Results 91 to 100 of about 15,285 (203)
Perancangan Autonomous Landing pada Quadcopter Menggunakan Behavior-Based Intelligent Fuzzy Control
Jurnal Teknik ITS, 2013 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
Predicting Quadcopter Drone Noise Using the Lattice Boltzmann Method [PDF]
The market for new vertical takeoff and landing vehicles, including autonomous urban air taxis and drones for applications such as package delivery, imaging, and surveillance, is growing rapidly.
Barad, Michael +3 more
core +1 more source
Jurnal Teknik ITS, 2012 Perkembangan teknologi sistem kendali pesawat sayap berputar (copter) semakin pesat salah satunya pada pesawat berbaling-baling empat (quadcopter). Landing merupakan bagian tersulit dalam penerbangan quadcopter. Ukuran quadcopter yang kecil mengakibatkan
Fadjri Andika Permadi +2 more
doaj
Periodicals of Engineering and Natural Sciences (PEN), 2018 Sarath S. Chandra, A. S. C. S. Sastry
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MATHEMATICAL MODEL OF THE SYSTEM CONTROL OF THE QUADCOPTER
Надежность и качество сложных системBackground. This article discusses the control of an unmanned aerial vehicle-a quadcopter. Materials and methods. A quadcopter of a given class is studied as an object of control, an analysis and mathematical description of the quadcopter control ...
A.I. Godunov +3 more
doaj +1 more source
Improved Fixed-Time Attitude Tracking Control for Quadcopter Unmanned Aerial Vehicles
IEEE AccessQuadcopters have become a unmanned aerial vehicle class playing essential roles in a wide range of real-world applications. Many missions in such applications require the quadcopter’s attitude to converge to given setpoints in a fixed time ...
Xuan Nguyen +3 more
doaj +1 more source
, 2019 O controlo de voo dos quadcopters tem grande interesse devido ao aumento de número de aplicações que recorrem a este tipo de aeronaves. As vantagens que o recurso a 4 conjuntos de motor e hélice como meio de propulsão apresenta em relação a outro tipo de drones, são a capacidade de se manter imóvel no ar e a capacidade de descolar e aterrar na vertical.
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A Combination of PD Controller and PIAFC for Stabilization of “x” Configuration Quadcopter
Emitter: International Journal of Engineering Technology, 2014 This paper presents a stabilization control method for “x” configuration quadcopter. The control method used the combination of PD (Proportional Derivative) controller and PIAFC (Proportional Integral Active Force Control).
Ni’am Tamami +2 more
doaj
Formation Flying for Quadcopters
, 2015 The purpose of this project is to design a control law to control a groupof quadcopters ying in formation in a specied reference track. To describe the movements of a quadcopter a mathematical model, basedon Newton-Euler equations, is formed and linearized into a linear statespacemodel. The control law is then designed by using feedback.
Hesselmar, Petra, Brodin, Kristoffer
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Load-Swing Attenuation in a Quadcopter-Payload System Through Trajectory Optimisation. [PDF]
Sensors (Basel)Feng B, Khatamianfar A.
europepmc +1 more source