TY - GEN
T1 - Hardware-in-the-Loop Simulation of Autonomous System using Neural Network in Small Computer Platform
AU - Suherman, Iman Herlambang
AU - Ayu, Aqila Dzikra
AU - Matthew, Hansel
AU - Subiantoro, Aries
AU - Kusumoputro, Benyamin
N1 - Publisher Copyright:
© 2023 American Institute of Physics Inc.. All rights reserved.
PY - 2023/12/11
Y1 - 2023/12/11
N2 - Unmanned Aerial Vehicle (UAV) also called unmanned aircraft is often used for various purposes such as photography, carrying goods, to industrial monitoring. Most of the control schemes for the UAV such as quadcopter is using PID based controller because of low computational cost and simplicity, but this type of controller is unable to compensate for nonlinear disturbances such as harsh wind or frame vibration. This can be solved by using neural network control but there are several constraints in UAV application, such as weight limitation, power limitation, even compatibility of the system that can be solved by using small computer platform. Continuing on previous research for low level quadcopter control based on neural network, the next step is to implement this control in Hardware-in-the-loop format safely by using Pressure Process Rig data that had the same nonlinear characteristic. This paper explores Hardware-in-the-loop simulation development with several small computer platform in the neural network control application. In addition, variation between several hardware and TensorFlow version is carried out to determine the effect of each variation. This paper shows how the various hardware and even different version of programming library can affect the performance of the neural network model computation.
AB - Unmanned Aerial Vehicle (UAV) also called unmanned aircraft is often used for various purposes such as photography, carrying goods, to industrial monitoring. Most of the control schemes for the UAV such as quadcopter is using PID based controller because of low computational cost and simplicity, but this type of controller is unable to compensate for nonlinear disturbances such as harsh wind or frame vibration. This can be solved by using neural network control but there are several constraints in UAV application, such as weight limitation, power limitation, even compatibility of the system that can be solved by using small computer platform. Continuing on previous research for low level quadcopter control based on neural network, the next step is to implement this control in Hardware-in-the-loop format safely by using Pressure Process Rig data that had the same nonlinear characteristic. This paper explores Hardware-in-the-loop simulation development with several small computer platform in the neural network control application. In addition, variation between several hardware and TensorFlow version is carried out to determine the effect of each variation. This paper shows how the various hardware and even different version of programming library can affect the performance of the neural network model computation.
UR - http://www.scopus.com/inward/record.url?scp=85180390647&partnerID=8YFLogxK
U2 - 10.1063/5.0182155
DO - 10.1063/5.0182155
M3 - Conference contribution
AN - SCOPUS:85180390647
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 -