DATA ACQUISITION OF POSITION AND SPEED OF ROTOR WITH ROTARY ENCODER AND MEASUREMENT OF CONTROL PARAMETERS ON SWASHPLATELESS COAXIAL DRONE SYSTEM

UAV(Unmanned Aerial Vehicle) or can be called drone have very rapid development at this time. Along with these developments, we found that drone can be controlled well with just two propellers. To move in the horizontal plane, the drone needs to change its orientation by doing pitch and roll. In thi...

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محفوظ في:
التفاصيل البيبلوغرافية
المؤلف الرئيسي: Rasyid Fadlurrahman, Nur
التنسيق: Final Project
اللغة:Indonesia
الوصول للمادة أونلاين:https://digilib.itb.ac.id/gdl/view/43634
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المؤسسة: Institut Teknologi Bandung
اللغة: Indonesia
id id-itb.:43634
spelling id-itb.:436342019-09-27T15:06:51ZDATA ACQUISITION OF POSITION AND SPEED OF ROTOR WITH ROTARY ENCODER AND MEASUREMENT OF CONTROL PARAMETERS ON SWASHPLATELESS COAXIAL DRONE SYSTEM Rasyid Fadlurrahman, Nur Indonesia Final Project UAV, rotary encoder, parameter, swashplateless, cyclic control, position, dan speed INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/43634 UAV(Unmanned Aerial Vehicle) or can be called drone have very rapid development at this time. Along with these developments, we found that drone can be controlled well with just two propellers. To move in the horizontal plane, the drone needs to change its orientation by doing pitch and roll. In this final project, the implementation of a swashplateless system will be discussed that can overcome this problem. Mechanically, this system can change the orientation of the propeller angle aerodynamically. This system is implemented by utilizing a microcontroller that converts PWM signals from commercial Flight Controllers into cyclic control signals.This control have advantages where the drone can be stabilized when flying in the sky, with the result that the camera can be implemented with no stabilizer like gimbal. The implemented cyclic control is a control of changes in rotor speed in one rotation. By controlling the speed at a certain angle, there will be an increase of force on one side of the propeller and the orientation of the propeller angle will change. In developing this system, a rotary encoder is needed to detect the position and speed of the rotor in the system. In this flight system also need to know also the parameters that affect the condition of flying drones when controlled. This control parameter is obtained from mathematical calculations based on the aerodynamic theory applied to the UAV. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description UAV(Unmanned Aerial Vehicle) or can be called drone have very rapid development at this time. Along with these developments, we found that drone can be controlled well with just two propellers. To move in the horizontal plane, the drone needs to change its orientation by doing pitch and roll. In this final project, the implementation of a swashplateless system will be discussed that can overcome this problem. Mechanically, this system can change the orientation of the propeller angle aerodynamically. This system is implemented by utilizing a microcontroller that converts PWM signals from commercial Flight Controllers into cyclic control signals.This control have advantages where the drone can be stabilized when flying in the sky, with the result that the camera can be implemented with no stabilizer like gimbal. The implemented cyclic control is a control of changes in rotor speed in one rotation. By controlling the speed at a certain angle, there will be an increase of force on one side of the propeller and the orientation of the propeller angle will change. In developing this system, a rotary encoder is needed to detect the position and speed of the rotor in the system. In this flight system also need to know also the parameters that affect the condition of flying drones when controlled. This control parameter is obtained from mathematical calculations based on the aerodynamic theory applied to the UAV.
format Final Project
author Rasyid Fadlurrahman, Nur
spellingShingle Rasyid Fadlurrahman, Nur
DATA ACQUISITION OF POSITION AND SPEED OF ROTOR WITH ROTARY ENCODER AND MEASUREMENT OF CONTROL PARAMETERS ON SWASHPLATELESS COAXIAL DRONE SYSTEM
author_facet Rasyid Fadlurrahman, Nur
author_sort Rasyid Fadlurrahman, Nur
title DATA ACQUISITION OF POSITION AND SPEED OF ROTOR WITH ROTARY ENCODER AND MEASUREMENT OF CONTROL PARAMETERS ON SWASHPLATELESS COAXIAL DRONE SYSTEM
title_short DATA ACQUISITION OF POSITION AND SPEED OF ROTOR WITH ROTARY ENCODER AND MEASUREMENT OF CONTROL PARAMETERS ON SWASHPLATELESS COAXIAL DRONE SYSTEM
title_full DATA ACQUISITION OF POSITION AND SPEED OF ROTOR WITH ROTARY ENCODER AND MEASUREMENT OF CONTROL PARAMETERS ON SWASHPLATELESS COAXIAL DRONE SYSTEM
title_fullStr DATA ACQUISITION OF POSITION AND SPEED OF ROTOR WITH ROTARY ENCODER AND MEASUREMENT OF CONTROL PARAMETERS ON SWASHPLATELESS COAXIAL DRONE SYSTEM
title_full_unstemmed DATA ACQUISITION OF POSITION AND SPEED OF ROTOR WITH ROTARY ENCODER AND MEASUREMENT OF CONTROL PARAMETERS ON SWASHPLATELESS COAXIAL DRONE SYSTEM
title_sort data acquisition of position and speed of rotor with rotary encoder and measurement of control parameters on swashplateless coaxial drone system
url https://digilib.itb.ac.id/gdl/view/43634
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