TY - GEN
T1 - Design and Simulation of Quadcopter Mode System on Hybrid UAV Quadplane Configuration
AU - Marta, Aryandi
AU - Muis, Abdul
N1 - Publisher Copyright:
© 2023 American Institute of Physics Inc.. All rights reserved.
PY - 2023/12/11
Y1 - 2023/12/11
N2 - The development of hybrid UAV is carried out to gain the advantage of fixed wing and rotorcraft type in one flying vehicle, so we get more flexibility to carry out its flying missions without requiring a special area for takeoff and landing. From several types of configurations, quadplane was chosen to be the object research because of its airframe which was simple and easy to develop. Quadplane is a fixed wing type UAV which is equipped with four electric motors, so it has the ability to fly like a quadcopter. In operational flight, quadplane has three flight modes, such as: quadcopter mode, transition mode, and fixed wing mode. In this study, the discussion will focus on developing a quadcopter mode system model. The system model is built using Matlab/Simulink which consists of several control blocks and equations of motion blocks. The control strategy used in this model are Proportional (P) and Proportional-Derivative (PD) controllers. From the simulation results that have been carried out, it was obtained that the quadcopter mode system model was able to follow the given reference value with 7.3% overshoot in the X direction, 7.2% overshoot in the Y direction, and a delay of 2.5 seconds in the Z direction.
AB - The development of hybrid UAV is carried out to gain the advantage of fixed wing and rotorcraft type in one flying vehicle, so we get more flexibility to carry out its flying missions without requiring a special area for takeoff and landing. From several types of configurations, quadplane was chosen to be the object research because of its airframe which was simple and easy to develop. Quadplane is a fixed wing type UAV which is equipped with four electric motors, so it has the ability to fly like a quadcopter. In operational flight, quadplane has three flight modes, such as: quadcopter mode, transition mode, and fixed wing mode. In this study, the discussion will focus on developing a quadcopter mode system model. The system model is built using Matlab/Simulink which consists of several control blocks and equations of motion blocks. The control strategy used in this model are Proportional (P) and Proportional-Derivative (PD) controllers. From the simulation results that have been carried out, it was obtained that the quadcopter mode system model was able to follow the given reference value with 7.3% overshoot in the X direction, 7.2% overshoot in the Y direction, and a delay of 2.5 seconds in the Z direction.
UR - http://www.scopus.com/inward/record.url?scp=85180394380&partnerID=8YFLogxK
U2 - 10.1063/5.0181435
DO - 10.1063/5.0181435
M3 - Conference contribution
AN - SCOPUS:85180394380
T3 - AIP Conference Proceedings
BT - AIP Conference Proceedings
A2 - Septanto, Harry
A2 - Adhynugraha, Muhammad Ilham
A2 - Vetrita, Yenni
A2 - Santosa, Cahya Edi
A2 - Sitompul, Peberlin Parulian
A2 - Yulihastin, Erma
A2 - Muhamad, Johan
A2 - Mardianis, null
A2 - Fitrianingsih, Ery
A2 - Batubara, Mario
A2 - Abadi, Prayitno
A2 - Restasari, Afni
PB - American Institute of Physics Inc.
T2 - 9th International Seminar on Aerospace Science and Technology, ISAST 2022
Y2 - 22 November 2022 through 23 November 2022
ER -