• Title/Summary/Keyword: drone control

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An Empirical Study on the Application of Drone based on LED-ID & RFID for Effective Stock Management of Unit Load Device - perspective of Air Cargo Terminal Case (항공화물 탑재용기(ULD)의 효율적 관리를 위한 LED-ID와 RFID 기반의 드론 적용 방안에 관한 연구- 항공화물터미널사례)

  • Baik, Namjin;Baik, Namkyu;Lee, Minwoo;Cha, Jae-Sang
    • Journal of Satellite, Information and Communications
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    • v.12 no.4
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    • pp.157-161
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    • 2017
  • Effective management of ULD (Unit Load Device) in Air Cargo Transportation is one of the Airline's main concerns. At present, the way of management of ULD which has the ID tag based on RFID is carried by cargo control staff with PDA. However, the activity of ULD management is limitted due to complexity of cargo terminal facilities. In this study, we offer the effective way of management of ULD by the DRONE equipped by LED-ID & RFID READER at the higher altitude in Air Cargo Terminal to recover the difficulty of identification due to complexity of terminal facilities. Further to the above, we suggest the operational effectiveness, limitation, and the direction of future research.

A Study on Vertiport Installation Standard of Drone Taxis(UAM) (드론택시(UAM)의 수직이착륙장(Vertiport) 설치기준 연구)

  • Choi, Ja-Seong;Lee, Seok-Hyun;Baek, Jeong-Seon;Hwang, Ho-Won
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.29 no.1
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    • pp.74-81
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    • 2021
  • UAM(Urban Air Mobility) systems have evolved in the form of helicopters in the 1960~1970s, tiltrotors in the 1980s, small aircraft transportation systems in the 2000s, and electric-powered Vertical Take-Off and Landing (eVTOL) in the 2010s; accordingly, the early heliport has evolved to its current form of a Vertiport. Vertical Takeoff and Landing Sites, Vertiports, are important factors for the successful introduction of UAM, along with the resolution of air traffic control (ATC), air security, and noise problems. However, there are no domestic or international installation standards and guidelines yet. Therefore, in this study, installation standards were prepared by referring to domestic and international case studies, ICAO standards, and MIT research papers. The study proposes to establish standards for Final Approach and Takeoff Area (FATO) as 1.5D, 1D for Touchdown and Lift-Off Area (TLOF), and 1.5D for Safety Area (SA). It also proposes to add "UAM Vertiport Installation Standards" to the 「Act on the Promotion and Foundation of Drone Utilization, Drone Act」.

A Study on the Anomaly Prediction System of Drone Using Big Data (빅데이터를 활용한 드론의 이상 예측시스템 연구)

  • Lee, Yang-Kyoo;Hong, Jun-Ki;Hong, Sung-Chan
    • Journal of Internet Computing and Services
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    • v.21 no.2
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    • pp.27-37
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    • 2020
  • Recently, big data is rapidly emerging as a core technology in the 4th industrial revolution. Further, the utilization and the demand of drones are continuously increasing with the development of the 4th industrial revolution. However, as the drones usage increases, the risk of drones falling increases. Drones always have a risk of being able to fall easily even with small problems due to its simple structure. In this paper, in order to predict the risk of drone fall and to prevent the fall, ESC (Electronic Speed Control) is attached integrally with the drone's driving motor and the acceleration sensor is stored to collect the vibration data in real time. By processing and monitoring the data in real time and analyzing the data through big data obtained in such a situation using a Fast Fourier Transform (FFT) algorithm, we proposed a prediction system that minimizes the risk of drone fall by analyzing big data collected from drones.

Experimental Verification of the Characteristic Analysis of the Aricultural Drone using Smart Operating Mode (스마트 운영 모드를 활용한 농업용 방제 드론의 특성 분석에 관한 실험적 검증)

  • Wooram Lee
    • The Journal of the Convergence on Culture Technology
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    • v.9 no.6
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    • pp.1049-1055
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    • 2023
  • The utilization of agricultural drones for pest control operations has been increasing due to its economic efficiency. However, variations in the effectiveness of these operations occur depending on the operator's proficiency. In this study, we applied a smart operating mode to overcome the limitations of manual flight mode and proposed a numerical model. Through comparative validation with prior research, we conducted experimental verification. As a result, we determined the spray time and calculation of spray area for each drone model. We selected a drone for pest control with a high similarity to the numerical model and verified it experimentally. Through this, we confirmed that the application of the smart operating mode is more effective in terms of calculation of spray area and operational efficiency compared to manual flight mode.

Development of Processor Real-Time Monitoring Software for Drone Flight Control Computer Based on NUTTX (NUTTX 기반 드론 비행조종컴퓨터의 통합시험을 위한 프로세서 모니터링 연구)

  • Choi Jinwon
    • Journal of Platform Technology
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    • v.10 no.4
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    • pp.62-69
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    • 2022
  • Flight control systems installed on unmanned aircraft require thorough verification from the design stage. This verification is made through the integrated flight control test environment. Typically, a debugger is used to monitor the internal state of a flight control computer in real time. Emulator with a real-time memory monitor and trace is relatively expensive. The JTAG Emulator is unable to operate in real time and has limitations that cannot be caught up with the processing speed of latest high-speed processors. In this paper, we describe the results of the development of internal monitoring software for drone flight control computer processors based on NUTTX/PIXHAWK. The results of this study show that the functions provided compared to commercial debugger are limited, but it can be sufficiently used to verify the flight control system using this system under limited budget.

