• Title/Summary/Keyword: Aircraft Allocation

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Arrival-Departure Capacity Allocation Algorithm for Multi-Airport Systems (다중공항 시스템의 도착-출발 가용량 배정 알고리즘)

  • Lee, Sang-Un
    • The Journal of the Institute of Internet, Broadcasting and Communication
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    • v.16 no.1
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    • pp.245-251
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    • 2016
  • This paper suggests a heuristic algorithm to obtain optimal solution of minimum number of aircraft delay in multi-airport arrivals/departures problem. This single airport arrivals/departures problem can be solved by mathematical optimization method only. The linear programming or genetic algorithm that is a kind of metaheuristic method is used for a multi-airport arrivals/departures problem. Firstly, the proposed algorithm selects the median minimum delays capacity in various arrivals/departures capacities at an airport for the number of aircraft in $i^{th}$ time interval (15 minutes) at each airport. Next, we suggest reallocate method for arrival aircraft between airports. This algorithm better result of the number of delayed aircraft then genetic algorithm.

Functional analysis of Avionics system for an air transport mission (항공 수송 임무 수행을 위한 Avionics 시스템의 기능 분석)

  • Song, Yun-Sub
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.17 no.3
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    • pp.40-50
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    • 2009
  • Avionics system's function for an air transport mission is analysed. The starting point for designing a Avionics system is a clear understanding of the mission requirements and the requirement allocation by the top level aircraft system. Therefore, the analysis begins by making a top-down analysis to the aircraft missions. The baseline mission is divided into segments, and each segment is subjected to a detailed analysis to establish the requirements for the Avionics system. Special attention is given to capture the key aspects of interfaces, and to incorporate them into the design.

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Resilience Allocation for Resilient Engineered System Design (복원가능 시스템 설계를 위한 복원도 할당)

  • Youn, Byeng-D.;Hu, Chao;Wang, Pingfeng;Yoon, Joung-Taek
    • Journal of Institute of Control, Robotics and Systems
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    • v.17 no.11
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    • pp.1082-1089
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    • 2011
  • Most engineered systems are designed with high levels of system redundancies to satisfy required reliability requirements under adverse events, resulting in high systems' LCCs (Life-Cycle Costs). Recent years have seen a surge of interest and tremendous advance in PHM (Prognostics and Health Management) methods that detect, diagnose, and predict the effects of adverse events. The PHM methods enable proactive maintenance decisions, giving rise to adaptive reliability. In this paper, we present a RAP (Resilience Allocation Problem) whose goal is to allocate reliability and PHM efficiency to components in an engineering context. The optimally allocated reliability and PHM efficiency levels serve as the design specifications for the system RBDO (Reliability-Based Design Optimization) and the system PHM design, which can be used to derive the detailed design of components and PHM units. The RAP is demonstrated using a simplified aircraft control actuator design problem resulting in a highly resilient actuator with optimally allocated reliability, PHM efficiency and redundancy for the given parameter settings.

Redundant Controls Allocation by a Modified Pseudo Inverse Redistribution Method (수정된 의사역행렬 재분배 기법을 이용한 여유 조종력 할당)

  • Jin, Jae-Hyun;Yoo, Chang-Sun;Ryu, Hyeok;Tahk, Min-Jea
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.9
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    • pp.65-71
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    • 2004
  • Redundant control surfaces arc adopted to modern aircraft designs because of high performance and fault tolerant control, so efficient redundancy management is necessary to take advantage of redundant control surfaces. This paper focuses on the control allocation scheme as one of redundancy management methods. A modified pseudo inverse redistribution method is proposed. The existing method sets all saturated controls as their limit values when a pseudo inverse is calculated. But the modified scheme sets only one saturated control as its limit value and redistributes remaining controls. It is shown that the proposed scheme is superior to the existing method by several numerical examples.

A Study on Congestion Change of Dual Airways between Korea-China (한·중 항로 복선화 전후 혼잡도 변화 연구)

  • Cho, Jin Ho;Baik, Ho Jong;Chang, Jo Won
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.28 no.1
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    • pp.7-13
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    • 2020
  • A significant growth in local air traffic volume is leading to airway congestion and flight delays especially for Incheon-China and Incheon-Europe sectors. A key method to increase the airway capacity is to place a supplemental airway parallel to the existing one and in cooperation between the aviation authorities between China and Korea, a dual airway track was implemented on December 6, 2018. Here, we use airline A's flight data to analyze the congestion change effect of the new airway. Results show total delay time to Europe is reduced 51% (13.4 to 6.6 minutes) as the delay distribution for 16-30 minutes, 31 minutes and greater decreased from 23.2% to 8.2% and 8.7% to 1.0% respectively. The delay to China also decreased but the drop is not as significant as flights to Europe. This is caused by the difference in flight distance, traffic volume, and characteristics of flights landing and transiting China. Flights to Europe show a broad distribution in altitude allocation and reduction in aircraft separation demonstrating the effectiveness of a dual airway track.

