Fladan kartoitus modernein kartoitusmenetelmin

Tässä tutkimuksessa on selvitetty erilaisten kartoitusmenetelmien käytettävyyttä luonnonoloiltaan erilaisten fladojen kartoituksessa. Kartoitusmenetelminä käytettiin kauko-ohjattavaa pienoisvenettä, johon oli kiinnitetty kaikuluotain, VRS-GPS sekä GPS; UAV- helikopteria, joka otti ilmakuvia; sekä kasvillisuuslinjoja, joiden tietoja verrattiin ilmakuviin. Syvyyden kartoittamiseen käytettiin ajoittain myös teleskooppivarrella ohjattavaa kelluvaa lauttaa, johon oli kiinnitetty kaikuluotain, VRS-GPS ja GPS. VRS-GPS mittasi kaikuluotaimen sijaintipisteet ja GPS:n sijaintitietoja käytettiin aineiston aikaleimana. Tutkimusfladat sijaitsivat Varsinais-Suomessa, Pohjanmaalla ja Pohjois-Pohjanmaalla. Kartoitusmenetelmien käytettävyys vaihteli tutkimusfladoilla. Kauko-ohjattava pienoisvene toimi kohtuullisesti kaikilla tutkimusfladoilla ja nopeutti syvyyskartoitusta huomattavasti. Runsas kivikkoisuus ja kasvillisuus kuitenkin vaikeuttivat tai jopa estivät kartoituksen joissain osissa fladaa. Kaikuluotaamalla saaduista syvyystiedoista tehtiin interpoloimalla syvyyskartta. UAV-ilmakuvaus toimi menetelmänä, mutta esimerkiksi veden kirkkaudella on suuri merkitys niiden monipuoliseen käyttöön. Kasvillisuuslinjoista saadaan tärkeää tietoa lajistosta. Kasvillisuuslinjoja verrattiin myös UAV-ilmakuvissa havaittavaan kasvillisuuteen. UAV-ilmakuvista ei ollut mahdollista havaita vedenalaista kasvillisuutta riittävän tarkasti. Tutkimuksessa on selvitetty fladojen nykytilaa. Nykytilan selvityksessä pyrittiin tutkimaan fladan syvyysjakaumaa luodun syvyyskartan avulla, kasvillisuutta sekä fladan morfologista ja kasvillista vaihetta. Fladan morfologiaa ja kasvillisuutta verrattiin jo olemassa oleviin teorioihin ja malleihin fladan kehityskaaresta. Tutkimusfladojen nykyinen kehitysvaihe oli selkeästi erotettavissa vaiheista fladan esiaste – flada – kluuviflada – flada. Ne pystyttiin kohtalaisesti sijoittamaan myös Munsterhjelmin (1997) Tammisaaren saaristossa flada-luokitteluun. Vaikka tutkimusfladojen morfologinen kehitysvaihe oli selkeä, niiden kasvillisuus ei yleensä vastannut morfologiselle vaiheelle tyypillistä kasvillisuutta. Niiden kasvillisuus oli myös ristiriidassa morfologisen vaiheen kanssa. Voitiin havaita, että morfologinen samankaltaisuus ei vaikuttanut löydettyyn lajistoon.

Estrategia de intervención militar de Estados Unidos en Medio Oriente: dinámicas y consecuencias del uso de drones en Yemen y Pakistán entre 2009 a 2013

Este es un estudio sobre la estrategia de guerra estadounidense en Medio Oriente basada en el uso sistemático de drones durante el periodo comprendido entre 2009 y 2013. Se busca explicar de qué manera puede considerarse el uso de este tipo de armamento como una práctica basada en la proyección de poder sin mayor vulnerabilidad. Los casos de Pakistán y Yemen son abordados, ya que evidencian las características de las operaciones selectivas por las que ha abogado el Presidente Obama. El estudio se inscribe dentro del realismo ofensivo, haciendo también referencia a sus limitaciones explicativas. Empero, se afirma que las dinámicas y consecuencias de la utilización de drones son intrínsecas a la necesidad estadounidense de combatir actores no estatales mediante prácticas que garanticen su seguridad y pretensiones hegemónicas a pesar de las implicaciones políticas , legales y sociales en las que puede incurrir.

