• 제목/요약/키워드: Attitude performance

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손씻기 교육과 홍보 경험에 따른 대학생의 손씻기 태도와 수행도 비교연구 (Comparative Study on Handwashing Attitudes and Performances of University Students According to Handwashing Education and Promotion Experience)

  • 김영서;강예지;권예지;김채린;남하늘;곽은미
    • 문화기술의 융합
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    • 제9권3호
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    • pp.529-536
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    • 2023
  • 본 연구는 대학생의 손씻기 교육과 홍보 경험에 따른 손씻기 수행도와 태도를 비교 분석하기 위해 시도되었다. 연구대상자는 대학생 205명이며, 자가보고 형식의 구조화된 설문지를 이용하여 자료를 수집하였다. 자료분석을 위해 SPSS 22.0 program을 이용하여 기술적 통계, Independent t-test를 시행하였고, 연구의 결과는 다음과 같다. 대학생의 손씻기 교육에 따른 손씻기 수행과 태도는 모두 교육을 받은 대상자에서 통계적으로 유의하게 높았다. 대학생의 손씻기 홍보에 따른 손씻기 수행과 태도를 분석한 결과에서는 손씻기 태도에서 통계적으로 유의한 차이가 있었지만 손씻기 수행은 유의하지 않았다. 본 연구결과를 바탕으로 대학생의 손씻기 교육과 홍보를 강화할 필요가 있으며, 손씻기 수행도와 태도를 증진시키기 위한 노력이 필요할 것이다.

무인 비행체용 저가의 ADGPS/INS 통합 항법 시스템 (Design of a Low-Cost Attitude Determination GPS/INS Integrated Navigation System for a UAV (Unmanned Aerial Vehicle))

  • 오상헌;이상정;박찬식;황동환
    • 제어로봇시스템학회논문지
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    • 제11권7호
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    • pp.633-643
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    • 2005
  • An unmanned aerial vehicle (UAV) is an aircraft controlled by .emote commands from ground station and/o. pre-programmed onboard autopilot system. A navigation system in the UAV provides a navigation data for a flight control computer(FCC). The FCC requires accurate and reliable position, velocity and attitude information for guidance and control. This paper proposes an ADGPS/INS integrated navigation system for a UAV. The proposed navigation system comprises an attitude determination GPS (ADGPS) receive., a navigation computer unit, and a low-cost commercial MEMS inertial measurement unit(IMU). The navigation algorithm contains a fault detection and isolation (FDI) function fur integrity. In order to evaluate the performance of the proposed navigation system, two flight tests were preformed using a small aircraft. The first flight test was carried out to confirm fundamental operation of the proposed navigation system and to check the effectiveness of the FDI algorithm. In the second flight test, the navigation performance and the benefit of the GPS attitude information were checked in a high dynamic environment. The flight test results show that the proposed ADGPS/INS integrated navigation system gives a reliable performance even when anomalous GPS data is provided and better navigation performance than a conventional GPS/INS integration unit.

외식업체 조리사들의 테크놀로지 주방시스템이 지각된 용이성.유용성과 태도 및 직무성과에 미치는 영향연구 (Effects of Culinary Staff's Technology Kitchen System upon Perceived Ease of Use, Usefulness, Attitude, and Job Performance in the Foodservice Industry)

  • 이인숙;윤혜현
    • 한국식품조리과학회지
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    • 제27권3호
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    • pp.71-79
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    • 2011
  • The purpose of this study was to understand effects of culinary staff's technology kitchen system upon perceived ease of use, usefulness, attitude, and job performance in the foodservice industry. Based on a total of 387 samples obtained from empirical research, this study reviewed the reliability and fitness of the research model and verified a total of four hypotheses using the Amos program. The hypothesized relationships in the model were tested simultaneously using a structural equation model (SEM). The proposed model provided an adequate fit to the data, ${\chi}^2$=226.501 (df=85), p<.001, CMIN/df 2.665, RMR .066, GFI .927, NFI .926, IFI .952, TLI .941, CFI .952. The results show that culinary staff's perceived ease of use(${\beta}$=.534) had a significant positive effect on perceived usefulness. Also, perceived ease of use (${\beta}$=.350) and perceived usefulness (${\beta}$=.297) had a positive significant effect on attitude. Further, attitude (${\beta}$=1.647) had a significant positive effect on job performance. Limitations and future research directions are also discussed.

