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Zeitschriftenartikel zum Thema "Pvsol"

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Bugała, Artur, und Karol Bednarek. „The use of computer simulations and measurements in determining the energy efficiency of photovoltaic installations“. ITM Web of Conferences 19 (2018): 01021. http://dx.doi.org/10.1051/itmconf/20181901021.

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The paper presents an analysis of the energy efficiency of a photovoltaic installation connected to the AC power grid. Forecasting of energy yield was carried out in two ways: with the use of PVSol software, as well as physical measurements of daily electricity production. On that basis, a statistical correlation between the results obtained from measurements and computer calculations was determined.
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Abernethy, Margaret A., Yu Flora Kuang und Bo Qin. „The Influence of CEO Power on Compensation Contract Design“. Accounting Review 90, Nr. 4 (01.10.2014): 1265–306. http://dx.doi.org/10.2308/accr-50971.

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ABSTRACT We investigate whether CEO power influences a firm's decision to change its compensation system in response to regulatory and public pressure. In particular, we assess whether CEO power influences the choice of performance measures as a form of camouflage to minimize the impact of these reforms on their wealth. We examine one component of CEO pay, namely, the use of performance-vested stock option (PVSO) plans, and find that firms with powerful CEOs attach less challenging targets in the initial PVSOs granted to their CEOs. Such firms also appear to adopt PVSO plans early, and are more likely to do so when faced with public outrage over executive compensation. Our results suggest that powerful CEOs attempt to appease public outrage by quickly adopting PVSOs, but that adopting PVSOs early does not appear to be an optimal strategy for increasing shareholder value. Regulators intended that implementation of PVSOs would be beneficial to shareholders by improving the link between CEO pay and firm performance. However, our results indicate that powerful CEOs can negate some of the beneficial effect of PVSOs through their influence on adoption and choice of performance targets. Data Availability: All data used in this study are publicly available from the sources indicated in the paper.
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ABDÜLSAMED, TABAK, und ENDIZ MUSTAFA SACID. „THE COMPARATIVE ANALYZES OF SOLAR ENERGY PRODUCTION POTENTIAL BETWEEN VAN AND ANTALYA USING PVSOL SIMULATION TOOL“. i-manager’s Journal on Instrumentation and Control Engineering 4, Nr. 3 (2016): 1. http://dx.doi.org/10.26634/jic.4.3.7061.

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Mehadi, Abdullah Al, Misbahul Alam Chowdhury, Mirza Muntasir Nishat, Fahim Faisal und Md Minhajul Islam. „A software-based approach in designing a rooftop bifacial PV system for the North Hall of Residence, IUT“. Clean Energy 5, Nr. 3 (08.07.2021): 403–22. http://dx.doi.org/10.1093/ce/zkab019.

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Abstract Bifacial rooftop photovoltaic panels appear to be an excellent means of power generation in this era of urbanization, especially for land-limited countries like Bangladesh. This paper presents a software-based approach to design and simulate a bifacial solar-panel-based energy model on the rooftop of the North Hall of Residence of the Islamic University of Technology, Gazipur. This vertically mounted model investigates the feasibility and applicability of such an energy model in a university residence, situated in a load-shedding-prone area. Hence, three prominent software platforms, namely PVSOL, PVsyst and System Advisor Model (SAM), are brought into action and rigorous simulations are performed for three different orientations; promising outcomes are observed in terms of annual energy yield, bifacial gain (BG) and consumption coverage of the grid and PV model. The annual energy demand of the North Hall is ~444 733.5 kWh. The three orientations can generate annually 92 508.62, 94 643.48 and 86 758.94 kWh, respectively. Hence, it is evident that the proposed orientations can supply almost 19–21% of the site’s annual demand. Monthly BG analysis shows an overall increase in energy gain of 13%, 15.6% and 6% for Orientation-1, Orientation-2 and Orientation-3, respectively. A rigorous comparative analysis and deviation analysis among the software results has been accomplished to gain more insight into the feasibility of the proposed system. Thus, we have focused on a detailed software-based estimation of energy production for different orientations of the PV panels, considering several factors, which will provide prior knowledge and assessment before going for hardware implementation in the future.
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Mubarak, Riyad, Eduardo Weide Luiz und Gunther Seckmeyer. „Why PV Modules Should Preferably No Longer Be Oriented to the South in the Near Future“. Energies 12, Nr. 23 (28.11.2019): 4528. http://dx.doi.org/10.3390/en12234528.

