• 제목/요약/키워드: Landing Distance

검색결과 85건 처리시간 0.023초

Performance Analysis of MLAT System Receiver for Aircraft Flight Control System

  • Yoo, Sang-Hoon;Oh, Jeong-Hun;Koh, Young-Mok;Kim, Su-Hong;Sung, Tae-Kyung
    • Journal of Positioning, Navigation, and Timing
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    • 제5권1호
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    • pp.29-36
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    • 2016
  • In this paper, performance on receivers of multilateration (MLAT) system that uses ADS-B signal, which is recently becoming popular, was analyzed to overcome shortcomings of existing aircraft flight control systems or reinforce the capabilities. A link budget was analyzed using a channel model in the airport environment with regard to Local Area Multilateration (LAM) for ground-controlled landing around the airport. In order to detect signals that arrived at the receiver successfully, sensitivity of receiver was analyzed using a signal-to-noise ratio (SNR) worksheet, and a method that improves accuracy of the distance measurement was proposed by adopting a peak estimation using sampling signals. Through simulations, optimum specifications of receivers were analyzed to have high precision positioning of LAM, and accuracy of LAM distance measurements was presented.

게임 캐릭터의 점프 동작 요인이 시각적 효과에 미치는 영향 (Affection of Game Character's Jumping Motion Factors on Visual Effects)

  • 고혜영;윤선정
    • 한국게임학회 논문지
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    • 제11권4호
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    • pp.3-14
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    • 2011
  • 본 논문은 게임 캐릭터의 자연스러운 점프 동작을 위해 점프 동작요인들이 시각적 효과에 미치는 영향을 분석하였다. 우선, 자연스러운 점프동작을 보여주는 상용 게임 3개를 선정하고 각 게임에서 4가지 체형별 캐릭터 점프 영상을 추출하였다. 이것을 점프동작의 4가지 주요 원칙인, 도약시의 힘, 착지시의 충격, 착지시의 탄력성과 동작의 유연성으로 평가하였다. 그리고 점프 동작별로 시간, 거리, 각도 요인으로 측정하였다. 최종적으로, 게임 캐릭터의 시각적 효과와 동작 요인들과의 일관된 특징을 분석하여 제시하였다. 본 연구는 자연스러운 캐릭터 점프 동작 구현을 위한 기초 자료로 활용이 될 수 있을 것이다.

레이저 빔 궤적을 이용한 자동 랜딩 시스템 (Automatic Landing System using a Trajectory of Laser Beam)

  • 황진아;남기군;이장명
    • 제어로봇시스템학회논문지
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    • 제13권1호
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    • pp.39-45
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    • 2007
  • This paper proposes a method of container position measurement using automatic landing system that is estimated by a laser range finder. In the most of container position measurement methods, CCD cameras or laser scanners have been used to get the source data. However those sensors are not only weak for disturbances, for examples, the light, fog, and rain, but also the system cost is high. When the spreader arrives at the goal position, it is still swung by inertia or by wind effect. In this paper, the spreader swung data have been used to find the container position. The laser range finder is equipped in the front side of spreader. It can measure distance and relative position between spreader and container. This laser range finder can be rotated as desired by a motor. And a tilt sensor is equipped on the spreader to measure spreader sway. The relative position information between the spreader and a container using the laser range finder and tilt sensor is estimated through the geometrical analysis.

A Comparative Analysis of Business Strategies between Full Service Airlines and Low Cost Carriers in Korea

  • KIM, Byoung-Goo;KIM, Boine
    • 산경연구논집
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    • 제13권12호
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    • pp.9-22
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    • 2022
  • Purpose: Establishing a competitive advantage in the aviation market is essential as the competition among domestic airlines intensifies. Therefore, this study examined the management strategies of both large domestic airlines and low-cost airlines. Research design, data, and methodology: This study classified domestic airlines into Full Service Airlines (FSA) and Low Cost Carriers (LCC), examined each airline's current status and characteristics, and conducted case analyses of FSA and LCC based on Porter's generic competitive strategy. Results: The analyses determined that LCC primarily implemented a cost-advantage strategy, and FSA implemented a differentiation strategy. However, as competition intensified, FSA pursued cost-advantage strategies while establishing LCC through subsidiaries. There are various specific cost reduction methods, including service simplicity, scalability, high utilization, low landing fees, low-cost unit, and point-to-point flight strategies. Conclusions: LCCs are focusing on cost advantage strategies that reduce costs; however, the FSA also runs special price events that are as good as LCCs and are comparable to LCCs on some routes. Furthermore, LCC has recently expanded its mid- and long-distance routes, making competition for long-distance routes with major airlines unavoidable.

경량항공기용 착수대 안전성 확보에 대한 연구 (The study on the safety of Sea Lane for LSA)

  • 신대원
    • 한국항공운항학회지
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    • 제25권2호
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    • pp.1-11
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    • 2017
  • In this study, we surveyed the regulations of the Seaplane base and Sea Lane for the Light Sport Aircraft(LSA), and analyzed the water landing/takeoff roll distance of LSA in Korea. Based on the information, we presented the situation of the Sea Lane and the Sea Lane Protection Zone concept, to ensure the Rectangle type Sea Lane and the Omni direction type Sea Lane. We analyzed the availability elements of the safety of Sea Lane for LSA in Korea. A Rectangle type Sea Lane 350 meters long and 40 meters wide, the diameter 350 meters for the An Omni direction type Sea Lane.

