• Title/Summary/Keyword: flight behavior

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Effects of Authentic Leadership on Positive Psychological Capital and Change-Oriented Organizational Citizenship Behavior in Flight Attendants -Focusing on the Mediating Effect of Positive Psychological Capital- (항공사 승무원의 진정성리더십이 긍정심리자본 및 변화지향 조직시민행동에 미치는 영향 -긍정심리자본의 매개효과를 중심으로-)

  • Park, Jung-Min;Ha, Dong-Hyun
    • The Journal of the Korea Contents Association
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    • v.16 no.9
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    • pp.51-65
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    • 2016
  • The purpose of this study was to examine whether authentic leadership influenced positive psychological capital and change-oriented organizational citizenship behavior(CO-OCB) in airline service context. Moreover, this study was designed to test the mediating effect of positive psychological capital between authentic leadership and CO-OCB to provide fundamental and practical information for airline industry. A convenience sample of 390 flight attendants was surveyed and a total of 377 usable questionnaires were analyzed. Then hypotheses were tested using structural equation modelling(SEM). The results were as follows. Firstly, authentic leadership was divided into 'self-awarenese', 'relational transparency', internalized moral perspective' and 'balanced process'. Secondly, 'self-awarenese' and 'internalized moral perspective' influenced positive psychological capital. Thirdly, positive psychological capital influenced CO-OCB. Fourtjly, positive psychological capital had mediating effects partially between authentic leadership and CO-OCB.

The Effect of Flight Attendant's Psychological Empowerment on the Service Behavior 'by and beyond' CSM (객실승무원의 심리적임파워먼트가 CSM기반과 CSM초월 서비스행동에 미치는 영향)

  • Lee, SooKyoung
    • Journal of Korea Society of Industrial Information Systems
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    • v.26 no.6
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    • pp.97-118
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    • 2021
  • This study empirically examines the effect of the psychological empowerment of airline cabin crews on customer-focused job performance attitude, service behavior by CSM, and service behavior beyond CSM. The research model and associated hypotheses were verified with the structural equation model. The findings of the study reveal that psychological empowerment has a effect on customer-focused job performance attitude and service behavior by CSM, but no effect on service behavior beyond CSM. And it is also shown that customer-focused job performance attitude has an effect on service behavior by CSM but no effect on service behavior beyond CSM. In addition, customer-focused job performance attitude shows a mediating effect between psychological empowerment and service behavior by CSM. On the other hand, it is analyzed that there is no mediating effect between psychological empowerment and service behavior beyond CSM. This study implies that the psychological empowerment and customer-focused job performance attitude of cabin crews are important at point of contact with customers to improve service quality, and psychological empowerment reinforces service behavior by CSM on the premise of customer-focused job performance attitude.

UAV Swarm Flight Control System Design Using Potential Functions and Sliding Mode Control (포텐셜 함수와 슬라이딩 모드 제어기법을 이용한 무인기 군집비행 제어기 설계)

  • Han, Ki-Hoon;Kim, You-Dan
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.5
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    • pp.448-454
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    • 2008
  • This paper deals with a behavior based decentralized control strategy for UAV swarming utilizing the artificial potential functions and the sliding mode control technique. Individual interactions for swarming behavior are modeled using the artificial potential functions. The motion of individual UAV is directed toward the negative gradient of the combined potential. For tracking the reference trajectory of UAV swarming, a swarming center is considered as the object of control. The sliding-mode control technique is adopted to make the proposed swarm control strategy robust with respect to the system uncertainties and the varying mission environment. Numerical simulation is performed to verify the performance of the proposed controller.

Fatigue Crack and Delamination Behavior in the Composite Material Containing n Saw-cut and Circular Hole (I) - Aramid Fiber Reinforced Metal Laminates - (소컷 및 원공 주위의 피로균열 형태변화와 층간분리거동 (I) - 아라미드섬유 강화 금속적층재의 경우 -)

  • Song, Sam-Hong;Kim, Cheol-Woong
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.27 no.1
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    • pp.58-65
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    • 2003
  • The aramid fiber reinforced metal laminates(AFRMLs) used for the wing part fair flight suffer the cyclic bending moment of variable amplitude during service. The fatigue crack propagation and delamination behavior in AFRMLs containing a saw-cut and circular hole was investigated using the average stress criterion(ASC) model. Mechanical tests were carried out using the cyclic bending moment of 4.9 N . m and delamination was observed by ultrasonic C-scan images. In case of AFRMLs containing a saw-cut fatigue crack propagated in aluminum matrix, inducing delamination. However, in case of AFRMLs containing a circular hole, delamination formed with two types under cyclic bending moment of 4.9 N . m. First, delamination formed along the fatigue crack in aluminum matrix. Second, delamination formed without any fatigue crack around the circular hole. Therefore, delamination was formed depending on the stress distribution near the circular hole.