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PV modules tilted and oriented toward east and west directions gain gradually more importance as an alternative to the presently-preferred south (north in the Southern Hemisphere) orientation and it is shown to become economically superior even under the reimbursement of feed-in tariff (FIT). This is a consequence of the increasing spread between the decreasing costs of self-consumed solar power and the costs for power from the grid. One-minute values of irradiance were measured by silicon sensors at different orientations and tilt angles in Hannover (Germany) over three years. We show that south-oriented collectors give the highest electrical power during the day, whereas combinations of east and west orientations (E-W) result in the highest self-consumption rate (SC), and combinations of southeast and southwest (SE-SW) orientations result in the highest degree of autarky (AD), although they reduce the yearly PV Power by 5–6%. Moreover, the economic analysis of PV systems without FIT shows that the SE-SW and E-W combinations have the lowest electricity cost and they are more beneficial in terms of internal rate of return (IRR), compared to the S orientation at the same tilt. For PV systems with FIT, the S orientation presently provides the highest transfer of money from the supplier. However, as a consequence of the continuing decline of FIT, the economic advantage of S orientation is decreasing. E-W and SE-SW orientations are more beneficial for the owner as soon as FIT decreases to 7 Ct/kWh. East and west orientations of PV modules do not only have benefits for the individual owner but avoid high costs for storing energy—regardless who would own the storage facilities—and by avoiding high noon peaks of solar energy production during sunny periods, which would become an increasing problem for the grid if more solar power is installed. Furthermore, two types of commonly used PV software (PVSOL and PVsyst) were used to simulate the system performance. The comparison with measurements showed that both PV software underestimate SC and AD for all studied orientations, leading to the conclusion that improvements are necessary in modelling.
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Santos, Milton Cesar P., Mario Sarcinelli-Filhot, Alexandre S. Brandaot und Ricardo Carelli. „Un Controlador Basado en la Fusión de Controladores PVTOL para Navegación 3D de Vehículos Aéreos Autónomos“. Revista Tecnología y Ciencia, Nr. 36 (30.10.2019): 226–43. http://dx.doi.org/10.33414/rtyc.36.226-243.2019.

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En este trabajo se propone una arquitectura de control basada en la fusión de las acciones de control generadas por tres controladores sencillos (controladores PVTOL, del inglés Planar Vertical Take-Off and Landing) para guiar vehículos aéreos autónomos en posicionamiento y seguimiento de caminos 3D. Considerando la navegación como una tarea compuesta por el control de la orientación del vehículo en relación al blanco (asociada a un controlador Z-PVTOL), por el control de su movimiento hacia adelante (asociado a un controlador XZ-PVTOL), y por la corrección de cualquier desplazamiento lateral (asociada a un controlador YZ-PVTOL, similar al controlador XZ-PVTOL), nuestro primer abordaje consistió en ejecutar dichas maniobras parciales una por vez, utilizando los controladores PVTOL, conmutando de uno al otro mediante la acción de un supervisor. En este trabajo el abordaje se cambió, pasando a considerarse que los controladores PVTOL actúan simultáneamente y generando la acción de control final mediante la fusión de las acciones de control generadas por ellos, acoplando así suavemente tres controladores muy sencillos. Se presentan resultados experimentales para validar el abordaje propuesta, y su desempeño en vuelo es comparado con el desempeño correspondiente a la estrategia de conmutación.
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Lambert, Susan J., Jason B. Scott, Sarah J. Pethybridge und Frank S. Hay. „Strain Characterization of Potato virus S Isolates from Tasmania, Australia“. Plant Disease 96, Nr. 6 (Juni 2012): 813–19. http://dx.doi.org/10.1094/pdis-07-11-0573.