Criação de uma estação de testes para um micro-helicóptero autónomo

Os UAV (Unmaned Air Vehicles) têm sido cada vez mais utilizados em vários ramos, como a geologia, a segurança pública, a robótica e na obtenção de imagens. Visto existir grande interesse no uso do equipamento, foi comprado um quadcopter com o objetivo poder tornálo o mais autónomo possível. Esta tese contém informações dos elementos utilizados nesse Arducopter e ainda a informação dos sensores que podem ser adaptados ao mesmo. Explica também como está estruturado todo o código e como o UAV pode ser configurado antes do voo. São também apresentados todos os resultados obtidos dos primeiros voos e as evoluções e alterações após cada teste.

Controle de atitude e altitude para um veículo aéreo não tripulado do tipo quadrirrotor

A Quadrotor is an Unmanned Aerial Vehicle (UAV) equipped with four rotors distributed on a simple mechanical "X"form structure. The aim of this work is to build and stabilize a Quadrotor aircraft in the roll, pitch and yaw angles at a certain altitude. The stabilization control approach is based on a transformation in the input variables in order to perform a decoupled control. The proposed strategy is based on breaking the control problem into two hierarchical levels: A lower level, object of this work, maintains the desired altitude an angles of the vehicle while the higher level establishes appropriate references to the lower level, performing the desired movements. A hardware and software architecture was specially developed and implemented for an experimental prototype used to test and validate the proposed control approach

Sistema de supervisão aérea baseado em navegação visual para detecção de anomalias em instalações de petróleo e gás

This work deals with the development of a prototype of a helicopter quadrotor for monitoring applications in oil facilities. Anomaly detection problems can be resolved through monitoringmissions performed by a suitably instrumented quadrotor, i.e. infrared thermosensors should be embedded. The proposed monitoring system aims to reduce accidents as well as to make possible the use of non-destructive techniques for detection and location of leaks caused by corrosion. To this end, the implementation of a prototype, its stabilization and a navigation strategy have been proposed. The control strategy is based on dividing the problem into two control hierarchical levels: the lower level stabilizes the angles and the altitude of the vehicle at the desired values, while the higher one provide appropriate references signals to the lower level in order the quadrotor performs the desired movements. The navigation strategy for helicopter quadrotor is made using information provided by a acquisition image system (monocular camera) embedded onto the helicopter. Considering that the low-level control has been solved, the proposed vision-based navigation technique treats the problem as high level control strategies, such as, relative position control, trajectory generation and trajectory tracking. For the position control we use a control technique for visual servoing based on image features. The trajectory generation is done in a offline step, which is a visual trajectory composed of a sequence of images. For the trajectory tracking problem is proposed a control strategy by continuous servovision, thus enabling a navigation strategy without metric maps. Simulation and experimental results are presented to validate the proposal

Controle de posição com restrição à orientação de um Veículo Aéreo Não-Tripulado tipo Quadrirrotor

Quadrotors aircraft are composed by four propellers mounted on four engines on a cross or x disposition, and, in this structure, the engines on the same arm spin in the same direction and the other arm in the opposite direction. By rotating each helix generates vertical upward thrust. The control is done by varying the rotational speed of each motor. Among the advantages of this type of vehicle can cite the mechanical simplicity of construction, the high degree of maneuverability and the ability to have vertical takeoffs and landings. The modeling and control of quadrirrotores have been a challenge due to problems such as nonlinearity and coupling between variables. Several strategies have been developed to control this type of vehicle, from the classical control to modern. There are air surveillance applications where a camera is fixed on the vehicle to point forward, where it is desired that the quadrotor moves at a fixed altitude toward the target also pointing forward, which imposes an artificial constraint motion, because it is not desired that it moves laterally, but only forwards or backwards and around its axes . This restriction is similar to the naturally existing on robots powered by wheels with differential drive, which also can not move laterally, due to the friction of the wheels. Therefore, a position control strategy similar to that used in this type of robot could be adapted for aerial robots like quadrotor. This dissertation presents and discusses some strategies for the control of position and orientation of quadrotors found in the literature and proposes a strategy based on dynamic control of mobile robots with differential drive, called the variable reference control. The validity of the proposed strategy is demonstrated through computer simulations

Improvement and evaluation of the MS2SV for mixed systems design described in abstraction high level

This paper presents an important improvement of the MS2SV tool. The MS2SV performs the translation of mixed systems developed in MATLAB / Simulink for a structural or behavioral description in VHDL-AMS. Previously, the MS2SV translated only models of the LIB MS2SV library. This improvement allows designer to create your own library to translation. As case study was used a rudder controller employed in an unmanned aerial vehicle. For comparison with the original model the VHDL-AMS code obtained by the translation was simulated in SystemVision environment. The results proved the efficiency of the tool using the translation improvement proposed in this paper.

