• 제목/요약/키워드: reconnaissance

검색결과 367건 처리시간 0.024초

Modeling wind load paths and sharing in a wood-frame building

  • He, Jing;Pan, Fang;Cai, C.S.
    • Wind and Structures
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    • 제29권3호
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    • pp.177-194
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    • 2019
  • While establishing adequate load paths in the light-frame wood structures is critical to maintain the overall structural integrity and avoid significant damage under extreme wind events, the understanding of the load paths is limited by the high redundant nature of this building type. The objective of the current study is to evaluate the system effects and investigate the load paths in the wood structures especially the older buildings for a better performance assessment of the existing building stock under high winds, which will provide guidance for building constructions in the future. This is done by developing building models with configurations that are suspicious to induce failure per post damage reconnaissance. The effect of each configuration to the structural integrity is evaluated by the first failure wind speed, amajor indicator beyond the linear to the nonlinear range. A 3D finite-element (FE) building model is adopted as a control case that is modeled using a validated methodology in a highly-detailed fashion where the nonlinearity of connections is explicitly simulated. This model is then altered systematically to analyze the effects of configuration variations in the model such as the gable end sheathing continuity and the gable end truss stiffness, etc. The resolution of the wind loads from scaled wind tunnel tests is also discussed by comparing the effects to wind loads derived from large-scale wind tests.

Implementation of Educational UAV with Automatic Navigation Flight

  • Park, Myeong-Chul;Hur, Hwa-ra
    • 한국컴퓨터정보학회논문지
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    • 제24권8호
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    • pp.29-35
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    • 2019
  • This paper proposes a UAV equipped with an automatic control system for educational purposes such as navigation flight or autonomous flight. The proposed UAV is capable of automatic navigation flight and it is possible to control more precisely and delicately than existing UAV which is directly controlled. And it has the advantage that it is possible to fly in a place out of sight. In addition, the user may arbitrarily change the route or route information to use it as an educational purpose for achieving the special purpose. It also allows you to check flight status by shooting a video during flight. For this purpose, it is designed to check the image in real time using 5.8GHz video transmitter and receiver. The flight information is recorded separately and used as data to judge the normal flight after the flight. The result of the paper can be flighted along the coordinates specified using GPS information. Since it can receive real-time video, it is expected to be used for various education purposes such as reconnaissance of polluted area, achievement of special purpose, and so on.

Bio-inspired Evasive Movement of UAVs based on Dragonfly Algorithm in Military Environment

  • Gudi, Siva Leela Krishna Chand;Kim, Bo-sun;Silvirianti, Silvirianti;Shin, Soo Young;Chae, Seog
    • Journal of information and communication convergence engineering
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    • 제17권1호
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    • pp.84-90
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    • 2019
  • Applications of unmanned aerial vehicles (UAVs) in the military environment have become popular because they require minimum human contribution and can avoid accidents during missions. UAVs are employed in various missions such as reconnaissance, observation, aggression, and protection. Consequently, counter-measures, known as anti-drone technologies, have been developed as well. In order to protect against threats from anti-drone technologies and enhance the survivability of UAVs, this study proposes an evasive measure. The proposed bio-inspired evasive maneuver of a UAV mimics a dragonfly's irregular flight. The unpredictable UAV movement is able to confuse enemies and avoid threats, thereby enhancing the UAV's survivability. The proposed system has been implemented on a commercial UAV platform (AR Drone 2.0) and tested in a real environment. The experiment results demonstrate that the proposed flight pattern has larger displacement values compared to a regular flight maneuver, thus making the UAV's position is difficult to predict.