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Potato virus S (PVS) is prevalent within potato (Solanum tuberosum) production worldwide. Traditionally, PVS has been split into two strains, Ordinary (PVSO) and Andean (PVSA), based on reaction in herbaceous indicator species such as Chenopodium quinoa. However, recent research has identified further strain designations, such as PVSO-CS (Ordinary and Chenopodium systemic). Forty-four isolates of PVS were collected from potato seed lines in different geographical regions within Tasmania, Australia. Isolates were initially characterized by reactions in C. quinoa. Nineteen isolates were characterized as PVSO, based on the development of local lesions and serological detection in inoculated leaves only. Three isolates were identified as PVSA-like, based on local lesion development in inoculated leaves, mild mottling or chlorotic spots on noninoculated leaves, and serological detection in both inoculated and noninoculated leaves. Thirteen isolates produced no symptoms, and were detected serologically in inoculated leaves only (PVSO-like). Four isolates produced no symptoms but were detected serologically in both inoculated and noninoculated leaves (PVSA-like). Five isolates produced symptoms in inoculated leaves only but were detected serologically in both inoculated and noninoculated leaves (also PVSA-like). The ability of isolates to infect tomato has also been used as a criterion to assist in PVS strain differentiation. A subsample of isolates (n = 16) was unable to infect tomato ‘Grosse Lisse’. Seventeen isolates representative of these groupings based on reactions in C. quinoa were also characterized by coat-protein sequencing. Phylogenetic comparisons suggested that all isolates were PVSO rather than PVSA. Therefore, whereas some of these PVS isolates were systemic in C. quinoa, findings from this study suggest that they were not PVSA, and that only PVSO and PVSO-CS isolates are present in Tasmania. The implications of this finding for disease management are discussed.
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Van Jura, Josh, David Haines und Andrew Gemperline. „Use of Portable and Dynamic Variable Speed Limits in Construction Zones“. Transportation Research Record: Journal of the Transportation Research Board 2672, Nr. 16 (06.09.2018): 35–45. http://dx.doi.org/10.1177/0361198118794284.

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The Utah Department of Transportation (UDOT) implemented dynamic management of portable variable speed limit (PVSL) technology to reduce regulatory speed limits through an active work space (AWS). UDOT also developed and tested an intelligent system approach to alter speed limits in construction work zones. The goal of the PVSL system was to provide a portable and dynamic system that was easy for construction personnel to use to prudently reduce speeds within an AWS and make construction work zones safer for workers and the traveling public, while limiting the need to reduce speed throughout the AWS, rather than the entire construction work zone. This was achieved through temporary regulatory reductions in driver speeds within the immediate boundary of an AWS when workers were on site and exposed to the danger of errant vehicles during active construction. The system also raises speed limits when workers were not present. This PVSL system used a dynamic variable speed limit (VSL) algorithm to raise and lower the regulatory speed limits. The PVSL system also provided a queue warning algorithm that operated independent of the VSL algorithm to control messages posted on the portable variable message sign (PVMS) trailers to disseminate dynamic information to drivers. UDOT has completed 2 years of PVSL system deployment testing in four separate construction work zones to evaluate the effectiveness of the system. This paper highlights key elements that guided development of the PVSL system, along with the successful results from deployment of the system.
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Poletti, Sophia C., Elisabeth Michel und Thomas Hummel. „Olfactory Training Using Heavy and Light Weight Molecule Odors“. Perception 46, Nr. 3-4 (05.10.2016): 343–51. http://dx.doi.org/10.1177/0301006616672881.

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Background Repeated short-term exposure to odors is known to improve olfaction in patients with acquired olfactory dysfunction. The aim was to find out whether differences in molecular weight of odors used for olfactory training influences olfaction. We hypothesized a greater improvement following training with light weight molecule (LWM) odors. Methods A prospective study was performed in patients with posttraumatic (PTOL) and postviral olfactory loss (PVOL). Olfactory training was performed over a period of 5 months. One group ( n = 48) used four odors containing heavy weight molecules (HWM; >150 g/mol) and another ( n = 48) containing LWM (<150 g/mol). Olfaction was tested before and after the training using the Sniffin’ Sticks test. Results Olfactory training was associated with olfactory improvement, with the improvement in PVOL patients being three times greater than that seen in the PTOL group. Compared with LWM training, HWM training was associated with a significantly greater improvement in Phenyl Ethyl Alcohol (PEA) threshold scores in PVOL patients; however, no such improvement could be shown for other subtests or in PTOL patients. Conclusion Overall, training was associated with olfactory improvement. With the exception of threshold scores in PVOL, there were no significant differences between LWM and HWM groups.
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Randall, George K., und Alex Bishop. „A TEST OF THE OKLAHOMA INMATE FORGIVENESS AND WELL-BEING MODEL“. Innovation in Aging 3, Supplement_1 (November 2019): S359. http://dx.doi.org/10.1093/geroni/igz038.1305.

