• Title/Summary/Keyword: a guidance

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The Effect of a Hospital Life Guidance Movie for Elderly In-patients (노인을 대상으로 한 입원생활 안내 동영상의 효과)

  • Jeong, Hyeon-Cheol;Seong, Kea-Mi;Jeong, Mi-Yang
    • Journal of Korean Academy of Fundamentals of Nursing
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    • v.17 no.2
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    • pp.142-148
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    • 2010
  • Purpose: This study was done to determine how a hospital life guidance movie enhanced the understanding of hospital life by elderly in-patients. Method: A non-equivalent control group post-test design was used for the study. The experimental group watched a movie on guidance for hospital life while an in-patient control group read corresponding guidance booklets. The understanding and satisfaction from the respective programs for the two groups were surveyed with a questionnaire. The data were analyzed using SPSS. Results: The group which watched the movie had a better understanding of hospital life than the group which read the booklets. The patients who watched the movie also expressed more satisfaction with their guide program than the patients who only read the booklets. Understanding of hospital life had relevance to satisfaction with the given program. Conclusion: The results of this study suggests that a movie on hospital life provides better guidance which helps the prospective patients understand and adapt better to their hospital life. Therefore, this type of movie is considered to be an effective medium to provide guidance to elderly in-patients.

Design and Implementation of a Career Guidance Program at Gachon University College of Medicine (가천대학교 의과대학 졸업 후 진로지도 프로그램 설계와 운영)

  • Kwi Hwa Park
    • Korean Medical Education Review
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    • v.26 no.1
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    • pp.41-47
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    • 2024
  • The ultimate goal of career guidance is to help medical students develop a career plan that matches their personal characteristics, allows them to train in their desired subspecialty, and helps them to adapt well to medical practice after graduation. Gachon Medical School has designed a longitudinal career guidance program called GLORI (Gachon Longitudinal Orientation and Career Development), which is based on the outcome of each phase. The program consists of regular courses and portfolio-based career guidance from a mentor professor. In phase 2 (basic medical science), the "Career Seminar" course was developed. This course focuses on self-understanding through a psychological inventory, exploration of postgraduate career paths, and interviews with professors in specialties of interest. In phase 3 (the integration of basic and clinical science), the "Exploring Nonclinical Career Options" course was introduced. This course presents perspectives from doctors who have followed various pioneering career trajectories, including biomedical engineering, medical journalism, writing, public health, health care administration, the pharmaceutical and medical device industries, and other areas. All teaching methods were designed to encourage student participation. The assessment methods are assignment-based, including self-reflective reports and presentations. In addition, a portfolio-based career guidance program is implemented in phases 3 and 4 (clinical clerkship). It is expected that this case study will serve as a practical example for developing comprehensive career guidance programs for medical schools.

Guidance Laws for Aircraft Automatic Landing (항공기 자동착륙 유도 법칙에 관한 연구)

  • Min, Byoung-Mun;No, Tae-Soo;Song, Ki-Jung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.5
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    • pp.41-47
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    • 2002
  • In this paper, a guidance law applicable to aircraft automatic landing is proposed and its performance is compared with the conventional ILS-type landing approach. The concept of miss distance, which is commonly used in the missile guidance laws, and Lyapunov stability are effectively combined to obtain the landing guidance law. The new landing guidance law is integrated into the existing controller and is applied to the landing approach and flare phases of landing procedure. Numerical simulation results show that the new landing guidance law is a viable alternative to the conventional strategies that directly control the longitudinal deviation or altitude.

The Study of Characteristics of Korea Fog and Forecast Guidance (한반도 안개 특성 분석 및 예보 기법 연구)

  • Kim, Jun-Sik;Kim, Jae-Hwan;Park, Sang-Hwan;Kim, Young-Chul
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.21 no.1
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    • pp.68-73
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    • 2013
  • This study is to make a protype of forecast guidance for forecasters from analyzing the characteristics of Korea Fog. The trend of Korea fog showed the decline in the number of foggy days and the duration time, the gradient is -1.24days/year under 3 miles and -0.98days/year under 1 mile and -1.64hours/year under 3 miles and -3.18hours/year under 1 mile in duration time in 27 ROKAF base. To find the protype of inland and coastal forecast guidance, Daegu base as a representation of the inland base and Gangneung base as the representation of the coastal base were chosen. For Daegu base, the mixture of relative humidity, sky condition, and the position of high pressure were selected for the forecast guidance. For Gangneung base, pressure pattern, sea surface temperature, sea currents, and 850hPa temperature patterns were selected for the forecast guidance.

