Proportional Integral Derivative Based Control For Autonoumous Vertical Take Off And Landing Of Quadcopter System
Since 2009, research on unmanned aerial vehicle (UAV) especially quadcopter system has attracted a considerable attention from researchers in the field. The quadcopter system is actually a class of flying robot that has ability to take off and landing in a vertical condition. Moreover, it has the ad...
| المؤلف الرئيسي: | |
|---|---|
| التنسيق: | أطروحة |
| اللغة: | الإنجليزية الإنجليزية |
| منشور في: |
UTeM
2016
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| الموضوعات: | |
| الوصول للمادة أونلاين: | http://eprints.utem.edu.my/id/eprint/18518/ https://plh.utem.edu.my/cgi-bin/koha/opac-detail.pl?biblionumber=100936 HF5351.M34 2016 |
| Abstract | Abstract here |