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Abstract Data was collected from older male offenders (N = 86 non-violent; N = 163 violent) incarcerated in Oklahoma. Testing a forgiveness model, positive evaluation of life PVOL was regressed on religiosity (REL) and forgiveness of self (FSelf), others (FOthers), and situation (FSit) using hierarchical OLS regression. Blocks of predictors included: a) age and education; b) religiosity; and c) FSelf, FOthers, and FSit. For the non-violent model of PVOL significant predictors included REL (β = .26, p ≤ .01) and FSelf (β = .40, p ≤ .01). For the violent offender model of PVOL significant predictors included REL (β = .31, p ≤ .001), FS (β = .21, p ≤ .01) and FSit (β = .33, p ≤ .001). Result indicate effects of REL and FSelf for both non-violent and violent offenders but a unique association of FSit for violent offenders. Implications for gerontological inquiry, practice, and policy are discussed.
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Dissertationen zum Thema "Pvsol"

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Hub, Michal. „Návrh fotovoltaické elektrárny s bateriovým úložištěm pro rodinný dům“. Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2021. http://www.nusl.cz/ntk/nusl-442441.

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This diploma thesis deals with the design of a photovoltaic power plant with a battery storage for a family house. In the theoretical part at first the principle of photovoltaic cells is analysed together with the various types used in this branch. Furthermore, the thesis deals with the description of photovoltaic systems and its individual parts consisting of inverters and accumulators. This thesis analyses the object for the installation of a photovoltaic power plant, including legislative and subsidy conditions. In the final part, itself system is analysed with a price proposal.
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Salazar, Amparo. „Commande d'objets volants miniatures : application à un avion à décollage et atterrissage vertical (PVTOL)“. Compiègne, 2005. http://www.theses.fr/2005COMP1553.

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Le travail de thèse porte d'une manière générale sur la commande d'engins volants ou d'hélicoptères miniatures. Le but est de développer de nouvelles stratégies de commande pour la stabilisation, le vol autonome des systèmes, mais aussi de s'intéresser à leur implémentation sur des prototypes réels. Dans un premier temps, on s'est intéressé à la commande d'un modèle réduit d'hélicoptère ou véhicule à décollage et atterrissage vertical se déplaçant dans un plan : PVTOL (Planar Vertical Take-Off and Landing) ou ADA V (Avion à Décollage et Atterrissage Vertical). Le PVTOL est un système simplifié qui a un nombre minimun d'états et d'entrées mais qui retient les caractéristiques principales nécessaires lorsqu'on réalise des lois de contrôle pour des aéronefs. Il représente également le mode longitudinal d'un hélicoptère. Le PVTOL a beaucoup intéressé la communauté d'Automatique par ses applications et son caractère non linéaire. Plusieurs lois de commande relativement simples basées sur des techniques de saturations emboîtées ont été proposées dans ce travail. Certaines stratégies respectent les bornes sur les entrées de commande. Une plate-forme expérimentale originale a été développée pour valider nos algorithmes de commande. Cette plate-forme est composée d'un prototype de l'avion PVTOL qui se déplace sur un plan incliné, plan qui définit l'espace de travail en deux dimensions, et aussi d'une caméra CCD utilisée comme capteur de position de l'engin. Dans une première étape et par simplicité, la caméra est placée à l'extérieur de l'avion, perpendiculaire au plan. Les mesures de la position et de l'orientation de l'objet sont obtenues de l'image donnée par la caméra. Nous avons utilisé une loi de commande simple pour stabiliser le système dans le but de simplifier les tests expérimentaux sur la plate-forme réelle. Cette loi de commande assure la convergence de l'état vers l'origine. L'étape suivante sera de placer la caméra à l'extérieur de l'avion pour estimer sa position et son orientation
The work of this thesis generally concerns the control of flying machines or miniature helicopters. The goal is to develop new control strategies for stabilization, autonomous flight of systems, but also to be interested in their implementation on real prototypes. Initially, we have been interested in the control of a small-scale model helicopter or a vertical takeoff vehicle moving on a plane : PVTOL (Planar Vertical Take-off and Landing) or ADAV (Avion à Décollage et Atterrissage Vertical). The PVTOL is a simplified system which has a minimun number of states and inputs but which retains many of the features that must be considered when designing controllaws for a real aircraft. It also represents the longitudinal mode of an helicopter. The PVTOL has interested the control community because of its applications and its nonlinear character. Relatively simple control laws based on techniques of nested saturations have been proposed in this work. These strategies respect the bounds on the control law inputs. An original experimental setup has been developed in order to validate our control algorithms. This experimental setup consists of a PVTOL aircraft prototype which moves on an inclined plane, which defines the workspace in two dimensions, and also of a CCD camera used as a position sensor. Initially and by simplicity, the camera has been placed outside and perpendicular to the plane. The position and the orientation have been obtained from the image given by the camera. We have used a simple control law for the stabilisation of the system, and in order to simplify the experimental tests on the real setup. This control law ensures the convergence of the state towards the origin
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Hably, Ahmad. „Approches bornées pour la commande des drones“. Phd thesis, Grenoble INPG, 2007. http://tel.archives-ouvertes.fr/tel-00235438.

