• 한국도서관정보학회지
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• 제47권2호
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• pp.329-358
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• 2016

이 연구는 아동의 독서태도를 다양한 측면에서 측정할 수 있는 검사도구를 개발하는 데에 목적이 있다. 이에 따라 선행 독서태도 검사 도구, 독서태도 모델과 독서태도에 관한 암묵적 지식 연구를 토대로 구성요인을 설정하고 문항을 작성하였다. 검사도구의 타당도와 신뢰도 검증을 위해 초등학교 4-6학년 학생을 대상으로 1차와 2차 검사를 실시하였다. 독서태도 검사도구에 대한 탐색적 요인분석을 통해 3개의 구성요인에서 8개의 하위요인을 추출하였고, 추출된 8개의 요인은 전체변량의 66.29%를 설명하였다. 문항내적 상관계수 r값은 모든 문항에서 0.4이상으로 나타났고, 독서태도 검사도구의 Cronbach ${\alpha}$값이 0.950으로 나타나 개발된 독서태도 검사도구의 신뢰도와 타당도가 양호함을 확인하였다. 따라서 인지, 정서, 행동의지를 독서태도 구성요인으로 하고 독서효용성과 독서효능감, 여가, 자극, 몰입, 표현, 학습, 적극성을 하위요인으로 하는 독서태도 검사도구는 아동의 독서태도에 관한 다양한 측면을 검사하기에 유용한 도구로 기능할 수 있다는 점을 제시하고 있다.

• 융합경영연구
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• 제6권4호
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• pp.1-16
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• 2018

Purpose - This study will investigate and identify the relationship between brand image, brand attitude and intent to purchase based on subjects that have remembered or watched more than one storytelling marketing ad related to airlines. The purpose of the project is to secure market competitiveness by presenting the basis for and use of the marketing strategy using storytelling, which can capture the goodwill of the aerospace competition market in the future. Research, design, data, and methodology - Prior to the research model and hypothesis testing phase, a verification factor analysis was conducted to assess internal consistency among each measurement item and to ensure reliability and validity of the measurement tool. Further, the organization was assessed for validity by calculating the mean variance estimation (AVE) and the construction concept reliability (CCR) through a positive factor analysis. Hypothesis verification was analyzed through a structural equation model, and each concept set in the hypothesis was entered as a potential variable, and each measurement item was entered as an observation variable. Results - Airline's storytelling marketing has a significant impact on the brand image and two emotional and cognitive responses have been shown to influence the brand image. In addition, airline storytelling marketing has a significant impact on brand attitudes and airline storytelling marketing derived from factor analysis has shown two emotional and cognitive responses to brand attitudes. Conclusions - The parts derived based on the research results show that storytelling marketing has a strong influence on the airline's brand image and attitude, and that it is necessary for airlines to have a brand image and attitude. Also, forming a favorable brand image has a significant impact on brand attitudes. We believe that by presenting basic data to the aviation industry in future research on airline storytelling, we will be able to increase understanding and contribution to development of storytelling marketing in aviation.

• 한국노년학
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• 제38권3호
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• pp.409-433
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• 2018