지능형 이족보행로봇을 위한 센서시스템 연구 (Sensor System Study for Intelligence Biped Walking Robot)

  • 김유신;황규득;최형식;이창만
    • 제어로봇시스템학회논문지
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    • 제11권1호
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    • pp.67-76
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    • 2005
  • In this paper, An analysis on the intelligence system for a biped walking robot(BWR) was made and its results were applied to the BWR. Various sensors were applied to the developed BWR for autonomous and intelligent walk in unknown environments. To measure the distance between the object and BWR, ultrasonic sensor and infrared-rays sensor were used. To identity surrounding environments, vision system was used. Gyro sensor was used to control the posture of BWR. Also, piezoelectricity sensor was used to identity the pressure of foot landing on the surface. Sensors applied to the robot have measurement errors according to noises or walking environments. To improve the function of these sensors, influences of noise or sensing errors were minimized using a sensor fusion scheme. A gait test using the sensor fusion system was performed, and its results are presented.

Design of a Wheeled Blimp

  • Sungchul Kang;Mihee Nam;Park, Changwoo;Kim, Munsang
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.30.5-30
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    • 2001
  • This paper describes a new design of blimp having wheeled vehicle part. This system can work both on the ground using wheeled vehicle and in the air using the floating capability of the blimp part. The passive wheeled mechanism in the vehicle part enables the stable taking off, landing on as well as it is greatly helpful to keep a stationary position on the floor. On the other hand, the floating capability enables the wheeled blimp to fly freely regardless of the ground condition or obstacles. The wheeled blimp can be used as an agent robot for the tole-presence application. Using multimedia devices such as camera, speaker, LCD and microphone mounted on the blimp surface, this system can get necessary information at the local site and communicate with person from a distance. As a typical tele-presence application, the wheeled blimp is currently being developed to a tole-guidance robot working in public indoor areas such 35 exhibition halls, departments, hospitals, etc ...

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Design of a Simulator and a Controller for ABS of Airplane

  • J.W. Jeon;J.H. Shin;Lee, K.C.;D.H. Hwang;Park, D.Y.;Kim, Y.J.
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.162.3-162
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    • 2001
  • The essence of ABS(Anti-skid Brake System) control is to continuously adjust brake pressure to maintain optimum brake torque. This optimum level should balance tire and runway friction its peak value, yielding maximum braking deceleration. It influences not only the deceleration and the taxing distance of an aircraft, but also the strength and the fatigue life of the landing gear. In this paper, an ABS control algorithm is developed with a dynamics model of 5-DOFD(Degree of Freedom). The algorithm is verified by simulations and the simulation results are presented. The dynamics model is simulated by the computer.

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땅강아지의 주음성에 관한 연구 (Phonotaxis of the African Mole Cricket, Gryllotalpa africana Palisot de Beauvois)

  • 김기황
    • 한국응용곤충학회지
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    • 제32권1호
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    • pp.76-82
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    • 1993
  • 경기도 화성군 소재 한국인삼연초연구소 경작시험장 내에서 1990년과 1992년에 땅강아지(Gryllotalpa africana)의 주음성을 조사하였다. 웅성충은 지표 밑 굴의 입구로부터 유인음을 냈은데 강도는 입구 15 cm 위에서 77~80 dB 이었다. 녹음된 웅충 유인음이 직경 1.4m의 funnel중앙에 설치된 2개의 horn speaker에 의해 105~110 dB 로 증폭하여 야외에서 방사되었을 때 비상 성충이 일몰 후 약 30분부터 1.5시간 동안 유인되었다. 유인성충들 중, 14.3~16.7%는 funnel안에, 65.7~74.7%는 발음원으로부터 2 m 이내에 지면에 착지하였다. 자충률은 66.7~74.3%였는데, 이는 야외 개최군의 성비에 기인하는 것으로 보였다. funnel 안과 그 중심에서 2m 이내의 거리에 착지하는 성층수는 blacklight trap에 유인된 성층수보다 다소 많은 경향을 보였다.

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인증규정을 고려한 KLA-100항공기 고양력장치 최적화 설계 (Flap Design Optimization for KLA-100 Aircraft in compliance with Airworthiness Certification)

  • 박진환;;;김상호;이재우
    • 한국항공우주학회지
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    • 제41권8호
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    • pp.649-656
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    • 2013
  • 고양력장치는 항공기의 이착륙 및 실속성능에 큰 영향을 미친다. 그러므로, 이 논문에서는 주어진 2차원 플랩 형상에 대하여 가장 최적화된 플랩 위치와 변위각을 얻는 슬롯티드 플랩 설계 최적화 프로세스을 제안하였다. 플랩 변위각 및 Gap, Overlap을 양력을 증가시키는 주요 변수로 생각하였고, 정확한 해석결과를 위해 공력해석 소프트웨어로 ANSYS Fluent 13.0.0$^{(R)}$을 사용하였다. 최적화된 형상은 SQP(Sequential Quadratic Programming) 알고리즘을 통해 도출됐으며, 최적화된 플랩과 함께 ADSP(Aircraft Design Synthesis Program) in-house 성능해석 코드를 사용하여 항공기의 성능을 시험하였고, 이착륙 거리, 실속속도 등의 성능변수들이 KAS-VLA 인증규정을 만족하는 결과를 얻었다.