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Les drones et les micro-drones font actuellement l'objet de développements très rapides. L'objectif principal de ce sujet de recherche est le développement de lois de commande permettant de contrôler deux systèmes sous actionnés classiques : l'avion à décollage et à atterrissage verticaux et le "quadrirotor" ou hélicoptère à quatre rotors fixes. La spécificité des approches développées est que les limites des actionneurs sont prises en compte tout en assurant un coût de calcul compatible avec une implantation et une exécution en temps réel sur un système informatique embarqué. La commande de l'assiette et de la position sont abordées dans ce travail. Les commandes proposées sont basées sur la stabilisation globale des chaînes d'intégrateurs linéaires et sur les techniques de commande prédictive rapide.
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Bonnet, Stéphane. „Approches numériques pour la commande des systèmes dynamiques“. Compiègne, 2008. http://www.theses.fr/2008COMP1745.

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Alors que la commande avancée repose en général sur la connaissance et l'utilisation d'un modèle analytique du système à piloter, l'idée de ce travail est d'utiliser pour la commande un modèle d'état numérique fourni sous forme d'une fonction de prédiction à un pas du comportement du système, au moyen d'algorithmes de commande prédictive appropriés. Ce modèle prend la forme d'une table qui, pour chaque condition initiale d'état et chaque entrée admissible prises dans un sous-ensemble discret des espaces continus correspondants, contient les valeurs de l'état et des sorties obtenues après un intervalle de temps fixé durant lequel on considère l'entrée comme constante. La structure de ce modèle permet de déterminer de manière efficace, à partir de la valeur courante de l'état du système, une prédiction de son état et de ses sorties en fonction de toute les entrées admissibles. Le choix de l'entrée appropriée pour le pas courant peut être déterminé en se donnant un objectif de sortie fixé. En particulier, on s'intéresse ici à obtenir des sorties du système un comportement dynamique équivalent à celui d'un système linéaire de référence. Le problème de commande est alors de trouver l'entrée qui minimise la distance des sorties prédites du système piloté et du système linéaire à chaque pas. L'algorithme de contrôle proposé met en oeuvre ce schéma de commande prédictive de façon à limiter au plus la quantité de calculs nécessaires, en considérant le modèle tabulé comme une approximation d'une fonction de prédiction continue représentée sous forme d'un interpolateur linéaire et en résolvant le problème d'optimisation de manière approchée par des algorithmes numériques de descente spécifiques. Deux applications de ce schéma sont proposées. D'abord, une expérimentation réelle sur une suspension magnétique de laboratoire permet de montrer son applicabilité à des systèmes électromécaniques rapides à entrée unique ainsi que sa robustesse vis-à-vis des perturbations et erreurs de modèle. Ensuite, des simulations sur un système à entrées multiples de type “PVTOL” montrent qu'il est possible de le généraliser à des systèmes plus complexes
While advanced control schemes are generally based upon the knowledge of an analytical plant model, the idea developed here is to use instead a numerical state-space model, given as a one-step prediction function of the dynamical behavior of the system, and suitable predictive control algorithms to perform the control task. That model is lookuptable-based. The table contains, for each initial state condition and admissible control input, both taken from discrete subspaces of the corresponding continuous state and input spaces of the plant, the output and state values obtained from a constant control after one time-step. Using that model and knowing the current state of the system, a prediction of its state and outputs as a function of possible inputs can be efficiently computed. If a given output objective for the next time-step is known, the appropriate control inputs can be computed. Here, the output objective is build so that the plant outputs follow a dynamical behavior similar to that of a given reference linear system. The control problem is then to find the inputs minimizing for the next step the distance between that objective and the predicted plant outputs. The proposed predictive control algorithm implements that control scheme while focusing on minimizing the computing effort needed. This is achieved by building a linear interpolator-based approximation of the prediction function from the lookup-table data and by approximately solving the minimization problem through specific and efficient descent-based numerical algorithms. Two applications of this scheme are carried out. The first one is a real-life experiment, applied to a laboratory active magnetic bearing where each axis is considered independently, showing the scheme correctly lends itself to the control of fast electromechanical systems and that it is robust towards perturbations and model errors. The second application deals with the stabilization of a simulated multiple-input “PVTOL”-type aircraft, showing the algorithm can be generalized to more complex systems
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Wood, Rohin. „Lyapunov-based control strategies for the global control of symmetric VTOL UAVs“. 2007. http://hdl.handle.net/2440/59390.