Um mecanismo para realçar a conectividade de roteamento geográfico na transmissão multimídia em VANTs

As redes de Veículos Aéreos Não Tripulados (VANTs) têm potencializado o uso de aplicações multimídia devido ao seu elevado grau de mobilidade e versatilidade. Esse crescimento ocorre pela facilidade de acesso e utilização dos VANTs quadricópteros em diversas aplicações civis. As aplicações civis têm como característica principal o uso de dados multimídia, como vídeos, por oferecerem uma perspectiva visual mais detalhada do ambiente. A transmissão desse tipo de dado nas redes VANTs por meio de protocolos geográ cos melhora a taxa de entrega de dados. Entretanto, ela ainda não é su ciente para prover qualidade de experiência (QoE). Isso ocorre devido ao elevado grau de mobilidade dos quadricópteros que ocasiona quebras de enlace durante a transmissão multimídia. Por consequência, ela prejudica a conectividade e induz a altas perdas de pacotes e atrasos. Então, este trabalho propõe um mecanismo, chamado RCRV, com base em técnicas de predição de mobilidade em termos de posicionamento e da estimativa do tempo de enlace para realçar a tomada de decisão de roteamento em protocolos geográ cos. Além disso, ele utiliza critérios que consideram os comportamentos de mobilidade dos VANTs. Assim, o RCRV possibilita o prolongamento da conectividade nas redes VANTs. O RCRV é um mecanismo que complementa as estratégias de roteamento dos protocolos geográ cos. Desse modo, adicionou-se o RCRV ao protocolo GPSR a m de avaliar os ganhos e benefícios do mecanismo em um protocolo de roteamento geográ co. Simulações foram realizadas com diferentes velocidades e números de VANTs. Os resultados mostraram que o RCRV aumenta a conectividade da transmissão, melhorando a entrega do conteúdo multimídia e a qualidade do vídeo observado pelo usuário.

Acurácia da mosaicagem gerada por veículo aéreo não tripulado utilizado na agricultura de precisão

The need for unmanned aerial vehicle (UAV) is a Brazilian reality in the worlds agricultural, once they have models penetrating the market with agrictural purpose. After processing, the images collected by a UAV can generate a mosaic of the study area. For making and georeferencing the mosaic, can be deployed or not ground control points. Thus, the study aimed to compare a mosaic with ground control points and without ground control points generated from images collected by a UAV used primarily for agricultural purposes. The results showed that the quality in the determination of areas and perimeters no presented significant difference with or without the use of ground control points. The mosaic generated without ground control points obtained an average error of 23.7% of the pixel size; with ground control points, the average error was 10.6%, providing an improvement of approximately 50%. Planimetric and altimetric errors, with respect to the ground control points, for the controlled mosaic, reached the order of decimeters, with planimetric accuracy of 12.8 cm, a result considered satisfactory taking into account mainly the purpose of assessed UAV

Identificação de bandas espectrais para detecção de cultura de cana-de-açúcar sadia e doente utilizando câmara hiperespectral embarcada em VANT

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Caracterização espectral de espécies de Mata Atlântica de Interior em nível foliar e de copa

Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)

Simulações empregando a decomposição de Adomian para resolver as equações da dinâmica de voo de quadrotores

Pós-graduação em Ciência da Computação - IBILCE

Montagem e avaliação de um sistema de varredura a LASER embarcado em VANT

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Montagem e avaliação de um sistema de varredura a LASER embarcado em VANT

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

In-Flight Collision Avoidance Controller Based Only on OS4 Embedded Sensors

The major goal of this research was the development and implementation of a control system able to avoid collisions during the flight for a mini-quadrotor helicopter, based only on its embedded sensors without changing the environment. However, it is important to highlight that the design aspects must be seriously considered in order to overcome hardware limitations and achieve control simplification. The controllers of a UAV (Unmanned Aerial Vehicle) robot deal with highly unstable dynamics and strong axes coupling. Furthermore, any additional embedded sensor increases the robot total weight and therefore, decreases its operating time. The best balance between embedded electronics and robot operating time is desired. This paper focuses not only on the development and implementation of a collision avoidance controller for a mini-robotic helicopter using only its embedded sensors, but also on the mathematical model that was essential for the controller developing phases. Based on this model we carried out the development of a simulation tool based on MatLab/Simulink that was fundamental for setting the controllers' parameters. This tool allowed us to simulate and improve the OS4 controllers in different modeled environments and test different approaches. After that, the controllers were embedded in the real robot and the results proved to be very robust and feasible. In addition to this, the controller has the advantage of being compatible with future path planners that we are developing.