본 연구는 어린이가 일상에서 노인과의 접촉을 통해 노인에 대한 차별적 태도(Ageist attitude)를 완화할 수 있는지, 해당 태도의 개선방안을 탐색하였다. 명시적 태도(Explicit attitude)의 측정에 사용되는 자기보고식(Self-reported) 척도가 의식에서 여과된 수준의 편견만 반영하는 한계를 고려해, 내면의 차별적 인식을 나타내는 '암묵적 태도(Implicit attitude)'를 측정하였다. 명시적 태도 측정에는 웃는 얼굴 5점 척도를, 암묵적 태도 측정에는 어린이용 암묵적 연령 연합검사(Children Implicit Age-association Test)를 사용하였다. 서울 및 수도권 초등학교 4~6학년 초등학생 503명의 자료를 수집했으며 기술통계, 다항 및 서열 로지스틱 회귀분석 방법으로 분석하였다. 분석결과는 크게 세 가지로 요약된다. 첫째, 노인에 대한 어린이의 명시적 태도와 암묵적 태도의 예측요인이 달랐다. 이는 편견의 '표출'을 완화하는 요소를 이용해 '내적 편견'을 예측하고 개선하는 데는 한계가 있으며 따라서 암묵적 편견에 대한 별도의 접근이 필요함을 보여준다. 둘째, 어린이의 연령차별적 태도와 노인 접촉경험의 관계는 어린이와 노인의 관계특성, 그리고 접촉의 양적 측면과 질적 측면에 따라 다소 복잡한 관계를 보였다. 종합적으로 요약하면 노인을 많이 그리고 긴밀하게 만나는 아이들이 표면적으로 또는 내면적으로 연령차별적일 가능성이 낮았다. 마지막으로, 접촉질이 중요한 명시적 태도와 달리 암묵적 태도는 접촉량과 약한 관련을 보였으며, 접촉질과는 관계가 없었다. 이는 편견 완화에 접촉량보다는 질의 효과를 강조해온 집단 간 접촉이론(Intergroup contact theory)으로 설명되지 않는 결과로, 접촉의 암묵적 태도에 대한 영향을 전반적으로 검토하고 이론을 보완할 필요가 있다.

• 제어로봇시스템학회논문지
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• 제5권1호
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• pp.62-68
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• 1999

The attitude of a vehicle can be precisely determined using GPS carrier phase measurements from more than two antennas attached to a vehicle and an efficient integer ambiguity resolution technique. Many methods utilizing the known baseline length as a constraint of independent elements of integer ambiguities are proposed to resolve integer ambiguity at real time. Three-dimensional search space is reduced to two-dimensional search space with this constraint. Thus the true integer ambiguity can be easily determined with less computational burden and fewer number of measurements. But there are still strong requirements for the real time integer ambiguity resolution, which uses single epoch measurement of long baseline. In this paper, a new constraint from the geometry of multiple baselines is derived. With this new constraint, two-dimensional search space is further reduced to one-dimensional search space. It makes possible to determine integer ambiguity with single epoch measurement. The proposed method is applied to real data to show its effectiveness.

• International Journal of Aeronautical and Space Sciences
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• 제3권2호
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• pp.88-94
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• 2002

This paper describes attitude determination algorithm for the low earth orbit(LEO) spacecraft using stellar inertial sensors. The cascaded gyro/star tracker extended Kalman filter is constructed to fuse two sensor data. And then the smoothing of the measurement are proposed for an unreasonable jump of star tracker. The smoothing algorithm for the rejection of star tracker error jumps is designed by scalar adaptive filter. The proposed algorithms operate to process the measurement of gyro/star tracker Kalman filter, therefore, it is comparatively simple to apply these methods to other integration systems. Simulations to gyro/star tracker integrated system show that the proposed method is effective.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1995년도 Proceedings of the Korea Automation Control Conference, 10th (KACC); Seoul, Korea; 23-25 Oct. 1995
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• pp.162-165
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• 1995

For an accurate on-line measurement of the ship's attitude the paper develops an intelligent sensing system which uses one servo-type accelerometer and two servo-type inclinometers appropriately located on the ship. By considering the dynamics of the servo-controlled rigid pendulums of the inclinometers, linear equations for the rolling and pitching of the ship are derived separately from each other. Moreover, one accelerometer is used for extracting the heaving signal. Through the introduction of linear dynamic models and the linear observation equations for the heaving, rolling and pitching, the on-line measurement of the three signals can be reduced to the state estimation of the linear dynamic systems. A bank of Kalman filters is adaptively used to achieve the on-line accurate state estimation and to overcome changes in parameters in the linear dynamic models.

• International Journal of Aeronautical and Space Sciences
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• 제17권2호
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• pp.214-221
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• 2016

An attitude estimation algorithm which integrates gyroscope and vision measurements using an adaptive complementary filter is proposed in this paper. In order to make the filter more tolerant to vision measurement fault and more robust to system dynamics, fuzzy interpolator is applied. For recognizing the dynamic condition of the system and vision measurement fault, the cut-off frequency of the complementary filter is determined adaptively by using the fuzzy logic with designed membership functions. The performance of the proposed algorithm is evaluated by experiments and it is confirmed that proposed algorithm works well in the static or dynamic condition.

