Motion control analysis of a quadcopter system part II — Modelling

S, Venkatasundarakumar T; Suwathy, R.; M, Haripriya T; Venkatesan, M.

doi:10.1109/iccic.2016.7919523

Cited by 5 publications

(2 citation statements)

References 3 publications

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“…Quadcopters adalah sistem robot udara VTOL dan memiliki dinamika yang kompleks meskipun desainnya sederhana [6]. Quadcopter telah menjadi penelitian yang menarik karena aplikasinya yang luas, seperti pengawasan, pemetaan, pengiriman drone, dan lain sebagainya [7].…”

Section: Quardcopterunclassified

Perancangan Sistem Komunikasi GSM pada Quadcopter Berbasis Arduino Uno R3

Amir,

Mardiansyah,

Sunardi

2023

tech

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Menanggapi permasalahan yang ada dibidang industri serta kemajuan teknologi elektronika dan komunikasi yang semakin pesat sementara dalam dunia telekomunikasi itu sendiri banyak peningkatan jenis pesan dan komunikasi yang menggunakan GSM, pada era globalisasi dan informasi pada zaman sekarang pengiriman dan penerimaan pesan lebih banyak ragamnya. Mulai dari pesan teks, gambar, data, audio dan video, dari perkembangan pesan dari berbagai regenerasi tersebut. Dalam skripsi ini hanya menggunakan pesan teks SMS untuk pengendalian Quadcopter dengan berbasis arduino uno R3. Pada umumnya Quadcopter dikendalikan dengan remote control atau dengan sensor tertentu, tapi rancangan Quadcopter yang dikendalikan menggunakan modul GSM dengan mode SMS teks untuk perintah kerja dan yang akan dibaca oleh Arduino Uno R3 yang akan dikonversi kedalam bahasa C oleh Arduino Uno R3 itu sendiri melalui library GSM.

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Section: Quardcopterunclassified

Perancangan Sistem Komunikasi GSM pada Quadcopter Berbasis Arduino Uno R3

Amir,

Mardiansyah,

Sunardi

2023

tech

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“…Consequently, they recommended taking into account larger moves and the effect of nonlinearity in the future researches. In [25,26], a simulation with an experimental process was performed to analyze the motion control of the quadcopter system. The authors noted the importance of these studies as a first step in the automation of aerial vehicle systems.…”

Section: Introductionmentioning

confidence: 99%

Modelling of quad‐rotor dynamics and Hardware‐in‐the‐Loop simulation

Saif

Eminoğlu

2022

The Journal of Engineering

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The quadcopter as one of the UAV (Unmanned aerial vehicles) is inherently unstable, and has six degrees of freedom (6 DOF), while the number of control inputs is four. The present work presents a sequential methodology to analyze and explain the control mechanism of quadcopter-UAV in academic and research institutions. This methodology includes simulation, modelling, attitude control, Hardware in-the Loop (HIL) testing methodology, performance evaluation, and an experimental testing platform. Coordinate systems, kinematics, and dynamics systems are derived in great detail. Then, a real-time test platform is designed to verify system stability in a safe environment. (HIL) simulation was performed by the Pixhawk flight controller board interfaced with the Mission Planner platform. The numerical results include the control parameters of the quadcopter position (phi, theta, psi), and the translation values. The simulation results showed high and reliable performance both at the desired roll, pitch, and yaw angles as well as at the quadcopter position in the coordinate axes. Furthermore, the results of the real-time experiments (indoor/outdoor flight tests) have successfully demonstrated good stability and high response. Based on the methodology used in this research, the cost and risk of real-time flight experiments for UAVs have been reduced.

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