999 resultados para Guidance and special necessities
Resumo:
Guidance and Diversity, for the majority of the European countries and North America , are related to the attention to children and young people with special necessities, that are attend in an educative institution and for those who are elaborated educative programs directed to obtain one better adaptation to the prevailing social system. In most of the cases is considered that the problematic of the special necessities is imputable to genetic or personal factors that only respond to internal factors to the individuals that display them avoiding the external factors that in some cases can be more decisive determinants at the time of the conductual manifestation. In this work is pleaded because the professionals of the Guidance, as much private or public scenes of the European countries, make more specific considerations at the time of taking care of children, young people and adults, as immigrants, coming of Latin America . In an ample sense one sets out to make Guidance in the Diversity more than Guidance for the Diversity under the conception of a Guidance for All which implies the elimination of the expression "special necessities", whose connotation in our countries is not most appropriate, and than it includes the idea of an Ethnic Guidance. Perhaps the best way of boarding of these conceptions is promoting a process of Guidance from the School and not only in the School.
Resumo:
Guidance and Diversity, for the majority of the European countries and North America , are related to the attention to children and young people with special necessities, that are attend in an educative institution and for those who are elaborated educative programs directed to obtain one better adaptation to the prevailing social system. In most of the cases is considered that the problematic of the special necessities is imputable to genetic or personal factors that only respond to internal factors to the individuals that display them avoiding the external factors that in some cases can be more decisive determinants at the time of the conductual manifestation. In this work is pleaded because the professionals of the Guidance, as much private or public scenes of the European countries, make more specific considerations at the time of taking care of children, young people and adults, as immigrants, coming of Latin America . In an ample sense one sets out to make Guidance in the Diversity more than Guidance for the Diversity under the conception of a Guidance for All which implies the elimination of the expression "special necessities", whose connotation in our countries is not most appropriate, and than it includes the idea of an Ethnic Guidance. Perhaps the best way of boarding of these conceptions is promoting a process of Guidance from the School and not only in the School.
Resumo:
Guidance and Diversity, for the majority of the European countries and North America , are related to the attention to children and young people with special necessities, that are attend in an educative institution and for those who are elaborated educative programs directed to obtain one better adaptation to the prevailing social system. In most of the cases is considered that the problematic of the special necessities is imputable to genetic or personal factors that only respond to internal factors to the individuals that display them avoiding the external factors that in some cases can be more decisive determinants at the time of the conductual manifestation. In this work is pleaded because the professionals of the Guidance, as much private or public scenes of the European countries, make more specific considerations at the time of taking care of children, young people and adults, as immigrants, coming of Latin America . In an ample sense one sets out to make Guidance in the Diversity more than Guidance for the Diversity under the conception of a Guidance for All which implies the elimination of the expression "special necessities", whose connotation in our countries is not most appropriate, and than it includes the idea of an Ethnic Guidance. Perhaps the best way of boarding of these conceptions is promoting a process of Guidance from the School and not only in the School.
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"Education is everyone's future."
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Includes index.
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"This manual supersedes TM 9-1430-495-34P, 28 June 1983"--P. [i]
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Includes index.
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"Mounting kit M241E5 1450-00-078-1217 accessory kit M219E1 1450-00-179-5317 accessory kit M218E1 1450-00-179-5318 mounting kit M184 1450-00-179-6095 Pershing 1a Field Artillery Missile System.
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The main focus of this paper is on the motion planning problem for an under-actuated, submerged, Omni-directional autonomous vehicle. Underactuation is extremely important to consider in ocean research and exploration. Battery failure, actuator malfunction and electronic shorts are a few reasons that may cause the vehicle to lose direct control of one or more degrees-of-freedom. Underactuation is also critical to understand when designing vehicles for specific tasks, such as torpedo-shaped vehicles. An under-actuated vehicle is less controllable, and hence, the motion planning problem is more difficult. Here, we present techniques based on geometric control to provide solutions to the under-actuated motion planning problem for a submerged underwater vehicle. Our results are validated with experiments.
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Maintaining the ecosystem is one of the main concerns in this modern age. With the fear of ever-increasing global warming, the UK is one of the key players to participate actively in taking measures to slow down at least its phenomenal rate. As an ingredient to this process, the Springer vehicle was designed and developed for environmental monitoring and pollutant tracking. This special issue paper highlighted the Springer hardware and software architecture including various navigational sensors, a speed controller, and an environmental monitoring unit. In addition, details regarding the modelling of the vessel were outlined based mainly on experimental data. The formulation of a fault tolerant multi-sensor data fusion technique was also presented. Moreover, control strategy based on a linear quadratic Gaussian controller was developed and simulated on the Springer model.
Gaussian controller is developed and simulated on the Springer model.