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The last decade has seen significant advances in the development of Vertical takeoff and landing (VTOL) unmanned aerial vehicles (UAVs). The emergence of enabling technologies, in addition to the practical usefulness of such systems has driven their development to a point where numerous technology demonstrators and commercial products are now in existence. Of particular interest has been the development of small scale, VTOL UAVs commonly referred to as mini and micro-VTOL UAVs. The versatility and agility of such vehicles offers great potential for the use in clustered, urban environments. Despite recent advancements, the autonomous navigation of VTOL UAVs remains a very challenging research area. The dynamics of VTOL UAVs are heavily nonlinear, underactuated and non-minimum phase. This, coupled with the aggressive maneuvers that such vehicles are expected to execute provides a stimulating problem in dynamic control. This is particularly true in the case of micro-VTOL UAVs. The fast, nonlinear nature of these systems render classical, linear control approaches inadequate. The past twenty years has seen great interest in the development of nonlinear control strategies. This has led to the emergence of a number of standard design tools, most notably feedback linearisation and Lyapunov-based, backstepping approaches. Such design techniques offer a framework for the derivation of model based control laws capable of achieving global stabilisation and trajectory tracking control for heavily nonlinear systems. Recently, there has been significant interest in the application of such nonlinear control paradigms for the stabilisation and control of VTOL UAVs. The aim of this thesis is to further the application and analysis of nonlinear control design techniques for the control of VTOL UAVs. In particular, focus is placed on Lyapunov-based, backstepping-type control approaches. The first half of this thesis investigates Lyapunov-based control strategies that cast the closed-loop VTOL dynamics into a globally stable, cascade structure. This work was directly inspired by, and builds on, a variety of previously published works. Firstly, an alternative design approach to that previously published is presented, resulting in an improved closed-loop dynamic structure. Although inspired by the VTOL system, this idea may be generalised for the control of a broad class of systems, and is presented as such. A singularity issue arising in the cascade control of VTOL vehicles is then investigated, and a novel approach to overcome this issue is formulated. The second half of this thesis is dedicated to the trajectory tracking control of VTOL UAVs at velocities where the influence of aerodynamics is significant. In general, the aerodynamic models of VTOL UAVs are heavily nonlinear and poorly known. The use of such models in a backstepping framework that uses explicit differentiation of these models for dynamic inversion is questioned, due to the potential sensitivity of such nonlinear models. Consequently, an alternative approach utilising coupled filters to avoid such sensitivity issues is proposed. All control designs formulated in this thesis are accompanied by proofs guaranteeing their global stability, and numerical simulations demonstrating their time domain response characteristics.
http://library.adelaide.edu.au/cgi-bin/Pwebrecon.cgi?BBID=1298413
Thesis (Ph.D.) -- University of Adelaide, School of Mechanical Engineering, 2007
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Buchteile zum Thema "Pvsol"

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Fantoni, Isabelle, und Rogelio Lozano. „The PVTOL aircraft“. In Non-linear Control for Underactuated Mechanical Systems, 173–94. London: Springer London, 2002. http://dx.doi.org/10.1007/978-1-4471-0177-2_12.

