PENGEMBANGAN MODEL MATEMATIKA SISTEM WAHANA UDARA MIKRO DENGAN SAYAP KEPAK
This thesis discusses about the modelling and simulation of a simple flapping-wing micro aerial vehicle (FMAV). A mathematical model of the FMAV system is required for understanding and analyzing the dynamic characteristics of it. To obtain the mathematical model, multi-rigid body approach is used....
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Format: | Final Project |
Language: | Indonesia |
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Online Access: | https://digilib.itb.ac.id/gdl/view/39024 |
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Institution: | Institut Teknologi Bandung |
Language: | Indonesia |