Preliminary Test of Adaptive Neuro-Fuzzy Inference System Controller for Spacecraft Attitude Control

  • Kim, Sung-Woo;Park, Sang-Young;Park, Chan-Deok
    • Journal of Astronomy and Space Sciences
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    • 제29권4호
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    • pp.389-395
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    • 2012
  • The problem of spacecraft attitude control is solved using an adaptive neuro-fuzzy inference system (ANFIS). An ANFIS produces a control signal for one of the three axes of a spacecraft's body frame, so in total three ANFISs are constructed for 3-axis attitude control. The fuzzy inference system of the ANFIS is initialized using a subtractive clustering method. The ANFIS is trained by a hybrid learning algorithm using the data obtained from attitude control simulations using state-dependent Riccati equation controller. The training data set for each axis is composed of state errors for 3 axes (roll, pitch, and yaw) and a control signal for one of the 3 axes. The stability region of the ANFIS controller is estimated numerically based on Lyapunov stability theory using a numerical method to calculate Jacobian matrix. To measure the performance of the ANFIS controller, root mean square error and correlation factor are used as performance indicators. The performance is tested on two ANFIS controllers trained in different conditions. The test results show that the performance indicators are proper in the sense that the ANFIS controller with the larger stability region provides better performance according to the performance indicators.

진료와 술기 수행의 교육전략 (Educational Strategies for Clinical and Technical Skills Performance)

  • 노혜린
    • 의학교육논단
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    • 제18권3호
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    • pp.132-144
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    • 2016
  • The aim of this study is to provide the background of developing guides to clinical performance and basic clinical skills and to introduce how to teach and learn using the guide. The students' performance problems presented in an objective clinical skills examination were disease-centered tertiary hospital clinical care, incomplete performance, doing by rote, and an exam-oriented learning attitude. The problems were caused by a tertiary hospital-based educational environment as well as schools and faculty who are unfamiliar with the concept of patient-centered care. The purpose of the guide to clinical performance and basic clinical skills is to overcome these problems and address the causes. The guides show a clinical presentation approach to primary care; clinical care integrated with knowledge, skills, and attitude; a schematic approach; and a patient-centered attitude. To achieve these goals, a strategy to change the educational culture is important. Curricular reform, faculty development, and improving educational facilities and environments are suggested.

팬데믹 상황에서 간호대학생의 윤리인식, 윤리적 의사결정 및 감염관리지침 수행태도가 감염관리지침 수행의도에 미치는 영향 (The Influence of Nursing Students' Ethical Awareness, Ethical Decision-making and Attitude toward Performance on Intention about Performance of Infection Control Guidelines in Pandemic Infectious Diseases)

  • 최동원
    • 한국보건간호학회지
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    • 제35권3호
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    • pp.343-355
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    • 2021
  • Purpose: This study aimed to identify the effects of nursing students' ethical awareness, ethical decision-making and attitude toward performance on intention about performance of infection control guidelines in pandemic infectious diseases. Methods: The survey was performed on 163 nursing students in three universities. Data were collected using a structured questionnaires and analyzed with t-test, analysis of variance (ANOVA), Pearson's correlation and multiple regression analysis. Results: Perceived health status, ethical awareness and attitude toward performance of infection control guidelines about major commitment were significant predictive variables. These variables accounted for 48.1% of the variance in major commitment. Conclusion: The findings indicate the necessity of developing educational programs to enhance nursing students's ethical awareness, and increase performance of control guidelines to prepare for the pandemic infectious diseases.

시스템 개발시 사용자 참여와 태도가 시스템의 실행 성과에 미치는 영향 (The Effect of Participation and Attitude in the Process of System Development on the Implementation of Information System)

  • 김준석;이해승
    • Asia pacific journal of information systems
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    • 제4권2호
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    • pp.247-263
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    • 1994
  • This paper reports the results of a field study investigating the effect of user participation and attitude on the success of information system implementation during the system development process. The theoretical framework for this research is based on the organizational change theory, in which the attitude affects the effects of user's participation. User participation and attitude were defined as independent variables and the performance of system implementation as dependent variable. User participation was defined as a direct participation by end users in the process of the new information system development. This was measured by user's participation/non-participation. User attitude refers to user's opinions or feelings before a new system is developed. This was measured by user's favor toward a system. The performance of system implementation was measured by the surrogate variable, the degree of individual satisfaction on developed system. To achieve the objective of this research, a field research method utilizing questionnaires were employed. They were distributed to 221 users present during and/or after system development. Among 185 questionnaires returned, 175 questionnaires were used for analysis. The major findings can be summarized as follows: First, there was no significant effect of user participation on user satisfaction. Second, there was a significant effect of user attitude on user satisfaction. Third, there was no significant interaction effect of user participation and attitude on user satisfaction. It is worth to note that the user's participation did not have any significant effect on the user's satisfaction. It seems the reason for the above result is due to user's involuntary participation. In fact, the user does not have much leverage in the process of system development, which may result in poor performance of user participation. Since user attitude is an important factor in the success of system implementation, however, a method to overcome unfavorable attitude of user should proceed all others.

