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Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germany
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
Quantity: 2 available
Seller: AHA-BUCH GmbH, Einbeck, Germany
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
Quantity: 1 available
Seller: Majestic Books, Hounslow, United Kingdom
Condition: New. Print on Demand. Seller Inventory # 391487582
Quantity: 4 available
Seller: moluna, Greven, Germany
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
Quantity: Over 20 available
Seller: Biblios, Frankfurt am main, HESSE, Germany
Condition: New. Seller Inventory # 18388112267
Quantity: 4 available
Seller: Mispah books, Redhill, SURRE, United Kingdom
paperback. Condition: New. New. book. Seller Inventory # ERICA80061398582166
Quantity: 1 available