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Vertical Takeoff and Landing UAV Aircraft System of YTU (YTU-VTOL-V1) - Softcover

 
9786139858217: Vertical Takeoff and Landing UAV Aircraft System of YTU (YTU-VTOL-V1)

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Hla Myo Tun
ISBN 10: 6139858216 ISBN 13: 9786139858217
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Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -For the conceptual design phase, it is uncomplicated methods and tools are used to do feasibility studies on a large number of VTOL designs with the specific goal to define the suitable design to meet the best performance for the VTOL aircraft. The next phase is preliminary design where one or a couple of designs from the conceptual phase are studied in more detail. The YTU-VTOL-V1 aircraft design possesses both Fixed-wing function and Rotary-wing function. The fixed-wing function is used for flight mode and the rotary-wing is used for helicopter mode. The autopilot system for YTU-VTOL-V1 aircraft system is based on the development of mathematical modeling and stability flight control system with PID controller which is used for longitudinal and lateral motion. Another portion is to accomplish the algorithm for vertical take-off and landing of YTU-VTOL-V1 aircraft system. This work approaches vision-based landing system for UAVs of the type Vertical Take-off and Landing (VTOL). In this work, target detection system is used for landing function. VTOL UAV is able to take-off and to land via a vertical movement in relation to the plain of the landing target with vision system. 168 pp. Englisch. Seller Inventory # 9786139858217

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Hla Myo Tun
ISBN 10: 6139858216 ISBN 13: 9786139858217
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Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - For the conceptual design phase, it is uncomplicated methods and tools are used to do feasibility studies on a large number of VTOL designs with the specific goal to define the suitable design to meet the best performance for the VTOL aircraft. The next phase is preliminary design where one or a couple of designs from the conceptual phase are studied in more detail. The YTU-VTOL-V1 aircraft design possesses both Fixed-wing function and Rotary-wing function. The fixed-wing function is used for flight mode and the rotary-wing is used for helicopter mode. The autopilot system for YTU-VTOL-V1 aircraft system is based on the development of mathematical modeling and stability flight control system with PID controller which is used for longitudinal and lateral motion. Another portion is to accomplish the algorithm for vertical take-off and landing of YTU-VTOL-V1 aircraft system. This work approaches vision-based landing system for UAVs of the type Vertical Take-off and Landing (VTOL). In this work, target detection system is used for landing function. VTOL UAV is able to take-off and to land via a vertical movement in relation to the plain of the landing target with vision system. Seller Inventory # 9786139858217

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ISBN 10: 6139858216 ISBN 13: 9786139858217
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Hla Myo Tun
Published by LAP LAMBERT Academic Publishing, 2018
ISBN 10: 6139858216 ISBN 13: 9786139858217
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Seller: moluna, Greven, Germany

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Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Tun Hla MyoProf. Dr. Hla Myo Tun received B.E.(Electronics) and PhD. (Electronic Engineering) degrees from Mandalay Technological University in 2002 and 2008, respectively. He received his master degree from Yangon Technological Univ. Seller Inventory # 385874586

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ISBN 10: 6139858216 ISBN 13: 9786139858217
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Seller: Biblios, Frankfurt am main, HESSE, Germany

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Tun, Hla Myo
Published by LAP Lambert Academic Publishing, 2018
ISBN 10: 6139858216 ISBN 13: 9786139858217
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Seller: Mispah books, Redhill, SURRE, United Kingdom

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paperback. Condition: New. New. book. Seller Inventory # ERICA80061398582166

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