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This thesis discusses about modelling and simulation of dynamics system with flapping-wing micro aerial vehicle/ FMAV. Modeling needs to be done in order to know the characteristics of motion of the system. To obtain a mathematical model, performed by the method of approach to a rigid system of mult...
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格式: | Final Project |
語言: | Indonesia |
在線閱讀: | https://digilib.itb.ac.id/gdl/view/15751 |
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機構: | Institut Teknologi Bandung |
語言: | Indonesia |
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