV. The presented strategy is based only on the visual information given by an adaptive tracking method based on the color information, which jointly with the dynamics of a camera fixed to a rotary wind UAV are used to develop an Image-based visual servoing IBVS system. This system is focused on continuously following a 3D moving target object, maintaining it with a fixed distance and centered on the image plane. The algorithm is validated on real flights on outdoors scenarios, showing the robustness of the proposed systems against winds perturbations, illumination and weather changes among others. The obtained results indicate that the proposed algorithms is suitable for complex controls task, such object following and pursuit, flying in formation, as well as their use for indoor navigation

Simulation of Freight Trains Equipped with Partially Filled Tank Containers and Related Resonance Phenomenon

To study the fluid motion-vehicle dynamics interaction, a model of four, liquid filled two-axle container freight wagons was set up. The railway vehicle has been modelled as a multi-body system (MBS). To include fluid sloshing, an equivalent mechanical model has been developed and incorporated. The influence of several factors has been studied in computer simulations, such as track defects, curve negotiation, train velocity, wheel wear, liquid and solid wagonload, and container baffles. SIMPACK has been used for MBS analysis, and ANSYS for liquid sloshing modelling and equivalent mechanical systems validation. Acceleration and braking manoeuvres of the freight train set the liquid cargo into motion. This longitudinal sloshing motion of the fluid cargo inside the tanks initiated a swinging motion of some components of the coupling gear. The coupling gear consists of UIC standard traction hooks and coupling screws that are located between buffers. One of the coupling screws is placed in the traction hook of the opposite wagon thus joining the two wagons, whereas the unused coupling screw rests on a hanger. Simulation results showed that, for certain combinations of type of liquid, filling level and container dimensions, the liquid cargo could provoke an undesirable, although not hazardous, release of the unused coupling screw from its hanger. The coupling screw's release was especially obtained when a period of acceleration was followed by an abrupt braking manoeuvre at 1 m/s2. It was shown that a resonance effect between the liquid's oscillation and the coupling screw's rotary motion could be the reason for the coupling screw's undesired release. Possible solutions to avoid the phenomenon are given.Acceleration and braking manoeuvres of the freight train set the liquid cargo into motion. This longitudinal sloshing motion of the fluid cargo inside the tanks initiated a swinging motion of some components of the coupling gear. The coupling gear consists of UIC standard traction hooks and coupling screws that are located between buffers. One of the coupling screws is placed in the traction hook of the opposite wagon thus joining the two wagons, whereas the unused coupling screw rests on a hanger. This paper reports on a study of the fluid motion-train vehicle dynamics interaction. In the study, a model of four, liquid-filled two-axle container freight wagons was developed. The railway vehicle has been modeled as a multi-body system (MBS). To include fluid sloshing, an equivalent mechanical model has been developed and incorporated. The influence of several factors has been studied in computer simulations, such as track defects, curve negotiation, train velocity, wheel wear, liquid and solid wagonload, and container baffles. A simulation program was used for MBS analysis, and a finite element analysis program was used for liquid sloshing modeling and equivalent mechanical systems validation. Acceleration and braking maneuvers of the freight train set the liquid cargo into motion. This longitudinal sloshing motion of the fluid cargo inside the tanks initiated a swinging motion of some components of the coupling gear. Simulation results showed that, for certain combinations of type of liquid, filling level and container dimensions, the liquid cargo could provoke an undesirable, although not hazardous, release of an unused coupling screw from its hanger. It was shown that a resonance effect between the liquid's oscillation and the coupling screw's rotary motion could be the reason for the coupling screw's undesired release. Solutions are suggested to avoid the resonance problem, and directions for future research are given.

Aerial Object Following Using Visual Fuzzy Servoing

This article presents a visual servoing system to follow a 3D moving object by a Micro Unmanned Aerial Vehicle (MUAV). The presented control strategy is based only on the visual information given by an adaptive tracking method based on the colour information. A visual fuzzy system has been developed for servoing the camera situated on a rotary wing MAUV, that also considers its own dynamics. This system is focused on continuously following of an aerial moving target object, maintaining it with a fixed safe distance and centred on the image plane. The algorithm is validated on real flights on outdoors scenarios, showing the robustness of the proposed systems against winds perturbations, illumination and weather changes among others. The obtained results indicate that the proposed algorithms is suitable for complex controls task, such object following and pursuit, flying in formation, as well as their use for indoor navigation

Utilización del cultivo plurianual de pataca (Helianthus tuberosus L.) para la producción de hidratos de carbono fermentables a partir de los tallos

