• Title/Summary/Keyword: 활주거리

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Advanced Estimation Model of Runway Visual Range using Deep Neural Network (심층신경망을 이용한 활주로 가시거리 예측 모델의 고도화)

  • Ku, SungKwan;Park, ChangHwan;Hong, SeokMin
    • Journal of Advanced Navigation Technology
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    • v.22 no.6
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    • pp.491-499
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    • 2018
  • Runway visual range (RVR), one of the important indicators of aircraft takeoff and landing, is affected by meteorological conditions such as temperature, humidity, etc. It is important to estimate the RVR at the time of arrival in advance. This study estimated the RVR of the local airport after 1 hour by upgrading the RVR estimation model using the proposed deep learning network. To this end, the advancement of the estimation model was carried out by changing the time interval of the meteorological data (temperature, humidity, wind speed, RVR) as input value and the linear conversion of the results. The proposed method generates estimation model based on the past measured meteorological data and estimates the RVR after 1 hour and confirms its validity by comparing with measured RVR after 1 hour. The proposed estimation model could be used for the RVR after 1 hour as reference in small airports in regions which do not forecast the RVR.

A Study on Correlation Between Skid Distance and Pre-Braking Speed (활주거리와 제동전 속도간의 상관관계에 관한 연구)

  • Jeong, U-Taek;O, Yeong-Tae;Park, Yeong-Su;Ryu, Tae-Seon
    • Journal of Korean Society of Transportation
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    • v.29 no.3
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    • pp.115-122
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    • 2011
  • This paper investigates the accuracy of the vehicle pre-braking speed estimated based upon measured skidding distance. Driver ordinarily takes sudden braking when urgent situation is developed in the front or when the driver is involved in an unexpected situation, and the driver may be inflicted upon an accident depending on the required stopping distance. Among factors influencing the stopping distance of vehicle such as recognition response time of driver, performance of vehicle's braking device, and state of road surface etc, pre-braking speed is seemingly the most important influencing factor. Currently, in the investigating section of traffic accidents, the state of overspeed is determined by the pre-skidding speed calculated based on the length of skid mark. In order to identify the accurate cause of the accident, it is strongly recommended that estimation of pre-braking speed should be estimated taking into account speed reduction during transient time. In this study, we propose a method for estimating more accurate exact speed information of vehicle at the time of traffic accident. The outcomes from this study potentially help better understanding of the characteristics of vehicle for traffic safety in the future.

Relationships Between Pre-Skidding and Pre-Braking Speed (활주 직전과 제동 직전 속도의 상관관계 규명에 관한 연구)

  • Ryu, Tae-Seon;Jeon, Jin-U;Park, Hong-Han;Lee, Su-Beom
    • Journal of Korean Society of Transportation
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    • v.27 no.1
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    • pp.43-51
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    • 2009
  • This paper investigates the accuracy of vehicle pre-braking speed estimates based upon tire/roadway coefficient of friction (drag factor) measurements and skid mark measurements Data for pre-braking and pre-skidding speeds were collected to determine if there were any correlations between pre-braking speeds and pre-skidding speeds. Braking tests were performed on two vehicles using various measurement devices including a fifth wheel, a speed gun, and a vericom 2000. The vehicle speeds, braking distances, skid mark distances, and deceleration histories were recorded. From these data. coefficients of friction and vehicle pre-skidding speeds for the tested road surface were calculated. The pre-skidding speeds were then compared to the actual pre-braking speeds of the vehicles in order to establish relationships between pre-skidding and pre-braking speed. A correlation between the Pre-skidding speed and the actual pre-braking speed was established for the study data.