초소형위성 SAR 탑재체 운용모드 설계 및 성능분석 (Operation Mode Design and Performance Analysis for Small Satellite SAR Payload)

  • 박종민;김동식;김완식;김종필
    • 한국인터넷방송통신학회논문지
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    • 제19권5호
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    • pp.169-173
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    • 2019
  • 본 논문에서는 SAR 탑재체의 운용모드 설계방안 및 설계결과 그리고 주요성능에 대한 분석 결과를 제시하였다. SAR 시스템 설계는 요구사항을 만족하는 주요변수의 설계값 도출로 진행된다. 저궤도에서 운용하는 100kg 미만의 초소형위성을 가정하고 고해상의 영상을 위하여 X-대역의 주파수를 선정하였다. 주어진 설계 요구사항을 반영하여 주파수 대역폭, 관측영역 설계, 안테나 설계를 진행하고, 설계결과를 반영하여 목표 영상품질인 NESZ 만족여부를 확인하였다. 또한 설계값을 반영하여 관측영역별로 최적의 PRF를 설계하였다. 또한 소형, 경량화를 위한 안테나 형태를 제안하였다. 또한 설계된 변수를 적용하여 체계성능을 확인하였다.

A comparative study of different active heave compensation approaches

  • Zinage, Shrenik;Somayajula, Abhilash
    • Ocean Systems Engineering
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    • 제10권4호
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    • pp.373-397
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    • 2020
  • Heave compensation is a vital part of various marine and offshore operations. It is used in various applications, including the transfer of cargo between two vessels in the open ocean, installation of topsides of an offshore structure, offshore drilling and for surveillance, reconnaissance and monitoring. These applications typically involve a load suspended from a hydraulically powered winch that is connected to a vessel that is undergoing dynamic motion in the ocean environment. The goal in these applications is to design a winch controller to keep the load at a regulated height by rejecting the net heave motion of the winch arising from ship motions at sea. In this study, we analyze and compare the performance of various control algorithms in stabilizing a suspended load while the vessel is subjected to changing sea conditions. The KCS container ship is chosen as the vessel undergoing dynamic motion in the ocean. The negative of the net heave motion at the winch is provided as a reference signal to track. Various control strategies like Proportional-Derivative (PD) Control, Model Predictive Control (MPC), Linear Quadratic Integral Control (LQI), and Sliding Mode Control (SMC) are implemented and tuned for effective heave compensation. The performance of the controllers is compared with respect to heave compensation, disturbance rejection and noise attenuation.

민/군 지구관측위성 개발 동향 및 향후 국내 위성사업 방향 (Development Trends of Civil/Military Earth Observation Satellite and Direction of Prospective Domestic Satellite Projects)

  • 정현재;최윤혁;황인영;서인호;김경근
    • 한국항공우주학회지
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    • 제49권9호
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    • pp.791-800
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    • 2021
  • 본 논문은 우주 선진국 및 우리나라의 민/군 지구관측위성 개발 동향에 대해 조사하였으며, 국내 위성사업의 현황 및 향후 방향에 대해 기술하였다. 우주 선진국의 민/군 지구관측위성 개발 동향은 미국, 러시아, 프랑스, 독일, 이탈리아, 이스라엘, 중국 그리고 일본에 대해 조사하였으며, 이를 바탕으로 향후 지구관측위성 개발 방향에 대해 예측하였다. 일반적으로 위성 개발이라는 용어는 위성시스템을 구성하는 위성체, 지상체 및 발사체 등을 모두 포함하여 개발하는 개념으로 사용되지만, 본 논문에서는 위성 시스템이 아닌 위성체 자체의 개발을 중점으로 사용하였다.

Operational Risk Assessment for Airworthiness Certification of Military Unmanned Aircraft Systems using the SORA Method

  • Namgung, Pyeong;Eom, Jeongho;Kwon, Taehwa;Jeon, Seungmok
    • 항공우주시스템공학회지
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    • 제15권4호
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    • pp.64-74
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    • 2021
  • Unmanned Aircraft Systems (UAS) are rapidly emerging not only as a key military power, such as surveillance and reconnaissance for military purposes but also as a new air transportation means in the form of Urban Air Mobility (UAM). Currently, airworthiness certification is carried out focused on the verification of technical standards for flight safety suitability of aircraft design in accordance with the Military Aircraft Flight Safety Certification Act and does not employ the model for operational risk assessment for mission areas and airspace. In this study, in order to evaluate the risk of the mission area from the perspective of the UAS operator, a risk assessment simulation has been conducted by applying the Specific Operations Risk Assessment (SORA) model to the operating environment of the Korean military UAS. Also, the validity of the SORA model has been verified through the analysis of simulation results, and a new application plan for airworthiness certification of the military unmanned aerial system has been presented.