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휠-트랙 하이브리드 모바일 플랫폼을 위한 지형 적응성 장애물 극복 자세 제어기 개발 (Development of Terrain-Adaptive Attitude Controller for Hybrid Mobile Platform with Wheel & Track)

  • 곽정환;김윤구;홍대한;안진웅
    • 대한임베디드공학회논문지
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    • 제7권2호
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    • pp.61-70
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    • 2012
  • This paper describes terrain-adaptive attitude controller for a hybrid mobile platform which operates in wheel & track mode. The wheel mode of the hybrid mobile platform allows quick driving performance in the flatland, while the track mode provides adaptive movement in the rough ground or stairway. The switching of the platform between two modes is automatically controlled by attitude controller algorithm. In addition, in the track mode, the platform automatically adjusts its attitude angle to overcome the obstacles in front. This paper demonstrates the attitude controller for the aforementioned wheel-track hybrid mobile platform in order to overcome terrain obstacles by using an adaptive method. The driving performance of the hybrid mobile platform has been tested and verified in various surrounding environments in both wheel and track mode. Further, this paper presents the experiments by using the track structure of mobile platform on forming adaptive attitude under various types of obstacles. The practicability and effectiveness of the proposed attitude controller of the platform has been demonstrated in urban building and a test-bed.

Performance Improvement of an INS by using a Magnetometer with Pedestrian Dynamic Constraints

  • Woyano, Feyissa;Park, Aangjoon;Lee, Soyeon
    • IEIE Transactions on Smart Processing and Computing
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    • 제6권1호
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    • pp.1-9
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    • 2017
  • This paper proposes to improve the performance of a strap down inertial navigation system using a foot-mounted low-cost inertial measurement unit/magnetometer by configuring an attitude and heading reference system. To track position accurately and for attitude estimations, considering different dynamic constraints, magnetic measurement and a zero velocity update technique is used. A conventional strap down method based on integrating angular rate to determine attitude will inevitably induce long-term drift, while magnetometers are subject to short-term orientation errors. To eliminate this accumulative error, and thus, use the navigation system for a long-duration mission, a hybrid configuration by integrating a miniature micro electromechanical system (MEMS)-based attitude and heading detector with the conventional navigation system is proposed in this paper. The attitude and heading detector is composed of three-axis MEMS accelerometers and three-axis MEMS magnetometers. With an absolute algorithm based on gravity and Earth's magnetic field, rather than an integral algorithm, the attitude detector can obtain an absolute attitude and heading estimation without drift errors, so it can be used to adjust the attitude and orientation of the strap down system. Finally, we verify (by both formula analysis and from test results) that the accumulative errors are effectively eliminated via this hybrid scheme.

Development of 3-Dimensional Position/Attitude Determination Radio-navigation System with FLAOA and TOA Measurements

  • Jeon, Jong-Hwa;Lim, Jeong-Min;Yoo, Sang-Hoon;Sung, Tae-Kyung
    • Journal of Positioning, Navigation, and Timing
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    • 제7권2호
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    • pp.61-71
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    • 2018
  • Existing radio positioning systems have a drawback that the attitude of user's tag is difficult to be determined. Although forward link angle of arrival (FLAOA) technology that uses measurements of array antenna arranged in a tag among the angle of arrival (AOA) technologies can estimate attitude and positioning of tags, it cannot extend the estimated results into three-dimensional (3D) results due to complex non-linear model displayed because of the effects of 3D positioning and attitude in tags. This paper proposed a radio navigation technique that determines 3D attitude and positioning via FLAOA / time of arrival (TOA) integration. According to the order of determining attitude and positioning, two integration techniques were proposed. To analyze the performance of the proposed technique, MATLAB-based simulations were used to verify the performance. The simulation results showed that the first proposed method, TOA-FLAOA integrated technique, showed about 0.15 m of positioning error, and $2-3^{\circ}$ of attitude error performances regardless of the positioning space size whereas the second method, differenced FLAOA-TOA integrated technique, revealed a problem that a positioning error became larger as the size of the positioning space became larger.