• Title/Summary/Keyword: Electric Vertical Take-off and Landing Aircraft

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Research on The Crash Location and Speed Distribution of Low Altitude Fixed-Wing Aircraft (저고도 운용 고정익 항공기의 고장 시 추락지점 및 속도 분포 연구)

  • Nam, Hong-Su;Park, Bae-Seon;Lee, Hak-Tae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.1
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    • pp.59-66
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    • 2022
  • In order to solve the problem of urban traffic congestion, Urban Air Mobility (UAM) concept using Electric Vertical Take-off and Landing (eVTOL) aircraft has been gaining popularity, and many domestic and international studies are underway. However, since these aircraft inevitably fly over densely populated areas, it is essential to ensure safety, which starts with accurately analyzing the crash risk. In this paper, the locations and impact speeds of crash are computed using six degree-of-freedom simulations of an eVTOL aircraft in a fixed-wing mode. System malfunction was modeled by a sudden loss of thrust with control surfaces being stuck during cruise. Because most of these eVTOL aircraft are still under development, a methodology of constructing a six degree-of-freedom dynamics model from generic specification is also developed. The results show that the crash locations are highly concentrated right under the aircraft within a square that has an edge length similar to the cruise altitude. Speed distribution is more complicated because almost identical crash locations can be achieved by two very different paths resulting in a large variation in the speeds.

Study of Longitudinal Stability of eVTOL UAM with Tilt Rotor and Tandem Wing (Tilt Rotor와 Tandem Wing을 적용한 eVTOL UAM의 세로안정성 연구)

  • Joo Chan-Young;Kim Ha-Min;Kim Min-Jae;Min Kyoung-Soon
    • The Journal of the Convergence on Culture Technology
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    • v.9 no.6
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    • pp.941-946
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    • 2023
  • To improve the lift, cruise speed, and range of eVTOL aircraft, which are being considered as future transportation vehicles, this paper introduces the concepts of Tilt Rotor and Tandem Wing to the aircraft. We developed an aircraft and conducted flight experiments to obtain flight videos and flight logs. The results of the analysis of the flight videos and flight logs showed that the aircraft's moment was excessively forward and the attitude was not recovered. To address this problem, we modified the wing incidence angles and surface areas in XFLR5 to obtain the optimal pitching moment coefficients to ensure vertical stability. We then analyzed the redesigned aircraft, developed using CATIA, through XFLR5. The results of this study provide valuable insights, suggesting that the incorporation of Tilt Rotor and Tandem Wing designs can contribute to achieving stable pitching moment coefficients. This innovative approach offers a promising avenue to significantly enhance vertical stability in UAM vehicles, paving the way for future advancements in the field.

Conceptual design and sensitivity analysis of a tilt + stopped rotor type eVTOL using motor weight estimation formula and iterative design (모터중량 추정식과 반복 설계를 통한 틸트+정지로터형 eVTOL 개념설계 및 민감도 분석)

  • Ju-heon Lee;Taejong Kim;Seo-yoon Jang;Hui-su Jo;Ho-Yon Hwang
    • Journal of Advanced Navigation Technology
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    • v.27 no.1
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    • pp.77-95
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    • 2023
  • In this study, the conceptual design of a tilt + stopped rotor type electric vertical take-off and landing (eVTOL) aircraft was performed using design iteration. Based on Hyundai Motor's S-A1, the mission profile was defined using the concept of urban air mobility (UAM), and configuration design and aerodynamic analysis were performed using OpenVSP and XFLR5 software. After estimating the required power for the designed eVTOL, the required performance of the battery and the maximum take-off weight (MTOW) were calculated. . It was iteratively calculated using Microsoft Excel and Visual Basic Application, and a new electric motor weight estimation formula was derived. Also, the sensitivity analyses of each design variables of an eVTOL was performed using the automated program.

Object Detection Capabilities and Performance Evaluation of 3D LiDAR Systems in Urban Air Mobility Environments (UAM 환경에서 3D LiDAR 시스템을 통한 객체 검출 기능 및 성능 평가)

  • Bon-soo Koo;In-ho choi;Jaewook Hwang
    • Journal of Advanced Navigation Technology
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    • v.28 no.3
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    • pp.300-308
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    • 2024
  • Urban air mobility (UAM) is emerging as a revolutionary transportation solution to urban congestion and environmental issues. Especially, electric vertical take-off and landing (eVTOL) aircraft are expected to enhance urban mobility, reduce traffic congestion, and decrease environmental pollution. However, the successful implementation and operation of UAM systems heavily rely on advanced technological infrastructure, particularly in sensor technology. Among these, 3D light detection and ranging (LiDAR) systems are essential for detecting obstacles and generating pathways in complex urban environments. This paper focuses on the challenges of developing LiDAR-based perception solutions, emphasizing the importance and performance of object detection capabilities using 3D LiDAR. It integrates LiDAR data processing algorithms and object detection methodologies to experimentally validate the effectiveness of perception solutions that contribute to the safe navigation of aircraft. This research significantly enhances the ability of aircraft to recognize and avoid obstacles effectively within urban settings.