Transverse buckling analysis of spatial diamond-shaped pylon cable-stayed bridge based on energy approach

  • Zheng, Xing;Huang, Qiao;Zheng, Qing-gang;Li, Zhen
    • Structural Engineering and Mechanics
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    • 제83권1호
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    • pp.123-134
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    • 2022
  • The stability of cable-stayed bridges is an important factor considered during design. In recent years, the novel spatial diamond-shaped bridge pylon has shown its advantages in various aspects, including the static response and the stability performance with the development of cable-stayed bridge towards long-span and heavy-load. Based on the energy approach, this paper presents a practical calculation method of the completed state stability of a cable-stayed bridge with two spatial diamond-shaped pylons. In the analysis, the possible transverse buckling of the girder, the top pylon column, and the mid pylon columns are considered simultaneously. The total potential energy of the spatial diamond-shaped pylon cable-stayed bridge is calculated. And based on the principle of stationary potential energy, the transverse buckling coefficients and corresponding buckling modes are obtained. Furthermore, an example is calculated using the design parameters of the Changtai Yangtze River Bridge, a 1176 m cable-stayed bridge under construction in China, to verify the effectiveness and accuracy of the proposed method in practical engineering. The critical loads and the buckling modes derived by the proposed method are in good agreement with the results of the finite element method. Finally, cable-stayed bridges varying pylon and girder stiffness ratios and pylon geometric dimensions are calculated to discuss the applicability and advantages of the proposed method. And a further discussion on the degrees of the polynomial functions when assuming buckling modes are presented.

한국공군의 첨단 항공기 도입에 따른 안전관리방안 연구 (A Study on Safety Management Methods for Introduction of the Advanced Aircraft by the Republic of Korea Air Force)

  • 구본언;이강준
    • 한국항공운항학회지
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    • 제29권2호
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    • pp.36-46
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    • 2021
  • The purpose of this study is to ensure safety by proactively identifying hazards that could be derived from changes in mission form and environment as the advanced aircraft such as F-35A stealth fighter, KC-330 Multi-role transport and tanker, RQ-4B high altitude unmanned reconnaissance aircraft, etc are introduced that the Republic of Korea Air Force(ROKAF) has never been operated so far. To this end, the safety management methods based on proactive and predictive approaches used in advanced countries(US Air Force, UK Royal Air Force, Royal Australian Air Force) operating aircraft types same or similar things being newly powered by the ROKAF were reviewed. In addition, the direction for improvement of the safety management methods operating in the ROKAF and the measures necessary for establishment of the new safety management techniques to be applied were suggested.

Assessment of seismic damage inspection and empirical vulnerability probability matrices for masonry structure

  • Li, Si-Qi;Chen, Yong-Sheng;Liu, Hong-Bo;Du, Ke;Chi, Bo
    • Earthquakes and Structures
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    • 제22권4호
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    • pp.387-399
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    • 2022
  • To study the seismic damage of masonry structures and understand the characteristics of the multi-intensity region, according to the Dujiang weir urbanization of China Wenchuan earthquake, the deterioration of 3991 masonry structures was summarized and statistically analysed. First, the seismic damage of multistory masonry structures in this area was investigated. The primary seismic damage of components was as follows: Damage of walls, openings, joints of longitudinal and transverse walls, windows (lower) walls, and tie columns. Many masonry structures with seismic designs were basically intact. Second, according to the main factors of construction, seismic intensity code levels survey, and influence on the seismic capacity, a vulnerability matrix calculation model was proposed to establish a vulnerability prediction matrix, and a comparative analysis was made based on the empirical seismic damage investigation matrix. The vulnerability prediction matrix was established using the proposed vulnerability matrix calculation model. The fitting relationship between the vulnerability prediction matrix and the actual seismic damage investigation matrix was compared and analysed. The relationship curves of the mean damage index for macrointensity and ground motion parameters were drawn through calculation and analysis, respectively. The numerical analysis was performed based on actual ground motion observation records, and fitting models of PGA, PGV, and MSDI were proposed.