• Title/Summary/Keyword: Flying Disc

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Smart Flying-Disc Monitoring System with IoT Technology (IoT 기술이 적용된 스마트 플라잉 디스크 모니터링 시스템 구축)

  • Lee, Jung-Chul;Jang, Young-Jong;Hwang, Tae-Ho
    • The Journal of the Korea institute of electronic communication sciences
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    • v.14 no.5
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    • pp.991-1000
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    • 2019
  • The flying-disc game has started since 1940. It has been spreading rapidly in Korea since 2007, mainly in elementary schools. Additionally, as sports science has been developed, research on flying discs has been continued to build a monitoring system for technological improvement and efficiency. In this paper, we acquire information on the user's flying-disc using 9-axis motion sensor and GPS. Then we propose a method for wireless transmission using Bluetooth 5.0. Specifically, the HW platform was designed and implemented not only to monitor a real-time data but also to compare and analyze rotational speed, flight trajectory, and a count of disc rotation through post-processing.

Flying Disc Golf Path-Tracing System Using Smart-Marker (스마트마커 연동 원반골프 경로 추적 시스템)

  • Choi, Chang-Hee;Lim, Jea-Yun;Choi, Kyung-wha
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.41 no.12
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    • pp.1942-1949
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    • 2016
  • This paper proposed automatic path-tracing methods for Flying Disc Golf by adopting IoT comcepts at smart-marker. We tried to implement service system by making database. Smart-marker's configurations & roles are proposed. By making test-boards and adoption to various Flying Disc Golf games, the efficiency is proved. The positions and distances captured by the smart-marker are transferred to the smart-pole per each hole. The smart-pole captured them and transfers to web-server which is databased them. The result can be searched by web or smartphone in real time.

A Study on Horizontal Moment Flight Coefficient Estimation of a Flying Disc Using Miniaturized Inertial Measurement Module (초소형 관성측정모듈을 이용한 플라잉디스크의 수평축 모멘트 미계수 추정 연구)

  • Son, Hyunjin;Lee, Ju Hwan;Lee, Young Jae;Sung, Sangkyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.5
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    • pp.385-392
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    • 2018
  • This paper suggests a new method to estimate the roll and pitch damping moment coefficients of a flying disc through sensor data from the onboard IMU module. This method can be easily performed than wind tunnel or computational fluid dynamics methods because it estimates aerodynamic coefficients simply after accumulating the inertial data through several repeated flight experiments. Estimated coefficients are applied to a simulator which is based on the flight dynamics of a flying disc. Finally, the predicted flight trajectory is compared with the true position provided by GPS, which demonstrated the validity of the proposed estimation method.

Application Design of FlyingDisc with GPS and Gyro Sensors (GPS와 자이로센서를 결합한 플라잉 디스크의 활용설계)

  • Kang, Kyungmo
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2015.05a
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    • pp.517-518
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    • 2015
  • In this research, the application of GPS and Gyro sensor based FlyingDisc with the value of 3D position and circulation sensors was proposed for school physical education. 3D Unity for 3 dimensional expression of sensors was applied for the 3D position and circulation direction from the FlyingDisc.

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A comparative analysis of the kinematical characteristics of Forehand & Backhand Flying Disc Throwing (플라잉디스크 포핸드 및 백핸드 던지기 동작의 운동학적 특성 비교)

  • Kim, Mee-Hyang;Park, Jong-Chul;Byun, Kyung-Seok
    • Journal of Digital Convergence
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    • v.17 no.12
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    • pp.555-563
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    • 2019
  • This study was to provide quantitative basic data on the forehand and backhand throw movements of flying disks. For this purpose, the kinematic variables were calculated using the three-dimensional motion analysis system. A comprehensive analysis of the study variables showed that it is important to throw flying disks accurately as well as far away, so in P2 and P3 it is necessary to control forward movement and concentrate on the rotation of the joints. In addition, rotational force transfer from pelvis to body is considered important for efficient rotational movement. The forehand was found to mainly utilize the movement of the upper extremity joint to perform throwing motion, while the backhand throw was found to be relatively utilized for the rotation of the torso and pelvis. Based on the quantitative data of this study, we hope that it can be used as a basic material for on-site training of Flying Discs.