Numerical Simulation of Inkjet Drop Formation in Piezo Inkjet Head (피에조 잉크젯 헤드의 액적 토출 형상 전산해석)

  • Joo, Youngcheol;Park, Sangkug;Kwon, Key-Si
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.17 no.7
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    • pp.641-647
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    • 2016
  • A drop-on-demand inkjet is used widely for various applications. Therefore, it is important to understand the jetting behavior of the drop from the piezo inkjet. In this study, to predict the jetting behavior, VOF (Volume-of-Fluid) simulation techniques were used and compared with the experimental results. The experimentally measured meniscus movement was used as the input data for the simulation. To verify the simulation, the measured jetting behavior of the mixture fluids of ethylene glycol and IPA (isopropyl alcohol), which has a mixing ratio of 50:50, was used. The numerical simulation of the drop formation using various mixture ratios and its comparison with the measured drop formation confirmed that the proposed method can predict the actual jetting. On the other hand, the satellite drop behavior showed slight differences because the small sized droplet is subject to a more aerodynamic effect during flight because the kinetic energy of the satellite droplet is far smaller than that of the main droplet.

Characterization of a Magnetron Sputtering Cathode by a 3D Particle Model (3차원 입자 모델을 이용한 마그네트론 스퍼터링 음극의 특성 분석)

  • Joo, Jung-Hoon
    • Journal of the Korean institute of surface engineering
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    • v.41 no.5
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    • pp.205-213
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    • 2008
  • A 3D particle code is developed to analyze electron behavior in a planar magnetron sputtering cathode either in balanced or unbalanced configuration. Three types of collisions are included; electron - neutral elastic, excitation to a metastable state and ionization. Flight path is calculated by a 4-th order Runge-Kutta method with a time step of 10 ps. Effects of electron starting position, magnetic field intensity and configuration were analyzed. For a more efficient and accurate modeling, multithreading technique is considered for multicore CPU computers. Under an assumption of cold ion approach, target erosion profiles are predicted for a flat target surface.

A Study on Adolescent psychological adjustment for neglected family

  • Jang, Chun-Ok
    • International Journal of Advanced Culture Technology
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    • v.6 no.2
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    • pp.30-35
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    • 2018
  • In contemporary society, neglected families increase adolescents' maladjustment behaviors, causing academic problems, psychological and emotional problems, and showing flight behavior. By identifying the nature of the protective factor against the dangerous environment of a neglected family and increasing the protection factor for the children in a dangerous environment, it is necessary to create the environment so that the young can grow up positively rather than adversely. The purpose of this study is to identify the characteristics of adolescents who are psychologically adaptive at the level of general family children among the adolescents who are in a dangerous environment. The results showed that self - esteem, ego - resilience, ego - identity, and community variables had a significant effect on discriminating adolescents who showed high psychological adjustment from risk factors of neglect while controlling other factors. SPSS 20.0 was used to analyze the data.

A Study on Course Correction Performance Expectation & Algorithm Implementation of 1D CCM (1D CCM 탄도수정 성능예측 및 알고리즘 구현 연구)

  • Kim, Ki-Pyo
    • Journal of the Korea Institute of Military Science and Technology
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    • v.10 no.1
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    • pp.5-13
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    • 2007
  • The trajectory of an current artillery munition is subject to a variety of different error sources resulting in more or less big deviation from the nominal predicted flight path. The 1D CCM(Course Correction Munition) has appeared to solve this problem and the mechanism of 1D CCM is a simple and low cost one using the influence of drag to range behavior of an artillery munition. In the paper 1D CCM concept has been simulated using wind tunnel experiment results of the specified Korean munition with CCF(Course Correction Fuze) and calculated the performance of its rang error reduction. From the simulated results it can be numerically explained that the possibility of adaptation of 1D CCM concept to Korean artillery munitions.

Nonlinear Aeroelastic Simulation of a Full-Span Aircraft with Oscillating Control Surfaces (항공기의 조종면 진동시 비선형 공탄성 시뮬레이션)

  • Yoo, Jae-Han;Kim, Dong-Hyun;Kwon, Hyuk-Jun;Lee, In;Paek, Seung-Kil;Kim, Young-Ik
    • Journal of the Korea Institute of Military Science and Technology
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    • v.5 no.4
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    • pp.81-87
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    • 2002
  • In this paper, the transonic aeroelastic behavior of the generic fighter model is investigated in the time domain. The simulation of flutter flight test using forced harmonic motion of control surfaces including inertial coupling effects is conducted at the various conditions. The nonlinear aerodynamic effects are considered using a transonic small disturbance equation. A modal model obtained by a free vibration analysis is used for the structural model. The relations between the computed flutter boundary and the simulation results of the responses using the harmonic motions of control surfaces at various conditions are investigated.

A Seat Inventory Management Model in the Presence of Dependent Demands (종속적 수요를 반영하는 좌석재고 할당 모형)

  • Kim, Sang-Won
    • Korean Management Science Review
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    • v.27 no.2
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    • pp.67-79
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    • 2010
  • When airlines sell the same seats on an air flight at different fares, demand for a fare class depends on demand for other fare classes due to demand dependency. Demand dependencies occur when customers will buy other fare class tickets if the originally requested fare were unavailable, or when customers postpone their purchase decisions in anticipation of reopening of the lower fare in the next period. Demand dependency as a result customer buying behavior has a considerable profit implication, which was ignored in many earlier studies. We investigate the impact of demand dependency on the optimal booking limits and the expected revenues under a single-period and a two-period setting. We show how to find optimal booking limits of the problem and provide numerical examples to illustrate the impact.