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Fantoni, Isabelle, und Amparo Palomino. „Nested Saturation Control for Stabilizing the PVTOL Aircraft“. In Unmanned Aerial Vehicles, 21–40. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118599938.ch2.

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Xu, Xinli, und Chunwei Zhang. „Cascade ADRC Based Fault-Tolerant Control for a Hovering PVTOL Aircraft“. In Robotics and Mechatronics, 239–49. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-17677-8_19.

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Torres, César Martínez, Luis Humberto Rodríguez Alfaro, Efrain Alcorta Garcia, Gerardo Romero Galvan und David Lara. „Lagrangian Model‐Based Fault Diagnosis in a PVTOL“. In Lagrangian Mechanics. InTech, 2017. http://dx.doi.org/10.5772/66395.

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Konferenzberichte zum Thema "Pvsol"

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Pushpavalli, M., P. Abirami, P. Sivagami und V. Geetha. „Investigation of Grid Connected PV System with Electrial Appliances, Electric Vehicles and Battery Systems using PVsol Software“. In Proceedings of the Fist International Conference on Advanced Scientific Innovation in Science, Engineering and Technology, ICASISET 2020, 16-17 May 2020, Chennai, India. EAI, 2021. http://dx.doi.org/10.4108/eai.16-5-2020.2304108.

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2

Zhang, Yunfan, Donghai Li, Dazhong Lao, Yong Su und Renming Bai. „TC on PVTOL“. In 2012 10th World Congress on Intelligent Control and Automation (WCICA 2012). IEEE, 2012. http://dx.doi.org/10.1109/wcica.2012.6358232.

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3

Aguilar-Ibanez, Carlos, Humberto Sossa-Azuela und Miguel S. Suarez-Castanon. „PVTOL Control: A Backstepping Approach“. In 2015 International Conference on Mechatronics, Electronics and Automotive Engineering (ICMEAE). IEEE, 2015. http://dx.doi.org/10.1109/icmeae.2015.44.

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4

Turker, T., T. Oflaz, H. Gorgun und G. Cansever. „A stabilizing controller for PVTOL aircraft“. In 2012 American Control Conference - ACC 2012. IEEE, 2012. http://dx.doi.org/10.1109/acc.2012.6314818.

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5

Popov, Alexander, Boris Andrievsky und Iuliia Zaitceva. „Stabilization of PVTOL aircraft by supertwisting algorithms“. In 2015 International Workshop on Recent Advances in Sliding Modes (RASM 2015). IEEE, 2015. http://dx.doi.org/10.1109/rasm.2015.7154645.

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6

Offermann, A., P. Castillo und J. De Miras. „Control of a PVTOL* with tilting rotors*“. In 2019 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE, 2019. http://dx.doi.org/10.1109/icuas.2019.8798341.

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7

Venkatesh, Ch, R. Mehra, Faruk Kazi und N. M. Singh. „Passivity based controller for underactuated PVTOL system“. In 2013 IEEE International Conference on Electronics, Computing and Communication Technologies (CONECCT). IEEE, 2013. http://dx.doi.org/10.1109/conecct.2013.6469304.

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8

Salazar, Sergio, Jonathan Flores und Rogelio Lozano. „Non-Linear Control for PVTOL Without Algebraic Restrictions“. In 2019 16th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE). IEEE, 2019. http://dx.doi.org/10.1109/iceee.2019.8884526.

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9

Ikeda, Ryoya, Takuya Hayashi und Hisakazu Nakamura. „Global Stabilization for PVTOL System via Minimum Projection Method“. In IECON 2019 - 45th Annual Conference of the IEEE Industrial Electronics Society. IEEE, 2019. http://dx.doi.org/10.1109/iecon.2019.8926765.

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10

Gruszka, Aleksandra, Michael Malisoff und Frederic Mazenc. „On tracking for the PVTOL model with bounded feedbacks“. In 2011 American Control Conference. IEEE, 2011. http://dx.doi.org/10.1109/acc.2011.5990817.

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