• 제목/요약/키워드: vertical takeoff

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국외 8m 이상 멀리뛰기 선수와 국내 선수들의 운동학적 비교 분석 (The Kinematic Comparison and Analysis between National Long Jumpers and Foreign long Jumpers with record of over 8 meter)

  • 류재균;장재관
    • 한국운동역학회지
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    • 제15권3호
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    • pp.133-142
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    • 2005
  • The purpose of this study was to compare of the kinematic variables from takeoff preparation to takeoff used by long jumpers who recorded over 8meters in 2002 Busan Asian Game and 2003 Daegu Universiade and 2001 national championship. The kinematic characteristics from the last three stride to takeoff at the takeoff board were analyzed such as velocities, heights and angles. The conclusion were as follows; In order to record over 8meters the national long jumpers should have under 5cm height variation at the penultimate stride of the run-up. In the approach phase the horizontal velocity of the jumpers should reach to 10m/s in touchdown at takeoff board The vertical velocity must have 3.75m/s simultaneously in order to record 8meters. The jumpers need to continue talent of the horizontal velocity in touchdown at takeoff board and require jumping power of the takeoff leg at takeoff board The appropriate body variation range ratio between takeoff and touchdown should be 1.2 vs 1 and the trunk angle at touch down on the board should be close to the erect posture for higher body flight.

곤충 모방 날갯짓 비행체의 안정적인 수직 이륙 비행 구현 (Demonstration of Stable Vertical Takeoff of an Insect-Mimicking Flapping-Wing System)

  • 판 호앙 부;트롱 쾅 트리;구옌 쿠옥 비엣;박훈철;변도영;구남서
    • 제어로봇시스템학회논문지
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    • 제18권2호
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    • pp.76-80
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    • 2012
  • This paper demonstrates how to implement inherent pitching stability in an insect-mimicking flapping-wing system for vertical takeoff. Design and fabrication of the insect-mimicking flapping-wing system is briefly described focusing on the recent modification. Force produced by the flapping-wing systems is estimated using the UBET (Unsteady Blade Element Theory) developed in the previous work. The estimation shows that the wing twist placed in the modified system can improve thrust production for about 10 %. The estimated thrust is compared with the measured thrust, which proves that the UBET provides fairly good estimations for the thrust produced by the flapping-wing systems. The vertical takeoff test shows that inherent pitching stability can be implemented in an insect-mimicking flapping-wing system by aligning the aerodynamic force center and center of gravity.

A Study on the Application of Human Factors to the Introduction of PAV & UAM

  • Ahn, Kyung Su;Jeong, Won Kyong
    • 한국항공운항학회지
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    • 제28권4호
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    • pp.171-175
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    • 2020
  • The present and future cities are expanding, and the noise and environmental pollution in cities are getting worse day by day, causing saturation of road and subway traffic. As a result, citizens are spending a great deal of time and money. The use of the sky as a measure to solve this problem has become a reality. However, airplanes that require airstrips and noisy helicopters are difficult to use in cities. As a solution, PAVs and UAMs that generate low noise and enable vertical takeoff and landing using electric energy, motor, hybrid, and hydrogen energy, are attracting attention, with its practicality being promoted in many countries. The development of urban environment and technology has led to the emergence of Personal Air Vehicle (PAV), Vertical Takeoff and Landing (eVTOL), and Urban Air Mobility (UAM) for shipping. Though currently at the level of testing, general commercialization of these air transport means is expected in the next five to fifteen years. This study suggests a plan on the application of human factors to the introduction of PAV and UAM.

수직이착륙기 설계 및 제작 (The design and production of the Vertical takeoff and landing aircraft)

  • 이웅희;박용수;배재성
    • 항공우주시스템공학회지
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    • 제2권4호
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    • pp.19-24
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    • 2008
  • In this study gives detail on the composition and process of Quad-rotor blade Vehicle. It may seem simple but we have many trouble because of many subtleties. Unless designed carefully, it is very difficult to control of stability by reason of disturbances in the air and unbalance in the motor. We want to have a more stable output so add other electronics supplement, and change the battery in oder to increasing thrust. It cannot be done quickly, nor cheaply because it is more difficult than first ideas that control of Quad-rotor. But we complete manufacture of basically controllable vertical takeoff and landing aircraft.

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세계 정상급 여자 허들 선수들이 사용하는 허들 넘는 기술의 운동학적 분석 (Kinematic Analysis of the Hurdle Clearance Technique used by World Top Class Women's Hurdler)

  • 류재균;장재관
    • 한국운동역학회지
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    • 제21권2호
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    • pp.131-140
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    • 2011
  • The purpose of this study was to evaluate the kinematic characteristics of 5th hurdle clearance during the 100m hurdle final competition at the 2010 Colorful DaeGu pre-championship meeting. This study was also intended to provide the technical data for better performance for preparing the 2011 world championship. Lee and Jung need to change technical movement by reducing the distance of the take-off point from the hurdle and by decreasing the vertical velocity of the C.G.(center of gravity) at the takeoff. Powell's angle of the take-off leg showed bigger at the touchdown and smaller at the takeoff comparing to Lee's and Jung's. Furthermore, Powell's horizontal velocity of the C.G. was maintained at the takeoff and touchdown. So, Lee and Jung need to change angle of the take-off leg the same as Powell's. Both Lee and Jung need to increase the angle of landing leg at the touchdown. In addition to increasing the angle Jung needs to improve the knee and ankle velocity with the hurdling leg.