A Study on the Allowances of Aircraft Landing Distance (항공기 착륙거리의 여유분 산정에 관한 연구)

  • Noh, Kun-Soo;Kim, Woong-Yi
    • Journal of Advanced Navigation Technology
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    • v.17 no.3
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    • pp.279-284
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    • 2013
  • Among the phases of flight operations pilots feel much pressure in landing segment. There is a number of factors affecting landing safety while pilots reduce aircraft speeds and make a touchdown and stop completely. If runway length is sufficient for landing, there maybe is no problem. But it is not the case all the time. So it is necessary to confirm whether landing performance is within limits or not. Required landing distance is actual landing distance demonstrated by flight test pilot plus allowances for average airline pilots. FAR(Federal Aviation Regulations) AFM certification is based upon manual landing for dry and wet runway. Other runway conditions are not the certification basis. JAR dictates even contaminated/slippery runway is included by prescribed allowances. Automatic landing is not certification basis, so actual landing distances are provided. In this paper I would like to analyze distance allowances included in each type of runway condition. In addition there is no regulation about allowances for specific runway condition, I would suggest adequate allowances for that case.

A Study on Evaluation of Aircraft Rapid Arresting System Using the Numerical Analysis (수치해석을 이용한 항공기 과주방지 포장시스템의 평가방법에 관한 연구)

  • Lee, Young-Soo;Kim, Choon-Seon;Ha, Wook-Jai;Han, Jae-Hyun
    • International Journal of Highway Engineering
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    • v.13 no.1
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    • pp.185-195
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    • 2011
  • Aircraft-related accidents cause mass casualties and major material damages. At present, runway-related accidents in our country account for 28% of all air accidents. Furthermore, internationally 33% of all air accidents is connected with runway. To prevent these accidents, FAA mandates the installation of aircraft rapid arresting system(ARAS) at the runway end safety areas which do not meet the FAA requirements. Even if the areas satisfy the conditions, FAA recommends the installation of ARAS to ensure the safety. In accordance of the international affairs, the domestic studies for ARAS are in progress and the legal formalities for domestic adoption of ARAS is under way. In this study, we analyzed the stopping distance, drag force, vertical force and tire penetration of runway overrun to assess the performance of ARAS reasonably by using two different kinds of analysis programs. The first is ARRESTOR program adopted by FAA, and the second is LS-DYNA which is available for 3-dimensional nonlineal dynamic analysis. As a result, analytically the stopping distances between two programs are similar. The drag force is rather different, but the tendencies are similar. Later on, the 3-dimensional simulation analysis considering various air-craft condition and properties of packaging materials is necessary. In addition, ongoing development of simulation analysis program is required for more accurate analistic results.

A Study on Acceleration of Transient Brake Section and Skidding Section (불완전 제동구간과 활주구간의 감속도 변화에 대한 연구)

  • Kim, Kil Bae;Jung, Woo Teak;Ryu, Tae Sun;Oh, Young Tae
    • Journal of Korean Society of Transportation
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    • v.30 no.5
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    • pp.83-90
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    • 2012
  • Driver ordinarily takes sudden braking when urgent situation is developed or when the vehicle is involved in an unexpected accident. Therefore, the most common trace at a traffic accident scene is skid mark. Currently, in investigating traffic accident, overspeed is determined by the length of skid mark. However, in order to identify accurate cause of accident, estimation of pre-braking speed which takes into account speed reduction during transient time should be considered as a requirement. In a recent study, several ways to estimate pre-braking speed were suggested, but none considered to differentiate the decelerating transient brake section and skidding section. This study analyzed trends of decelerating transient brake section and skidding section by real braking test.

Development for Estimation Model of Runway Visual Range using Deep Neural Network (심층신경망을 활용한 활주로 가시거리 예측 모델 개발)

  • Ku, SungKwan;Hong, SeokMin
    • Journal of Advanced Navigation Technology
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    • v.21 no.5
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    • pp.435-442
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    • 2017
  • The runway visual range affected by fog and so on is one of the important indicators to determine whether aircraft can take off and land at the airport or not. In the case of airports where transportation airplanes are operated, major weather forecasts including the runway visual range for local area have been released and provided to aviation workers for recognizing that. This paper proposes a runway visual range estimation model with a deep neural network applied recently to various fields such as image processing, speech recognition, natural language processing, etc. It is developed and implemented for estimating a runway visual range of local airport with a deep neural network. It utilizes the past actual weather observation data of the applied airfield for constituting the learning of the neural network. It can show comparatively the accurate estimation result when it compares the results with the existing observation data. The proposed model can be used to generate weather information on the airfield for which no other forecasting function is available.