La pataca (Helianthus tuberosus L.) es una especie de cultivo con un alto potencial en la producción de hidratos de carbono de reserva en forma de polifructanos, especialmente inulina, que se acumulan temporalmente en los tallos en forma de polisacáridos para translocarse posteriormente a los tubérculos, donde son almacenados. Aunque tradicionalmente el producto de interés del cultivo son los tubérculos, que acumulan gran cantidad de hidratos de carbono fermentables (HCF) cuando se recogen al final del ciclo de desarrollo, en este trabajo se pretende evaluar el potencial de la pataca como productor de HCF a partir de los tallos cosechados en el momento de máximo contenido en HCF, mediante un sistema de cultivo plurianual. Se han realizado los siguientes estudios: i) Determinación del momento óptimo de cosecha en ensayos con 12 clones ii) Potencial del cultivo plurianual de la pataca en términos de producción anual de biomasa aérea y de HCF en cosechas sucesivas, iii) Ensayos de conservación de la biomasa aérea, iv) Estimación de los costes de las dos modalidades de cultivo de pataca para producción de HCF y v) Estimación de la sostenibilidad energética de la producción de bioetanol mediante la utilización de los subproductos. Para la determinación del momento óptimo de la cosecha de la biomasa aérea se ensayaron 12 clones de diferente precocidad en Madrid; 4 tempranos (Huertos de Moya, C-17, Columbia y D-19) y 8 tardíos (Boniches, China, K-8, Salmantina, Nahodka, C-13, INIA y Violeta de Rennes). El máximo contenido en HCF tuvo lugar en el estado fenológico de botón floral-flor que además coincidió con la máxima producción de biomasa aérea. De acuerdo con los resultados obtenidos, la cosecha de los clones tempranos se debería realizar en el mes de julio y en los clones tardíos en septiembre, siendo éstos últimos más productivos. La producción media más representativa entre los 12 clones, obtenida en el estado fenológico de botón floral fue de 23,40 t ms/ha (clon INIA), con un contenido medio en HCF de 30,30 % lo que supondría una producción potencial media de 7,06 t HCF/ha. La producción máxima en HCF se obtuvo en el clon Boniches con 7,61 t/ha y 22,81 t ms/ha de biomasa aérea. En el sistema de cultivo plurianual la cantidad de tallos por unidad de superficie aumenta cada año debido a la cantidad de tubérculos que van quedando en el terreno, sobre todo a partir del 3er año, lo que produce la disminución del peso unitario de los tallos, con el consiguiente riesgo de encamado. El aclareo de los tallos nacidos a principios de primavera mediante herbicidas tipo Glifosato o mediante una labor de rotocultor rebaja la densidad final de tallos y mejora los rendimientos del cultivo. En las experiencias de conservación de la biomasa aérea se obtuvo una buena conservación por un período de 6 meses de los HCF contenidos en los tallos secos empacados y almacenados bajo cubierta. Considerando que el rendimiento práctico de la fermentación alcohólica es de 0,5 l de etanol por cada kg de azúcar, la producción potencial de etanol para una cosecha de tallos de 7,06 t de HCF/ha sería de 3.530 l/ha. El bagazo producido en la extracción de los HCF de la biomasa aérea supondría 11,91 t/ha lo que utilizado para fines térmicos supone más de 3 veces la energía primaria requerida en el proceso de producción de etanol, considerando un poder calorífico inferior de 3.832,6 kcal/kg. Para una producción de HCF a partir de la biomasa aérea de 7,06 t/ha y en tubérculos al final del ciclo de 12,11 t/ha, los costes de producción estimados para cada uno de ellos fueron de 184,69 €/t para los HCF procedentes de la biomasa aérea y 311,30 €/t para los de tubérculos. Como resultado de este trabajo se puede concluir que la producción de HCF a partir de la biomasa aérea de pataca en cultivo plurianual, es viable desde un punto de vista técnico, con reducción de los costes de producción respecto al sistema tradicional de cosecha de tubérculos. Entre las ventajas técnicas de esta modalidad de cultivo, cabe destacar: la reducción de operaciones de cultivo, la facilidad y menor coste de la cosecha, y la posibilidad de conservación de los HCF en la biomasa cosechada sin mermas durante varios meses. Estas ventajas, compensan con creces el menor rendimiento por unidad de superficie que se obtiene con este sistema de cultivo frente al de cosecha de los tubérculos. Jerusalem artichoke (Helianthus tuberosus L.) (JA) is a crop with a high potential for the production of carbohydrates in the form of polyfructans, especially inulin, which are temporarily accumulated in the stems in the form of polysaccharides. Subsequently they are translocated to the tubers, where they are finally accumulated. In this work the potential of Jerusalem artichoke for fermentable carbohydrates from stems that are harvested at their peak of carbohydrates accumulation is assessed as compared to the traditional cultivation system that aims at the production of tubers harvested at the end of the growth cycle. Tubers are storage organs of polyfructans, namely fermentable carbohydrates. Studies addressed in this work were: i) Determination of the optimum period of time for stem harvesting as a function of clone precocity in a 12-clone field experiment; ii) Study of the potential of JA poly-annual crop regarding the annual yield of aerial biomass and fermentable carbohydrates (HCF) over the years; iii) Tests of storage of the aerial biomass, iv) Comparative analysis of the two JA cultivation systems for HCF production: the poly-annual system for aerial biomass harvesting versus the annual cultivation system for tubers and v) Estimation of the energy sustainability of the bioethanol production by using by-products of the production chain. In order to determine the best period of time for aerial biomass harvesting twelve JA clones of different precocity were tested in Madrid: four early clones (Huertos de Moya, C-17, Columbia and D-19) and eight late clones (Boniches, China, K-8 , Salmantina, Nahodka, C-13, INIA and Violeta de Rennes). Best time was between the phenological stages of floral buds (closed capitula) and blossom (opened capitula), period in which the peak of biomass production coincides with the peak of HCF accumulation in the stems. According to the results, the early clones should be harvested in July and the late ones in September, being the late clones more productive. The clone named INIA was the one that exhibited more steady yields in biomass over the 12 clones experimented. The average potential biomass production of this clone was 23.40 t dm/ha when harvested at the floral buds phenological stage; mean HCF content is 30.30%, representing 7.06 t HCF/ha yield. However, the highest HCF production was obtained for the clone Boniches, 7.61 t HCF/ha from a production of 22.81 t aerial biomass/ha. In the poly-annual cultivation system the number of stems per unit area increases over the years due to the increase in the number of tubers that are left under ground; this effect is particularly important after the 3rd year of the poly-annual crop and results in a decrease of the stems unit weight and a risk of lodging. Thinning of JA shoots in early spring, by means of an herbicide treatment based on glyphosate or by means of one pass with a rotary tiller, results in a decrease of the crop stem density and in higher crop yields. Tests of biomass storing showed that the method of keeping dried stems packed and stored under cover results in a good preservation of HCF for a period of six months at least. Assuming that the fermentation yield is 0.5 L ethanol per kg sugars and a HCF stem production of 7.06 t HCF/ha, the potential for bioethanol is estimated at 3530 L/ha. The use of bagasse -by-product of the process of HCF extraction from the JA stems- for thermal purposes would represent over 3 times the primary energy required for the industrial ethanol production process, assuming 11.91 t/ha bagasse and 3832.6 kcal/kg heating value. HCF production costs of 7.06 t HCF/ha yield from aerial biomass and HCF production costs of 12.11 t HCF/ha from tubers were estimated at 184.69 €/t HCF and 311.30 €/t HCF, respectively. It can be concluded that the production of HCF from JA stems, following a poly-annual cultivation system, can be feasible from a technical standpoint and lead to lower production costs as compared to the traditional annual cultivation system for the production of HCF from tubers. Among the technical advantages of the poly-annual cultivation system it is worth mentioning the reduction in crop operations, the ease and efficiency of harvesting operations and the possibility of HCF preservation without incurring in HCF losses during the storage period, which can last several months. These advantages might compensate the lower yield of HCF per unit area that is obtained in the poly-annual crop system, which aims at stems harvesting, versus the annual one, which involves tubers harvesting.