A Novel Cost Estimation Method for UAM eVTOLs (전기 추진 수직이착륙 도심 항공 모빌리티 항공기의 비용 예측 연구)

  • Kim, Hyunsoo;Yee, Kwanjung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.3
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    • pp.233-241
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    • 2021
  • As increasing the feasibility of the eVTOL UAM(electric vertical take-off and landing urban air mobility), numerous corporations and laboratories are conducting researches. In the aircraft development process, estimating the cost of the aircraft is essential part in terms of budgeting and commercial viability analysis. However, it is difficult to predict the cost of an eVTOL UAM owing to various configurations and little open cost information. This paper presents a novel method to predict the vehicle cost of various eVTOL configurations by modifying previous studies of the aircraft cost estimation. A vehicle cost of Wisk Cora is calculated by the presented method as an example to illuminate the method. The method is indirectly validated by comparing the vehicle costs of six representative eVTOL aircraft with those from the UAM study reports.

A Study on the AHP Analysis of initial UAM Pilot Education and Training Subjects (초기 UAM 조종사 교육훈련 과목 선정 AHP 분석 연구)

  • Sung-yeob Kim;Jung-min Choi;Jihun Choi
    • Journal of Advanced Navigation Technology
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    • v.27 no.3
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    • pp.269-273
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    • 2023
  • Based on the K-UAM roadmap, this study was conducted to select major education and training subjects necessary for the composition of the initial UAM pilot education and training curriculum. Currently, UAM aircraft have similar characteristics to rotorcraft that can take off and land vertically around VTOL functions. Therefore, in this study, the Rotary Wing Pilot Training Curriculum of the Army Aviation School, which represents Rotary Wing Flight Education, was selected as a comparative group, and education and training subjects for initial UAM pilot training were selected. First, a hierarchical structure for the AHP survey was designed based on the Army's rotorcraft pilot education and training subjects, and the AHP survey was conducted by selecting experts from each class. If the education and training subjects given as priorities through AHP analysis are applied to initial UAM pilot training, it is expected to contribute to the effect of education and training and ultimately to the safe operation of UAM.

A Study on the Prevention of Bird Collision in UAM (UAM 조류 충돌 방지대책 수립에 관한 연구)

  • Daniel Kim;Hee-duk Cho;Seung-woo Lee;Jae-woo Kim
    • Journal of Advanced Navigation Technology
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    • v.28 no.3
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    • pp.338-347
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    • 2024
  • This paper deals with the study of bird collision avoidance measures in UAM operations from an operator's perspective. Urban air traffic is defined as a next-generation transportation system that uses environmentally friendly electric vertical take-off and landing (eVTOL) aircraft to provide transportation services between key points within and around urban centers. For the successful establishment of the UAM industry, it is necessary to ensure safety issues that determine public acceptance. Among the hazards that can occur in aviation operations, preventing bird collisions in urban environments is a measure that can greatly secure operational safety and public acceptance. In addition to physical measures, procedural control measures are required to prevent bird strikes. In order to ensure the safety of UAM operations, this study aims to provide a direction for the establishment of UAM bird collision prevention measures by categorizing bird collision prevention measures into physical and procedural methods and flight sections such as takeoff, landing, and corridor sections. Through this, we hope to contribute to the improvement of the safety of the urban air traffic operation system.

UAM Traffic Flow Management Based on Milestone in Collaborative Decision-Making (협력적 의사결정체계(CDM) 마일스톤 기반 도심항공교통(UAM) 흐름관리)

  • Do-hyun Kim;Hyo-seok Chang
    • Journal of Advanced Navigation Technology
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    • v.28 no.4
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    • pp.436-441
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    • 2024
  • Urban air mobility (UAM) is an innovative air traffic management system that utilizes electric vertical take off and landing aircraft(eVTOL) to transport passengers and cargo in urban areas. The corridor can be defined as the airspace that the vehicle operates in and must be collaboratively managed. For the stable operation of UAM, it is essential to have strategic separation and a collaborative decision-making(CDM) system for cooperation and coordination among stakeholders. This study examines the application of time-based milestones from traditional air traffic flow management to the UAM system to ensure safe traffic volume and optimize air traffic flow. For traffic flow management, the milestone time information is categorized into a total of 13 key milestone time indicators based on the UAM movement status, and the sharing entities providing each time indicator and the flow of milestones are defined. Emphasizing the need for a CDM to balance UAM traffic and capacity, sharing and managing milestone information among stakeholders is expected to improve UAM aircraft departure flow and enhance operational efficiency.

Preliminary Conceptual Design of a Multicopter Type eVTOL using Reverse Engineering Techniques for Urban Air Mobility (도심항공 모빌리티(UAM)를 위한 역설계 기법을 사용한 멀티콥터형 eVTOL의 기본 개념설계)

  • Choi, Won-Seok;Yi, Dong-Kyu;Hwang, Ho-Yon
    • Journal of Advanced Navigation Technology
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    • v.25 no.1
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    • pp.29-39
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    • 2021
  • As a means of solving traffic congestion in the downtown of large city, the interest in urban air mobility (UAM) using electric vertical take-off landing personal aerial vehicle (eVTOL PAV) is increasing. eVTOL configurations that will be used for UAM are classified by lift-and-cruise, tilt rotors, tilt-wings, tilted-ducted fans, multicopters, depending on propulsion types. This study tries to perform preliminary conceptual design for a given mission profile using reverse engineering techniques by taking the multicopter type Airbus's CityAirbus as a basic model. Wetted area, lift to drag ratio, drag coefficients were calculated using the OpenVSP which is an aerodynamic analysis software. The power required for each mission section of CityAirbus were calculated, and the corresponding battery and motor were selected. Also, total weight was predicted by estimating component weights of eVTOL.