도마에서 Driggs 기술의 운동학적 사례-분석 (The Kinematic Analysis of Driggs Motion in Horse Vaulting - a case study)

  • 김윤지
    • 한국운동역학회지
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    • 제15권3호
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    • pp.175-183
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    • 2005
  • This study investigates the kinetic characteristics of the Driggs motion in horse vaulting by stages through the three-dimensional video analysis of YTY and TABARA who won a high score and a low score respectively from the Driggs motion in horse vaulting during the Daegu Universiade 2003, which involves putting one's hands on the horse vaulting rotating sideways, stretching and rotating backward in the air, and twisting 900 degrees, so as to help develop the techniques of Korean gymnastic athletes. From the analyses of the duration of body center, horizontality, vertical position and horizontality, vertical speed and angle factors for each of four phases from the contact of the board to the takeoff from the horse vaulting. I arrived at the following conclusions: 1. It was found that the motion of bending oneself forward while rapidly stretching the knee joint when taking off from the board increases the horizontal speed of body center and shortens the time of the first jump. 2. It was found that S1 who won a high score shortened the time of the contact and takeoff from the horse vaulting and enlarged the shoulder joint angle for full blocking motion. It was also found that horizontal speed decreased while vertical speed increased when you rapidly stretch the right elbow joint while taking off from the horse vaulting. 3. It was found that horizontal distance was shortened to increase the height and time of staying in the air during the second jump.

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

  • 최자성;이석현;백정선;황호원
    • 한국항공운항학회지
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    • 제29권1호
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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」.

2D 게임을 위한 수직 이착륙 비행체의 물리 기반 시뮬레이션 (Physics-based Simulation of a VTVL Vehicle for 2D Games)

  • 문석진;최민규
    • 한국컴퓨터그래픽스학회논문지
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    • 제19권1호
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    • pp.21-25
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    • 2013
  • 최근 활발하게 발표되고 있는 물리 기반 이차원 캐주얼 게임들은이차원상의 제어에 따른 편의성과 사용자의 물리적 경험에 따른 직관적인 조작성 및 친숙함에 힘입어 큰 사용자층을 형성하고 있다. 본 논문에서는 비행 조작에서의 편의 성을 보장하며 물리적 사실성에 따른 흥미를 유발할 수 있는 물리 기반 이차원 비행 시뮬레이션 게임을 고려한다. 우선 이에 적합한 두 개의 추진기를 가진 수직 이착륙 비행체 모델을 제시한다. 각 추진기에서의 추력을 두 개의 조이스틱 등을 사용하여 직접 제어 할 수 있다. 하지만 이와 같은 기계식 조정 방식을 통해 고난이도의 역동적 곡예비행을 하기 위해서는 꽤 많은 연습이 필요하다. 보다 손쉽고 직관적인 조작을 위하여 PD 제어를 통해 비행체의 속도 및 위치를 빠르고 정확하게 제어할 수 있는 전기식 조정 방식(fly-by-wire)을 제안한다. 제안된 비행체 및 비행 제어 기법은 여러 흥미로운 이차원 게임 제작에 사용될 수 있을 것으로 기대된다.

도심항공 모빌리티(UAM)의 국내 적용을 위한 수직이착륙장 설계 요구조건 분석 및 형상 제안 (Design Requirement Analysis and Configuration Proposal of a Vertiport for Domestic Applications of the Urban Air Mobility)

  • 안병선;황호연
    • 한국항행학회논문지
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    • 제25권1호
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    • pp.40-51
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    • 2021
  • 본 논문에서는 도심항공 모빌리티(UAM) 시스템을 국내에서 운용하기 위해 필요한 국내외 규정을 분석하여 수직이착륙장의 설계 요구 조건을 도출하고 이착륙 패드의 크기를 규정하였으며, 이를 바탕으로 수직이착륙장 형상을 제안하였다. 먼저, 인구 밀집도가 높은 수도권에 대해 국토교통부에서 제시한 실증노선을 기준으로 수직이착륙장의 시범 위치를 선정하고 각 위치의 특징을 분석하였으며 크기를 측정하여 수직이착륙장의 설치 가능 수를 파악하였다. 이후 수직이착륙장 운영에 필요한 변수들을 설정하여 동시운용과 주기장 수에 따른 시간당, 하루, 한 달 동안의 항공기 운용 가능 대수, 수용 가능 인원, 효율성 등을 계산하였다. 마지막으로, CATIA를 사용하여 가상의 수직이착륙장 형상을 설계요구조건을 적용하여 구현하였다.

Kinematic Analysis of Back Somersault Pike According to Skill Level in Platform Diving

  • Park, Jiho;Yoon, Sukhoon
    • 한국운동역학회지
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    • 제27권3호
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    • pp.157-164
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    • 2017
  • Objective: The purpose of this study was to investigate kinematic differences in back pike somersault in platform diving according to skill level and to apply the findings to improve performance. Method: Korean divers participating in this study were divided into a skilled group (age: $21.6{\pm}4.16y$, height: $1.68{\pm}0.03m$, weight: $62.0{\pm}3.94kg$, career: $12.6{\pm}5.13y$) and a less-skilled group (age: $20.6{\pm}2.7y$, height: $1.72{\pm}0.05m$, weight: $64.8{\pm}6.76kg$, career: $12.2{\pm}2.49y$) and an independent t-test was performed to analyze differences between groups at the moment of takeoff. Results: The two groups showed significant differences in displacement and velocity of center of mass (COM), takeoff angle, hip joint angle, knee joint angular velocity, and hip joint angular velocity at the takeoff (p<.05), and significant differences in displacement of COM, hip joint, and ankle joint during flight (p<.05). Conclusion: For a successful back pike, the COM should rise quickly in the vertical direction and the hip joint angle and angular velocity should increase. To improve performance, the back pike turn should be practiced on the ground before an attempt on a 10-m platform, to stretch the ankle and knee joints and enable quick flexion of the hip joint when turning in flight.