Estimation of the Aerodynamics of UFO-Type Aircraft as a Future VTOL Aircraft (미래 수직이착륙 항공기로서의 UFO형 항공기 공기역학 추정)

  • Han, Cheolheui
    • Journal of Institute of Convergence Technology
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    • v.5 no.2
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    • pp.1-6
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    • 2015
  • Flying Saucer(flying disk type UFO) is a rotating disk that flies through the air. Thus, the aerodynamical features of the Flying Saucer can be estimated by taking a close look on the aerodynamics of the rotating disk. In the present paper, the aerodynamics of the rotating disk are reviewed focusing on the their application to the possibility of the UFO type VTOL aircraft. Finally, a combination of Avro Aircraft and Frisbee concepts is suggested as a possible new UFO type VTOL aircraft.

Aerodynamic analysis of disc type flying-object and flying-wing (원반형 비행체와 전익기의 공력특성 분석)

  • Lee, Yeong-Jun;An, Hyeon-Jin;Kim, Byeong-Su
    • Proceeding of EDISON Challenge
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    • 2014.03a
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    • pp.550-555
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    • 2014
  • 전익기는 전쟁 중 등장해 활약했다는 점과 그 독특한 형태로 유명세를 타기 시작한 비행체의 한 종류이다. 공기역학적으로 동일한 속도로 비행할 때 일반적인 항공기와 비교해서 적은 동력으로 더 멀리 날수 있는 전익기의 특성과 그 발전방향을 보았을 때 동체의 익면적이 넓어 생기는 특성을 극대화 시키면서 더욱 독특한 형태의 비행체로 나타나는 모습이 원반형 비행체이다. 본 연구는 EDISON Simulation을 활용한 두 비행체의 공력특성 비교를 통해 실제로 원반형 비행체가 많이 쓰이지 않는 이유와 그 장단점에 대한 데이터를 확보했으며 특히 원반형 비행체의 경우 Cockpit 유무와 그 크기에 따라 실속각이 커지는 것을 확인하였다.

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3D 플라잉 디스크의 회전 운동에 따른 비정상 유동 해석

  • Park, Da-Un;Kim, Tae-Uk
    • Proceeding of EDISON Challenge
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    • 2016.11a
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    • pp.4-8
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    • 2016
  • 본 연구에서는 플라잉 디스크를 이용하여 회전 운동의 유무에 따른 공력특성의 변화를 비교 분석하였다. 회전 운동이 발생하면 표면에 비대칭적으로 압력이 분포하기 때문에 롤링 모멘트가 발생하고 마그너스 효과로 측력이 발생하고 피칭모멘트, 회전감쇠모멘트가 발생하고 롤 안정성이 증가한다.

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'Plastic' Axial Flux Machines: Design and Prototyping of a Multi-Disc PM Synchronous Motor for Aircraft Applications

  • Cerchio M.;Griva G.;Profumo F.;Tenconi A.
    • KIEE International Transaction on Electrical Machinery and Energy Conversion Systems
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    • v.5B no.3
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    • pp.207-214
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    • 2005
  • After more than 100 years of development, rotating electric machines are a mature industrial product. Nevertheless, improvements are still possible for specific applications, and it is likely that the major evolution will be promoted by new materials and unconventional structures. Till now, plastic materials are an infrequent choice for the electric machines structural parts, but pioneering applications, such as aeronautical components, let some technological scouting: a low-weight/high-efficiency plastic axial flux motor for a solar flying platform is presented as an example of combined new-material/new-geometry development. The basic design aspects and the prototyping choices are presented and discussed together with the first experimental results.

지면효과를 고려한 비행체에 따른 공력 특성 분석

  • Kim, Tae-Uk;Park, Da-Un
    • Proceeding of EDISON Challenge
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    • 2016.11a
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    • pp.58-62
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    • 2016
  • 본 연구에서는 지면효과의 영향을 비행체의 형상에 따라 비교하기 위해 에어포일, 플랩을 장착한 에어포일 그리고 플라잉디스크를 EDISON_CFD를 통해 해석하고자 한다. 받음각 $0^{\circ}$, $5^{\circ}$, $10^{\circ}$에 대하여 마하수 0.18, 단위 길이 당 레이놀즈수 $3.78{\times}10^{-5}/m$의 유동조건에서 2차원 범용 소프트웨어인 KFLOW_EDISION_13의 S-A Turbulent Model을 이용하여 지면과의 높이를 형상 코드길이를 기준으로 0.25c, 0.5c, 1c, 3c로 변경하면서 해석을 수행하였다. 그 결과 세 형상 모두 일반적인 지면효과인 지면과 가까울수록 양력계수는 증가, 항력계수는 감소하여 양항비가 증가하는 경향을 보여주었다. 하지만 일부 예외적인 부분을 확인하여 분석을 실시하였다.

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