Captive Flight Test System Configuration and Verification for Multi-mode Guidance Missile System (복합유도방식이 적용된 유도탄의 탑재비행시험(CFT) 시스템 구성 및 검증)

  • Park, Inchul;Heo, Wonyoung;Lee, Yongho;Jeong, Seyoung
    • Journal of the Korea Institute of Military Science and Technology
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    • v.19 no.5
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    • pp.606-612
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    • 2016
  • A Captive Flight Test(CFT) is used to verify the performance of missile component such as seeker and guiding algorithm of missile. Recently most of surface to air missile adapts multi-mode guidance method which include command guidance and active/passive guidance. A CFT system for missile system adapting multi-mode guidance method consists of pod equipment, command transmitting system and measuring system. In this paper, we proposed CFT system and testing method for missile which adapt multi-mode guidance, and system integration procedure by using distributed missile system integration method and procedure. The proposed CFT system and system integration method was applied to CFT of surface to air missile, and brought successful result.

Positioning and Driving Control of Fork-type Automatic Guided Vehicle With Laser Navigation

  • Kim, Jaeyong;Cho, Hyunhak;Kim, Sungshin
    • International Journal of Fuzzy Logic and Intelligent Systems
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    • v.13 no.4
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    • pp.307-314
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    • 2013
  • We designed and implemented a fork-type automatic guided vehicle (AGV) with a laser guidance system. Most previous AGVs have used two types of guidance systems: magnetgyro and wire guidance. However, these guidance systems have high costs, are difficult to maintain with changes in the operating environment, and can drive only a pre-determined path with installed sensors. A laser guidance system was developed for addressing these issues, but limitations including slow response time and low accuracy remain. We present a laser guidance system and control system for AGVs with laser navigation. For analyzing the performance of the proposed system, we designed and built a fork-type AGV, and performed repetitions of our experiments under the same working conditions. The results show an average positioning error of 51.76 mm between the simulated driving path and the driving path of the actual fork-type AGV. Consequently, we verified that the proposed method is effective and suitable for use in actual AGVs.

Absolutely Stable Region for Missile Guidance Loop (유도탄 유도루프의 절대안정한 시간영역)

  • Kim, Jong-Ju;Lyou, Joon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.3
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    • pp.244-249
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    • 2008
  • In this paper, the stable region for missile guidance loop employing an integrated proportional navigation guidance law is derived. The missile guidance loop is formulated as a closed-loop control system consisting of a linear time-invariant feed-forward block and a time-varying feedback gain. By applying the circle criterion to the system, a bound for the time of flight up to which stability can be assured is established as functions of flight time. Less conservative results, as compared to the result by Popov criterion, are obtained.

Target Pointing Guidance Design Using Time-to-Go Estimator (Time-to-Go 추정기를 이용한 목표점 지향 유도 법칙 설계)

  • Whang, lck-Ho
    • Journal of Institute of Control, Robotics and Systems
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    • v.8 no.1
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    • pp.60-66
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    • 2002
  • In this paper, a new target pointing guidance algorithm is proposed by combining the optimal target pointing solution and a simple time-to-Go estimator. Also investigated are some properties of the guidance algorithm which include a relation to conventional PNG, convergence region and convergence trajectories of error states according to the time-to-go estimator gain. Some guidelines for designing the pointing guidance law are commented based on the convergence properties. A design example in the case of large initial heading errors is presented and its performance is investigated by simulation.

REPRESENTATION OF NAVIGATION INFORMATION FOR VISUAL CAR NAVIGATION SYSTEM

  • Joo, In-Hak;Lee, Seung-Yong;Cho, Seong-Ik
    • Proceedings of the KSRS Conference
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    • 2007.10a
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    • pp.508-511
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    • 2007
  • Car navigation system is one of the most important applications in telematics. A newest trend of car navigation system is using real video captured by camera equipped on the vehicle, because video can overcome the semantic gap between map and real world. In this paper, we suggest a visual car navigation system that visually represents navigation information or route guidance. It can improve drivers' understanding about real world by capturing real-time video and displaying navigation information overlaid on it. Main services of the visual car navigation system are graphical turn guidance and lane change guidance. We suggest the system architecture that implements the services by integrating conventional route finding and guidance, computer vision functions, and augmented reality display functions. What we designed as a core part of the system is visual navigation controller, which controls other modules and dynamically determines visual representation methods of navigation information according to a determination rule based on current location and driving circumstances. We briefly show the implementation of system.

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A Study on Efficient Activities in Railway Safety Guidance (효율적인 철도안전지도 활동에 관한 연구 한국철도공사 중심으로 -)

  • Kim, Tae-gil;Kim, Ki-Young;Kang, Kyung-sik
    • Journal of the Korea Safety Management & Science
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    • v.17 no.3
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    • pp.81-88
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    • 2015
  • Infrastructure such as tracks, catenary, rolling stock and signaling systems, and close interface with the human factors of train drivers, shunting staff and maintenance staff are required for train operations. Safety management is the most essential part for the functioning of a train. In line with the safety management, each rail operator has a safety guidance system and the Ministry of Land, Infrastructure and Transport operates Railway Safety Inspector system. Safety Inspector System is to train employees working in the field to be aware of rules and regulations, and to improve identified risk factors. Hence, it is necessary to establish systematic training and inspection methods for safety guidance staff and make clear the roles and responsibilities of safety inspectors according to the Occupational Safety and Health Act, and safety instructors for several inspections according to the Railroad Safety Act.