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Decision Optimization of Machine Sets Taking Into Consideration Logical Tree Minimization of Design Guidelines

Dynamic Simulation in the Development of Construction Machinery. - The Eighth Scandinavian International Conference on Fluid Power, vol.1, pp.651-667. Francis J. and Betts P.L. (1997): Modelling incompressible flow in a pressure relief valve. - Proceedings of the Institution of Mechanical Engineers, Part E: Journal of Process Mechanical Engineering, vol.211, No.2, pp.83-93. Giergiel J. (1990): Identification of Mechanical Systems. - Warsaw: PWN. Kurowski W. (2001): Modelling technical objects. - Manuscript Development

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The Matlab Toolbox for Modeling Complex Mechanisms

. Li K., Chen I., Yeo S.H. and Lim Ch.K. (2011): Development of finger-motion capturing device based on optical linear encoder. - Journal of Rehabilitation Research & Development, vol.48, No.1, pp.69-82. Kucuk S. and Bingul Z. (2010): An off-line robot simulation toolbox. - Computer Application in Engineering Education, 18, pp.41-52, DOI 10.1002/cae.20236. Legnani G. (2006): SPACELIB: a software library for the Kinematic and dynamic analysis of systems of rigid bodies. - U. di Brescia. http://www.ing.unibs.it/~glegnani/ López-Nicolás G

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Methods for Determining the Take-off Speed of Launchers for Unmanned Aerial Vehicles

Abstract

Unmanned aerial vehicles (UAV) are currently a very rapidly developing type of aviation. The problem of support during the take-off with the use of, i.e. take-off launchers arose along with their development, especially for UAVs with weights and dimensions preventing manual take-off. One of the major issues associated with UAV take-off launchers is for its UAV accelerating element to obtain its initial speed. The article presents three methods of determining launcher take-off speeds for unmanned aerial vehicles, i.e. the concentrated very oblique projection method, the high-speed camera methods, and the acceleration recorder method. The take-off launcher carriage speed in the oblique projection method is determined from a formula. This method involves “ejections” of concentrated masses from the UAV mass range and measuring the component values resulting from the used formula, which contains the range of the oblique projection, the elevation of the projection and its angle. The method using the high-speed camera involves recording the course of ejections of the concentrated mass from the launcher. The average take-off speed is determined on the basis of a take-off run length (section of the launcher race, where the unit accelerates) and defining the start and end frame of the carriage movement. The third method for the determination of the take-off speed utilizes an acceleration recorder. The method with the recorder involves registering a change in the accelerations when the take-off carriage is being accelerated by a system fixed on the carriage or the accelerated object. The article presents the methodology of dynamic tests of object acceleration on a launcher, necessary for the determination of speed with the mentioned methods. Selected results from actual tests with the use of the 01/WS/2015 launcher, which is an element of the ZOCP JET2 set, were presented. The test results are presented in a tabular form. The methods for the determination of the take-off speed were compared on the basis of performed tests. Based on the obtained results, the factors impacting the accuracy of each of the methods were identified.

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Assessment Method of End-of-Life Vehicles Recycling Network Efficiency

, S., Thomas, J., Economies of scale and scope: a cost analysis of municipal solid waste services , Land economics, Vol. 77 (4), pp. 548-560, 2001. [5] Chavez, A. P., Armijo de Vega, C., Benitez, S. O., Measuring Progress of Waste Management Programs , International Journal of Environmental Science and Development, Vol. 2 (5), pp. 372-376, 2011. [6] DG Environment A study to examine the benefits of the End of Life Vehicles Directive and the costs and benefits of a revision of the 2015 targets for recycling, re-use and recovery under the ELV Directive

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Evaluation of properties of concrete incorporating ash as mineral admixtures

European Cement Association, 2011. [5] WBCSD&IEA (World Business Council for Sustainable Development & International Energy Agency). Cement Technology Roadmap 2009: Carbon Emissions Reductions up to 2050 . Organisation for Economic Co-operation and Development, 2009. [6] Ramme B W, Tharaniyil M P. Coal Combustion Products Utilization Handbook: 2nd Edition , We Energies, 2004. [7] Naik T R, Kraus R N, Siddique R. Demonstration of Manufacturing Technology for Concrete and CLSM Utilizing Wood Ash From Wisconsin: Report

