Development of a Low-Cost Embedded Flight Controller for Quadcopter

Sumantri, Bambang; Tamami, Niam; Nuraga, Yudha Birawa; Kurniawan, B I

doi:10.1109/ies50839.2020.9231564

Cited by 6 publications

(4 citation statements)

References 9 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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“…PID stands for Proportional, Integral, and Derivative, and it is a feature of flight controller software that analyzes sensor data and determines how quickly the motors should spin to keep the quadcopter rotating at the appropriate speed, Figures 8 and 9. The PID controller's objective is to reduce "error", which is the differrence between a measured value (gyro sensor measurement) [18] and the desired set-point (the desired rotation speed). The proportional component of the PID preserves quadcopter stability, while the integral component accomplishes precision and the derivative component controls speed.…”

Section: Pid Control Systemmentioning

confidence: 99%

Comparing dynamic model and flight control of plus and cross quadcopter configurations

Ali¹,

Abdulhady²

2022

FME Transactions

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This research investigates and demonstrates the fundamental differences in performance and operation of both the cross and quadcopter configurations. The system's nonlinear dynamic model was first derived and implemented in Simulink for each quadcopter. The identical initial control values were applied for both quadcopters. The plus-configuration creates a yaw moment when a pitch or roll control input is supplied using multi-rotor controls; however, the cross-configuration decouples pitch and roll control from yaw. However, the plus-quad showed considerable instability while rotating with a pitch and rolling due to the self-generated residual rotation of the four rotors, which is small in the cross quadcopter, making it more maneuverability stable. The obtained results showed that both quadcopters consume the same energy amount.

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“…In a quadcopter with four BLDC motors, four slaves are needed to control each BLDC motor. In paper [2], a low-cost quadcopter can be built using the STM32F103C8T6 microcontroller, IMU MPU6050, and ultrasonic sensor HC-SR04. This study uses control PID as a quadcopter control algorithm but has not found a suitable PID value to get a good response.…”

Section: Introductionmentioning

confidence: 99%

Quadcopter Main Board Design with PID Algorithm as Controller

Bachtiar

Wibowo

Prastyawan

et al. 2022

Inf. J. Ilm. Bid. Teknol. Inf. dan Komun.

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Kontes Robot Terbang Indonesia (KRTI) Flight controller division has a mission to independently make an unmanned aerial vehicle (UAV) controller. UAV controllers are usually made by non-local manufacturers, who have a package between the controller and the aircraft. Due to limited pins and specific functions, most controllers cannot adapt to user requirements. For this reason, in this study, we made a UAV controller with a more significant number of pins that can be programmed independently. Main Controller is a master board device used to control the stability of the UAV when flying. The main controller has been designed specifically for certain products so that the UAV cannot be modified. In this study, it is proposed to make the main controller that is specifically designed to fly a Quadcopter UAV. Movement control for quadcopter stability when flying using the Proportional Integral Derivative (PID) method. The main controller has a function that is to regulate the entire course of flight on unmanned vehicles. PID control can adapt to changes so that the system becomes stable. The PID control on the Main Controller is intended to balance the quadcopter concerning its orientation angle. The Main Controller is also tasked with recording data from sensors such as the Inertial Measurement Unit (IMU) and reading data from the remote. The controller successfully flew the quadcopter with a P value of 0.245, an I value of 0.0139, and a D value of 0.0085.

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Development of a Low-Cost Embedded Flight Controller for Quadcopter

Cited by 6 publications

References 9 publications

Perancangan Sistem Komunikasi GSM pada Quadcopter Berbasis Arduino Uno R3

Perancangan Sistem Komunikasi GSM pada Quadcopter Berbasis Arduino Uno R3

Comparing dynamic model and flight control of plus and cross quadcopter configurations

Quadcopter Main Board Design with PID Algorithm as Controller

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