A Study on the Reduction of Cosmic Radiation Exposure by Flight Crew (항공승무원의 우주방사선 피폭 저감에 관한 연구)

  • Ahn, Hee-Bok;Kim, Kyu-Wang;Choi, Youn-Chul
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.28 no.1
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    • pp.1-6
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    • 2020
  • The purpose of this study is to analyze the radiation dose data of the space crew of the flight crew and to present a plan for the health management of the flight crew on the basis of the analysis. The analysis show that the average exposure dose of the flight attendants continued to rise, and the exposure dose of the flight attendants was five(5) times higher than that of the radiation workers. As a way to reduce the effects of cosmic radiation, this paper suggests appropriate personnel allocation by model, balanced allocation of high and low latitude routes by crew according to the aircraft type, and a low altitude flight plan for high latitude flight. This study will help aviation crew members understand cosmic radiation and trust in the company's policies. In the future, it will be necessary to enhance the flight safety of the crew by deriving meaningful results by analyzing data related to cosmic radiation of various routes.

A Concept on Seat Assignment Systems

  • Premasathian, Nol;Tantipisankul, Tasanee;Sinapiromsaran, Charoen
    • 제어로봇시스템학회:학술대회논문집
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    • 2003.10a
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    • pp.458-461
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    • 2003
  • This paper presents a concept on seat assignment systems. The concept is based on the assumption that customers or passengers prefer to select seats at their own choosing and allowing them to do so would fragment remaining seats. This undesirable condition may make a group of people intending to be seated together unable to find a sufficient number of consecutive seats. The concept proposed is to set aside a number of seats when the map of available seats is shown for customer's selection. A number of functions are created to allot seats to be visible for choosing according to the number and locations of the remaining seats and the number in the group of the passengers. Passengers' preferences such as window or aisle seating, front seating are taken into accounts. A primitive example of seat assignment system of a Boeing 717 aircraft, assuming the number of passengers in a group being 1, 2 or 3, is given based on the concept.

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A model-based fault diagnosis in uncertain systems

  • Kwon, Oh-Kyu;Sung, Yul-Wan
    • 제어로봇시스템학회:학술대회논문집
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    • 1990.10b
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    • pp.1210-1215
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    • 1990
  • This paper deals with the fault diagnosis problem in uncertain linear systems having undermodelling, linearization errors and noise inputs. The new approach proposed in this paper uses an appropriate test variable and the difference between system parameters which are estimated by the least squares method to locate the fault. The singular value decomposion is used to decouple the correlation between the estimated system parameters and to observe the trend of parameter changes. Some simulations applied to aircraft ergines show good allocation of the fault even though the system model has significant uncertainties. The feature of the approach is to diagnose the uncertain system through simple parameter operations and not to need complex calculations in the diagnosis procedure as compared with other methods.

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Trend Analysis of Unmanned Technology Using Patent Information

  • Park, Jaeyong;Kang, Dongsu
    • Journal of the Korea Society of Computer and Information
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    • v.22 no.3
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    • pp.89-96
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    • 2017
  • Artificial intelligence and robot technology have been received attention as core technologies of the 4th industrial revolution. This paradigm change of science technology raises the importance of unmanned technology field. This paper categorizes unmanned technology as unmanned ground system, unmanned maritime system, and unmanned aircraft system, And it analyzes 557 cases of open patents and classifies each sort of specific technology elements. After then patent information, which were classified by technology, by patent assignees, and by IPC codes, covers unmanned technology maturity, development direction of research and core technology trends. This research provides directions of unmanned technology research and diverse field technology development through cooperation with various perspectives of quantitative analysis of patents.

A Study on the Expert System development for Fire Allocation of Aircraft Artillery (항공기 및 포병 화력자산 분배 지원 전문가시스템 개발에 관한 연구)

  • 김화수;이기호;최병권
    • Proceedings of the Korea Inteligent Information System Society Conference
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    • 2000.04a
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    • pp.443-453
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    • 2000
  • 장차전의 양상은 고도의 과학전, 타격수단의 다양화 등에 따라 고속이체기동전이 t행될 것이며, 이러한 전쟁양상은 정확하고, 보다 빠른 첩보와 정보의 수집 및 분석을 통하여 아군의 신속한 의사결정 및 대응을 요구한다. 이를 위하여 첩보와 정보 수집 및 분석을 자동화하기 위한 전장정보분석 자동화에 관한 연구가 국방과학연구소 주관으로 실시되고 있다. 따라서 이와 연계된 의사결정 자동화에 관한 연구가 필요하게 되었다. 본 연구는 이러한 요구에 부응할 수 있는 전장정보를 활용한 의사결정의 중요한 한 분야인 화력분배를 자동화하기 위한 전문가시스템의 지식베이스모듈에 대한 분석 및 설계에 관한 연구이다.기존에는 화력분야에 대한 아방책 선정까지를 자동화하는 전문가시스템 개발에 대한 연구가 수행되었으나, 본 연구에서는 자동화의 효율성을 높이기 위해서 아방책 선정에서 나아가 아군 화력자산의 파괴율을 고려하고, 지휘관의 의도에 부합하는 아군 화력자산을 배분하는 전문가시스템 개발에 관한 연구를 수행하였다. 본 연구에서는 화력분배 자동화를 위하여 화력분배와 관련된 현행 업무 관련 지식을 획득 및 분석하고 이를 바탕으로 화력자산 분배를 위한 규칙도출 시 개념설계, 상세설계, 알고리즘제시, 규칙추출예시를 하였으며 본 연구결과의 기대효과는 본문을 참고 바란다.

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