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Modelling Accuracy of a Car Steering Mechanism with Rack and Pinion and McPherson Suspension

References [1] Meissonier J., Fauroux J-C., Gogu G. and Montezin C. (2006): Geometric identification of an elasto-kinematical model in a car suspension . – Proc. I. Mech. E., vol.220, No.9, Part D: J. Automobile Engineering, pp.1209-1220. Meissonier J. Fauroux J-C. Gogu G. Montezin C. 2006 Geometric identification of an elasto-kinematical model in a car suspension Proc. I. Mech. E. 220 9 Part D: J. Automobile Engineering, 1209 1220 [2] Mantaras D.A., Luque P. and Vera C. (2004): Development and validation of a three

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Simulation Investigation of Rotor Loads and Blade Deformations in Steady States and at Boundaries of Helicopter Flight Envelope

Airloads Rotor , American Helicopter Society Technical Meeting on Aeromechanics Design for Vertical Lift, San Francisco, California 2016. [5] Yeo, H., Johnson, W., Comparison of Rotor Structural Loads Calculated Using Comprehensive Analysis , 31 st European Rotorcraft Forum, Florence 2005. [6] Biedron, R. T., Lee-Rausch, E. M., Computation of UH-60A Airloads Using CFD/CSD Coupling on Unstructured Meshes , American Helicopter Society 67 th Annual Forum, Virginia Beach, Virginia 2011. [7] Gula, P., Gorecki, T., Design, Experiments and Development of

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Description of Diesel Fuel Based on Synchronous Fluorescence Spectroscopy

., Synchronyzed excitation of fluorescence emission spectra , Nature Phys. Sci., 231, 64-65, London 1971. [5] Operation manual, Aqualog Horiba, rev. A, 2011. [6] Patra, D., Mishra, A. K., Total synchronous fluorescence scan spectra of petroleum products , Anal. Bioanal. Chem., Vol. 373, Is. 4-5, 304-309, 2002. [7] Patra, D., Mishra, A. K., Recent developments in multi-component synchronous fluorescence scan analysis , Trends in analytical chemistry, Vol. 21, No. 12, 2002. [8] Poryvkina, L., Babichenko, S., Davydova, O., SFS characterisation of oil

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Simulation Investigation of Operational Conditions of Rotor for High-Speed Compound Helicopter

. [4] Hirschberg M., Dynamic developments continue apace: New Sikorsky and Bell rotorcraft forge ahead , Vertiflite, Vol. 61, No. 6, pp. 16-19, 2015. [5] http://www.airbus.com/newsroom/press-releases/de/2017/06/Airbus-Helicopters-reveals-Racer-high-speed-demonstrator-configuration.html . [6] Robb, R. L., Hybrid helicopters: compounding the quest for speed , Vertiflite, Vol. 52, No. 6, pp. 30-56, 2006. [7] Silva, C., Yeo, H., Johnson, W., Design of a slowed-rotor compound helicopter for future joint service missions , American Helicopter Society

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Comparative Analysis of the Operating Indexes of Manually and Automatically Controlled Passenger Car Powertrain System at Variable Load States

Engines, Ecology & Diagnostic, PTNSS 2007, pp. 25-30, 2007. [4] Horwath, E., Torok, A., Development of road transport emission standards , Production Enginering Archives, Vol. 7, No 2, pp. 6-10, 2015. [5] Mamala, J., Kompensacja niedostatku siły napędowej w procesie rozpędzenia samochodu osobowego , Habilitation Thesis, Opole 2011. [6] Mitschke, M., Dynamika samochodu , Wydawnictwo WKiŁ, Warszawa 1972. [7] Jazar, R. N., Vehicle Dynamics: Theory and Applications , Springer Science, 2008. [8] Siłka, W., Teoria ruchu samochodu , WNT

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