Design approach of passive vibration control using damping tape for quadrotor drone in hover (제자리 비행 조건에서 쿼드로터의 감쇠 테이프를 이용한 수동적 진동 제어 설계 방법 연구)

  • Sejun Kim;Hyungmo Kim;Seongwoo Cheon;Sungjun Kim;Haeseong Cho;Lae-Hyong Kang
    • Journal of Aerospace System Engineering
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    • v.18 no.1
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    • pp.37-45
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    • 2024
  • This paper presents a design approach for passive vibration control to reduce vertical vibrations transmitted to the control unit during hovering flight of a quadrotor drone. Ground vibration test simulation based on finite element model was performed for forced vibration analysis of the quadrotor drone. First, modal analysis was performed to evaluate dynamic characteristics. Forced vibration response analysis was then performed to obtain the steady-state response within the operating frequency range under the hovering flight condition. Furthermore, to obtain the vibration reduction effect, a viscous damping tape was applied at positions that could induce vibrations transmitted to the control unit under the same conditions. Such a passive vibration control approach was investigated. Relevant vibration reduction effect was assessed with respect to the application of damping materials and the attachment position.

An Automatic Collision Avoidance System for Drone using a LiDAR sensor (LiDAR 센서를 이용한 드론 자동 충돌방지 시스템)

  • Chong, Ui-Pil;An, Woo-Jin;Kim, Yearn-Min;Lee, Jung-Chul
    • Journal of the Institute of Convergence Signal Processing
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    • v.19 no.2
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    • pp.54-60
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    • 2018
  • In this paper, we propose an efficient automatic control method for the collision avoidance of drones. In general, the drones are controlled by transmitting to the flight control (FC) module the received PWM signals transmitted from a RC controller which transduce movements of the knob into PWM signal. We implemented the collision avoidance module in-between receiver and FC module to monitor and change the throttle, pitch and roll control signals to avoid drone collision. In order to avoid the collision, a LiDAR distance sensor and a servo-motor are installed and periodically measure the obstacle distance within -45 degrees from 45 degrees in flight direction. If the collision is predicted, the received PWM signal is changed and transmitted to the FC module to prevent the collision. We applied our proposed method to a hexacopter and the experimental results show that the safety is improved because it can prevent the collision caused by the inadvertency or inexperienced maneuver.

Quadrotor altitude control with experimental data-based PID controller (실험 데이터 기반의 PID제어기를 이용한 쿼드로터의 고도제어)

  • Ho-Sung Lee;Ji-Sun Park;Ho-Lim Choi
    • Journal of IKEEE
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    • v.28 no.2
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    • pp.136-144
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    • 2024
  • In this paper, we propose a PID controller for altitude control of quadrotor system with experimental analysis. The Routh-Hurwitz test is applied to analyze the system to which our proposed controller is applied. We also summarize experimental data in which the gain values of kP, kI, and kD are changed using MATLAB and Simulink based on mathematical modeling of the quadrotor system. Based on the summarized experimental data, we analyze the effect of changes in each gain values (kP, kI, kD) of PID controller on altitude control of quadrotor, and present an algorithm for tuning the PID controller gain values. The PID controller with the proposed algorithm is applied to AR.Drone system, subsequently and result are verifised through experiments.

Density map estimation based on deep-learning for pest control drone optimization (드론 방제의 최적화를 위한 딥러닝 기반의 밀도맵 추정)

  • Baek-gyeom Seong;Xiongzhe Han;Seung-hwa Yu;Chun-gu Lee;Yeongho Kang;Hyun Ho Woo;Hunsuk Lee;Dae-Hyun Lee
    • Journal of Drive and Control
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    • v.21 no.2
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    • pp.53-64
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    • 2024
  • Global population growth has resulted in an increased demand for food production. Simultaneously, aging rural communities have led to a decrease in the workforce, thereby increasing the demand for automation in agriculture. Drones are particularly useful for unmanned pest control fields. However, the current method of uniform spraying leads to environmental damage due to overuse of pesticides and drift by wind. To address this issue, it is necessary to enhance spraying performance through precise performance evaluation. Therefore, as a foundational study aimed at optimizing drone-based pest control technologies, this research evaluated water-sensitive paper (WSP) via density map estimation using convolutional neural networks (CNN) with a encoder-decoder structure. To achieve more accurate estimation, this study implemented multi-task learning, incorporating an additional classifier for image segmentation alongside the density map estimation classifier. The proposed model in this study resulted in a R-squared (R2) of 0.976 for coverage area in the evaluation data set, demonstrating satisfactory performance in evaluating WSP at various density levels. Further research is needed to improve the accuracy of spray result estimations and develop a real-time assessment technology in the field.

A Study on the Practice of Engineering Education in Graduation Standards Certification Process through the Design and Implementation of Drone for Ground Driving and Aerial Flight (지상주행과 공중비행이 가능한 Drone 설계 및 구현을 통한 졸업기준 인증 과정에서 공학교육 실천에 관한 연구)

  • Jang, Woo-Jin;Yoo, Jeong-Min;Chang, Eun-Young
    • Journal of Practical Engineering Education
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    • v.10 no.1
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    • pp.17-24
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    • 2018
  • Through the design and production of works for the third semester as a major unit, It is proposed the process of satisfying the graduation standards with the design and production process of the drone which can be applied to various mobile environments. Using the shape of Ring Propeller, it is made to be able to play both the role of generating lift as a propeller and the role of a wheel that touches the ground through the surface of the rim. In addition, the Servo Motor is used to convert the drive shaft of the motor to the correct angle according to the command. Then, based on the idea, the 3D printing is implemented to confirm the result of the configuration, and the circuit for driving the propulsion is designed and manufactured. As a result, the conversion of the desired propulsion system during air navigation and operation failed due to the weight increase of the propellant. It is confirmed that the size of the thrust and the tolerance limit of the ring propeller are the errors. Through these processes, it has been recognized to have experience of creative thinking and cooperation through engineering approach and comprehensive design, and confirmed to satisfy the graduation criteria by writing an engineering paper on the result.