Use of calculus of variations to determine the shape of hovering rotors of minimum power and its application to micro air vehicles

In this paper, calculus of variations and combined blade element and momentum theory (BEMT) are used to demonstrate that, in hover, when neither root nor tip losses are considered; the rotor, which minimizes the total power (MPR), generates an induced velocity that varies linearly along the blade span. The angle of attack of every blade element is constant and equal to its optimum value. The traditional ideal twist (ITR) and optimum (OR) rotors are revisited in the context of this variational framework. Two more optimum rotors are obtained considering root and tip losses, the ORL, and the MPRL. A comparison between these five rotors is presented and discussed. The MPR and MPRL present a remarkable saving of power for low values of both thrust coefficient and maximum aerodynamic efficiency. The result obtained can be exploited to improve the aerodynamic behaviour of rotary wing micro air vehicles (MAV). A comparison with experimental results obtained from the literature is presented.

A General Purpose Configurable Navigation Controller for Micro Aerial Multirotor Vehicles

In this paper, we consider the problem of autonomous navigation of multirotor platforms in GPS-denied environments. The focus of this work is on safe navigation based on unperfect odometry measurements, such as on-board optical flow measurements. The multirotor platform is modeled as a flying object with specific kinematic constraints that must be taken into account in order to obtain successful results. A navigation controller is proposed featuring a set of configurable parameters that allow, for instance, to have a configuration setup for fast trajectory following, and another to soften the control laws and make the vehicle navigation more precise and slow whenever necessary. The proposed controller has been successfully implemented in two different multirotor platforms with similar sensoring capabilities showing the openness and tolerance of the approach. This research is focused around the Computer Vision Group's objective of applying multirotor vehicles to civilian service applications. The presented work was implemented to compete in the International Micro Air Vehicle Conference and Flight Competition IMAV 2012, gaining two awards: the Special Award on "Best Automatic Performance - IMAV 2012" and the second overall prize in the participating category "Indoor Flight Dynamics - Rotary Wing MAV". Most of the code related to the present work is available as two open-source projects hosted in GitHub.