• 가정과삶의질연구
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• 제5권2호
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• pp.145-162
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• 1987

The purpose of this study is to investigate the relations between Wives' marital satisfaction and Divorce attitude as a basis building in marital stability . A measurement tools used for this study are marital satisfaction scale, which was adapted and reproducted from Dyadic Adjustment Scale(DAS) developed by Spanier and Divorce attitude Scale, which was developed by researcher refer to preceding study connected with a cause of divorce. The subjects were 354 married women dwelling in Seoul. Statistical methods such as frequency, percentile. mean , standard deviation, one way ANOVA, and Pearson Correlation were used for data analysis. The results of this study are as follows; 1) there is the tendency to high marital satisfaction group rather more than low marital satisfaction group and to permissional attitude group rather more than negative attitude group about divorce attitude. 2) There was difference in marital satisfaction by number of children, wives's educational level, parents marriage happiness. While, there was no difference in marital satisfaction by length of marriage, family income, wives employments status, marriage pattern. 3) There was partially difference in wives' attitude toward divorce by wives educational level, family income. Both there was no difference in wives attitude toward divorce by the other factors. 4) wives' attitude toward divorce correlates with marital satisfaction. The correlation coefficients is 283 significantly of .001 level. The more satisfaction wife feels about her own matrimony. the more negative a attitude she has toward divorce. This menas that attitude toward divorce depends upon their matrimony. 5) The four type of marital stability are as follows; high marital stability type, high subjective unstability type, high objective unstability type, high marital unstability type.

• 동력기계공학회지
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• 제17권5호
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• pp.121-127
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• 2013

In this paper, we propose a distance measurement system for automatic berthing control using a stereo camera mounted on a rotation control device, and a radial pattern target. Automatically controlling the position and attitude of a ship aims to prevent maritime accidents due to human error. Our goal is to measure the relative distance between a ship and an onshore or offshore target for berthing. Therefore, the distance should be continuously measured while tracking a fixed point on a target. To this end, we developed a stereo camerabased distance measurement system that satisfied these requirements. This paper describes the structure and principle of the measurement system. We validate the distance error for target incline due to the relative position and attitude between a camera and a target in miniature scale. In addition, the findings of an experiment in an outdoor environment demonstrate that the proposed measurement system has accuracy within 1 m at a range of 20-100 m which is the acceptable accuracy for automatic berthing.

• Journal of Biosystems Engineering
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• 제37권6호
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• pp.342-351
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• 2012

Purpose: Aerial spraying with an agricultural unmanned helicopter became a new paradigm in the agricultural practice. Laterally tilting behavior of a conventional agricultural helicopter, resulting in the biased down-wash and uneven spray deposit is a physically intrinsic phenomenon while hovering and cruise flights. Authors studied and developed a roll-balanced agricultural helicopter with a raised pylon tail rotor system. In this study, the attitude of the roll-balanced helicopter was determined using the Kalman filter algorithm, and the quality of roll balancing of a bare-airframe helicopter was evaluated. Methods: Instantaneous attitudes were estimated using the advantage of gyroscope, followed by the long term correction and prediction using accelerometer data for the advantage of convergence. The attitudes of the fuselage were calculated by applying the Kalman filter algorithm. The spraying maneuver of the helicopter was performed at a field of 50 m long, and the attitude data were acquired and evaluated. Results: The determination of attitude using the inertial measurement unit(IMU) and Kalman filter was reliable and practical. The intrinsic attitude of the developed helicopter was stable and roll-balanced. The deviation of roll angle was ${\pm}6.3^{\circ}$ with an average of $0^{\circ}$, referring to roll-balanced. Conclusions: Handling quality of the roll attitude determined to be steadily balanced. The balancing behavior of the developed helicopter would result in an even spray pattern during aerial application.