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This research project set out to explore Unitary Authority (UA) involvement in festivals and special events across Wales. It considers the level and nature of UA involvement and investigates activity by event purpose; reasons for, and characteristics of, UA engagement; and, crucially, the extent and nature of event evaluation. The study’s aim was to begin the development of a baseline of information for further research into the growing use of festivals and special events as a strategy for local economic development in Wales. A quantitative survey approach facilitated a comprehensive snapshot of UA responses whilst also incorporating discursive elements. A telephone survey was designed and undertaken with representatives of all 22 UA departments responsible for festivals and events in Wales. The research reveals a significant level of festival and special event activity across Wales, supported primarily for its perceived socio-cultural value. However, evaluation would appear to be focused on improving processes and measuring economic outputs rather than assessing whether socio-cultural objectives are being achieved. Whilst overwhelmingly positive about efforts to improve approaches to evaluation, respondents held clear views about the complications most likely to hamper any such efforts. These responses focused upon the need for flexibility, cost effectiveness and comparability across festival and special event typologies.
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The author undertook a qualitative and quantitative survey of 130 guidance counsellors and primary school principles focusing on perceptions of what school guidance and counselling will be like in 25 years. Generally the participants held similar beliefs and were bullish about employment prospects.
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A forced landing is an unscheduled event in flight requiring an emergency landing, and is most commonly attributed to engine failure, failure of avionics or adverse weather. Since the ability to conduct a successful forced landing is the primary indicator for safety in the aviation industry, automating this capability for unmanned aerial vehicles (UAVs) will help facilitate their integration into, and subsequent routine operations over civilian airspace. Currently, there is no commercial system available to perform this task; however, a team at the Australian Research Centre for Aerospace Automation (ARCAA) is working towards developing such an automated forced landing system. This system, codenamed Flight Guardian, will operate onboard the aircraft and use machine vision for site identification, artificial intelligence for data assessment and evaluation, and path planning, guidance and control techniques to actualize the landing. This thesis focuses on research specific to the third category, and presents the design, testing and evaluation of a Trajectory Generation and Guidance System (TGGS) that navigates the aircraft to land at a chosen site, following an engine failure. Firstly, two algorithms are developed that adapts manned aircraft forced landing techniques to suit the UAV planning problem. Algorithm 1 allows the UAV to select a route (from a library) based on a fixed glide range and the ambient wind conditions, while Algorithm 2 uses a series of adjustable waypoints to cater for changing winds. A comparison of both algorithms in over 200 simulated forced landings found that using Algorithm 2, twice as many landings were within the designated area, with an average lateral miss distance of 200 m at the aimpoint. These results present a baseline for further refinements to the planning algorithms. A significant contribution is seen in the design of the 3-D Dubins Curves planning algorithm, which extends the elementary concepts underlying 2-D Dubins paths to account for powerless flight in three dimensions. This has also resulted in the development of new methods in testing for path traversability, in losing excess altitude, and in the actual path formation to ensure aircraft stability. Simulations using this algorithm have demonstrated lateral and vertical miss distances of under 20 m at the approach point, in wind speeds of up to 9 m/s. This is greater than a tenfold improvement on Algorithm 2 and emulates the performance of manned, powered aircraft. The lateral guidance algorithm originally developed by Park, Deyst, and How (2007) is enhanced to include wind information in the guidance logic. A simple assumption is also made that reduces the complexity of the algorithm in following a circular path, yet without sacrificing performance. Finally, a specific method of supplying the correct turning direction is also used. Simulations have shown that this new algorithm, named the Enhanced Nonlinear Guidance (ENG) algorithm, performs much better in changing winds, with cross-track errors at the approach point within 2 m, compared to over 10 m using Park's algorithm. A fourth contribution is made in designing the Flight Path Following Guidance (FPFG) algorithm, which uses path angle calculations and the MacCready theory to determine the optimal speed to fly in winds. This algorithm also uses proportional integral- derivative (PID) gain schedules to finely tune the tracking accuracies, and has demonstrated in simulation vertical miss distances of under 2 m in changing winds. A fifth contribution is made in designing the Modified Proportional Navigation (MPN) algorithm, which uses principles from proportional navigation and the ENG algorithm, as well as methods specifically its own, to calculate the required pitch to fly. This algorithm is robust to wind changes, and is easily adaptable to any aircraft type. Tracking accuracies obtained with this algorithm are also comparable to those obtained using the FPFG algorithm. For all three preceding guidance algorithms, a novel method utilising the geometric and time relationship between aircraft and path is also employed to ensure that the aircraft is still able to track the desired path to completion in strong winds, while remaining stabilised. Finally, a derived contribution is made in modifying the 3-D Dubins Curves algorithm to suit helicopter flight dynamics. This modification allows a helicopter to autonomously track both stationary and moving targets in flight, and is highly advantageous for applications such as traffic surveillance, police pursuit, security or payload delivery. Each of these achievements serves to enhance the on-board autonomy and safety of a UAV, which in turn will help facilitate the integration of UAVs into civilian airspace for a wider appreciation of the good that they can provide. The automated UAV forced landing planning and guidance strategies presented in this thesis will allow the progression of this technology from the design and developmental stages, through to a prototype system that can demonstrate its effectiveness to the UAV research and operations community.