Comparative Analysis of Runway Ultimate Capacity using Wake Turbulence Re-Categorization (Wake Turbulence RECAT을 적용한 활주로 절대 수용량 비교 분석)

  • Jeongwoo Park;Huiyang Kim;SungKwan Ku
    • Journal of Advanced Navigation Technology
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    • v.25 no.6
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    • pp.498-509
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    • 2021
  • The wake turbulence at the wingtip of preceding aircraft may affect the normal operation of following aircraft. Aircraft are classified into four categories according to their maximum take-off weight, and horizontal separation is applied with this category matrix. The FAA and EUROCONTROL revealed that the magnitude and effect of preceding aircraft wake turbulence were smaller than the current distance separation minima suggest. This new information presents the opportunity for revising wake turbulence minima into seven categories (RECAT). This paper confirms the feasibility of implementing RECAT at major airports in South Korea using the draft of ICAO Doc. 10122. The paper also calculates the ultimate runway capacity of Incheon International Airport in South Korea using the Harris Model and comparatively analyzes the amount of runway capacity. As a result of the analysis, it was confirmed that the implementation of RECAT could increase the ultimate runway capacity of Incheon International Airport. This paper's calculation methods and results can be used as primary data for implementing RECAT in other airports.

A cephalometric study on the relationship between mandibular opening movement and morphology of craniofacial skeleton (아동의 개구운동과 두개안면골격형태의 상관성 -측모두부방사선 계측법적 연구-)

  • Kim, Min-Shil;Chung, Kyu-Rhim
    • The korean journal of orthodontics
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    • v.30 no.3 s.80
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    • pp.297-306
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    • 2000
  • Lateral cephalometric X-ray films in maximal intercuspation and maximal opening of 68 children were taken and analyzed to examine the pattern of condylar movement and to study the relationship between opening movement and morphologic factors of craniofacial skeleton. The results were as follows : 1. The mean value of maximal opening capacity was 47.1mm, condylar moving distance was 18.1mm, horizontal condyle movement was 17.5mm, vertical condyle movement was 3.8mm and condylar moving angle was $13.1^{\circ}$. 2. The maximal opening capacity had positive relationship with the length of anterior cranial base, mandible and maxillary complex and with posterior facial height and had negative relationship with articular angle, sagittal jaw relationship. 3. Vertical condyle movement and condylar moving angle had positive relationship with articular angle and had negative relationship with gonial angle. 4. Horizontal condyle movement and condylar moving distance had positive relationship with the length of maxillary complex.

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읽을거리 - 항공기 실전원리(11) - 사고원인을 밝혀라! -

  • 한국항공우주산업진흥협회
    • Aerospace Industry
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    • s.106
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    • pp.68-69
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    • 2010
  • 지난 4월10일, 오전 10시 56분쯤 러시아 모스크바 서쪽 350km에 위치한 스몰렌스크 군용공항 활주로 부근에 Tu-154 폴란드 정부 전용기가 추락하는 사고가 발생했다. 이 사고로 레흐 카친스키(Kaczynski) 폴란드 대통령 부부를 비롯한 폴란드 정부대표단 88명과 승무원 8명 등 96명의 탑승객 전원이 사망했다. 일단 러시아 정부는 관제탑의 지시를 따르지 않고 무리하게 착륙을 시도한 조종사의 과실로 보고 있으나 정치적으로 민감한 사안이라 정확한 사고원인 규명에는 다소 시간이 소요될 것으로 전망된다. 이번 사고를 통해 항공사고 원인규명을 위한 항공사고 조사에 대해 알아본다.

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