Results 111 to 120 of about 14,458 (214)
Perancangan Autonomous Landing pada Quadcopter Menggunakan Behavior-Based Intelligent Fuzzy Control
Quadcopter adalah salah satu platform unmanned aerial vehicle (UAV) yang saat ini banyak diriset karena kemampuannya melakukan take-off dan landing secara vertikal.
Chalidia Nurin Hamdani +2 more
doaj
Autonomous Quadcopter Videographer [PDF]
In recent years, the interest in quadcopters as a robotics platform for autonomous photography has increased. This is due to their small size and mobility, which allow them to reach places that are difficult or even impossible for humans.
Coaguila, Quiquia Rey
core
Quadcopter diharapkan dapat bergerak secara lincah dan efektif menyusuri lintasan horisontal. Berdasar hukum fisisnya, gerak lateral dapat terjadi karena adanya daya angkat dan terjadinya perubahan sudut dari quadcopter tersebut.
Tri Awan Nusa Putra +2 more
doaj
Aerodynamic Analysis of a Quadcopter Drone Propeller with the Use of Computational Fluid Dynamics
In the current work, an analysis for the initial aerodynamic assessment of a small sized quadcopter drone propeller is presented, focusing on the drone aerodynamic characteristics optimization.
Konstantinos Christodoulou +5 more
doaj +1 more source
Implementasi kendali Fuzzy Untuk Kestabilan Ketinggian Quadcopter
Unmanned Aerial Vehicle (UAV) merupakan teknologi robot yang dapat membantu manusia dalam menjelajah udara, salah satu contoh nya adalah quadcopter. Quadcopter merupakan bentuk dari aeromodelling yang mempunyai motor sebanyak empat dengan dengan jenis ...
Anggagita, Sandra
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MODEL UAV QUADCOPTER DENGAN KONTROLER PROPORTIONAL DERIVATIVE [PDF]
UAV (unmanned aerial vehicle) quadcopter didefinisikan sebagai mini-rotorcraft tanpa awak yang memiliki kemampuan untuk mengendalikan dinamika pergerakan dirinya untuk mencapai tujuan tertentu.
HARITS ANWAR ROZI
core
Proportional Derivative Active Force Control for “X” Configuration Quadcopter
This paper present a control method “x” configuration quadcopter. The control method used PDAFC (Proportional Derivative Active Force Control). PD is used to stabilize quadcopter, and AFC is used to reject uncertainty disturbance (e.g.
Niam Tamami +2 more
doaj +1 more source
Wind Source Localization System Based on a Palm-Sized Quadcopter
In this study, we implemented a compact wind direction sensor on a palm-sized quadcopter to achieve wind source localization (WSL). We designed an anemotaxis algorithm based on the sensor data and experimentally validated its efficacy.
Keisuke Yokota +2 more
doaj +1 more source
Investigating Quadcopter Control Methods Using Computer Simulation
In this thesis, I am working on implementing the P, PI, PD and PID controller to a non-linear quadcopter. Thereafter I will analyse and compare their performances using MATLAB/Simulink.
Mana, Muhammad
core
Guided Autonomy for Quadcopter Photography [PDF]
Photographing small objects with a quadcopter is non-trivial to perform with many common user interfaces, especially when it requires maneuvering an Unmanned Aerial Vehicle (C) to difficult angles in order to shoot high perspectives.
Alabachi, Saif
core

