• 제목/요약/키워드: Software attitude

검색결과 224건 처리시간 0.03초

자세 측정용 GPS/INS통합 시스템 개발 (A Development of Attitude GPS/INS Integration System)

  • 오천균;이재호;서흥석;성태경
    • 대한전기학회:학술대회논문집
    • /
    • 대한전기학회 2001년도 하계학술대회 논문집 D
    • /
    • pp.1984-1986
    • /
    • 2001
  • In order to provided continuous solutions, latest developing navigation systems tend to integrate GPS receiver with INS or DR. Using the GPS carrier-phase measurements, an attitude GPS receiver with three antennas obtain the 3-dimensional attitude such as roll, pitch, and heading as well as position and velocity. With these angle measurements, in the attitude GPS/INS integrated system, attitude or gyro errors can be directly compensated. In this paper, we develop an integrated navigation system that combines attitude GPS receiver with INS. The performance of real-time integrated navigation system is determined by not only the implements of integration filter but also the synchronization of measurements. To meet these real-time requirements, the navigation software is implemented in multi-tasking structure in this paper. We also employ time-synchronization technique in the multi-sensor fusion. Experimental results show that the performance of the attitude GPS/INS integrated system is consistent even when cycle-slip occurs in carrier-phase measurements.

  • PDF

Implementation and Validation of Earth Acquisition Algorithm for Communication, Ocean and Meteorological Satellite

  • Park, Sang-Wook;Lee, Young-Ran;Lee, Byoung-Sun;Hwang, Yoo-La;Lee, Un-Seob
    • Journal of Astronomy and Space Sciences
    • /
    • 제28권4호
    • /
    • pp.345-354
    • /
    • 2011
  • Earth acquisition is to solve when earth can be visible from satellite after Sun acquisition during launch and early operation period or on-station satellite anomaly. In this paper, the algorithm and test result of the Communication, Ocean and Meteorological Satellite (COMS) Earth acquisition are presented in case of on-station satellite anomaly status. The algorithms for the calculation of Earth-pointing attitude control parameters including those attitude direction vector, rotation matrix, and maneuver time and duration are based on COMS configuration (Eurostar 3000 bus). The coordinate system uses the reference initial frame. The constraint calculating available time-slot to perform the earth acquisition considers eclipse, angular separation, solar local time, and infra-red earth sensor blinding conditions. The results of Electronics and Telecommunications Research Institute (ETRI) are compared with that of the Astrium software to validate the implemented ETRI software.

Development of KOMPSAT-2 Vehicle Dynamic Simulator for Attitude Control Subsystem Functional Verification

  • Suk, Byong-Suk;Lyou, Joon
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 제어로봇시스템학회 2003년도 ICCAS
    • /
    • pp.1465-1469
    • /
    • 2003
  • In general satellite verification process, the AOCS (Attitude & Orbit Control Subsystem) should be verified through several kinds of verification test which can be divided into two major category like FBT (Fixed Bed Test) and polarity test. And each test performed in different levels such as ETB (Electrical Test Bed) and satellite level. The test method of FBT is to simulate satellite dynamics with sensors and actuators supported by necessary environmental models in ETB level. The VDS (Vehicle Dynamic Simulator) try to make the real situation as possible as the on-board processor will undergo after launch. The purpose of FBT test is to verify that attitude control logic function and hardware interface is designed as expected with closed loop simulation. The VDS is one of major equipments for performing FBT and consists of software and hardware parts. The VDS operates in VME environments with target board, several commercial boards and custom boards based on the VxWorks real time operating system. In order to make time synchronization between VDS and satellite on-board processor, high reliable semaphore was implemented to make synchronization with the interrupt signal from on-board processor. In this paper, the real-time operating environment used on VDS equipment is introduced, and the hardware and software configurations of VDS summarized in the systematic point of view. Also, we try to figure out the operational concept of VDS and AOCS verification test method with close-loop simulation.

  • PDF

E-서비스품질과 소비자 태도 및 만족도 간의 관계: 중국 음식배달 애플리케이션 중심으로 (Influences of the E-service Quality of Food Delivery Application in China on Customer Attitude, and Satisfaction)

  • 강상;유지건;김영국
    • 아태비즈니스연구
    • /
    • 제13권3호
    • /
    • pp.375-387
    • /
    • 2022
  • Purpose - The food delivery mobile application market is growing rapidly in the catering service industry. The purpose of this study was to investigate the effects of E-service quality on consumer attitudes and satisfaction in the food delivery service field in China. Design/methodology/approach - A total of 390 copies of this questionnaire were distributed between February 17 and March 25, 2021 on the Chinese survey site (https://www.wjx.cn). Three hundred forty-nine parts were used for the final analysis. Validity and reliability were analyzed using SPSS 25.0 statistical program, and correlation and regression analysis were performed. Findings - The study results showed among the e-service quality components of food delivery application software, trust, convenience, proximity and reactivity have an impact on consumer attitudes. Research implications or Originality - The service quality of food application software is an important factor determining consumer attitude. The limitations of this study and suggestions for future research were discussed.

Study on the Influence of Stakeholders in Construction Projects

  • Rajeev, S.;Kothai, P.S.
    • Journal of Construction Engineering and Project Management
    • /
    • 제4권2호
    • /
    • pp.8-11
    • /
    • 2014
  • The interactions and interrelationships between stakeholders largely determine the overall performance of a construction project, and have the crucial responsibility for delivering a project to successful completion. An important component of stakeholder management is stakeholder analysis. Two case studies are conducted within Kerala (India). The main objective was to carry out stakeholder analysis using stakeholder organiser deluxe software, considering the data's collected from the project execution team using questionnaire. During data collection the key stakeholders were identified, to know how to manage them, their interest, power, attitude level etc, for quality improvement. Analyze the results using the software Stakeholder organizer deluxe and modeling of stakeholders is to be done. Finally validate the models of the projects. These findings may mainly reflect the stakeholder management environment in the respective regions of project implementation.

지역아동센터를 위한 소프트웨어 교육 프로그램 운영 및 효과 (Operation and effect of software education program for Community Child Center)

  • 마대성
    • 정보교육학회논문지
    • /
    • 제22권1호
    • /
    • pp.123-130
    • /
    • 2018
  • 본 연구의 목적은 G지역 지역아동센터를 대상으로 찾아가는 SW 놀이터 프로그램을 운영하면서 아동센터 학생들이 SW 교육에 대한 인식의 변화를 통해 SW 교육에 대해 흥미를 붙이고 학습해 나가는 과정을 살펴보고자 하였다. 지역아동센터내의 학생들은 학년과 나이가 다양하므로 수준별 교육과정과 교수학습 과정안을 제시하였다. 그 결과 SW 교육에 대한 학생들의 태도와 만족도가 높아졌고, 소외계층을 위한 교육 프로그램이 절실히 필요함을 알 수 있었다.

Creation of High-Quality Abstractions in Software Engineering

  • Alexey Razumowsky
    • International Journal of Computer Science & Network Security
    • /
    • 제23권7호
    • /
    • pp.193-201
    • /
    • 2023
  • Abstraction is the cornerstone of ideal software engineering (SWE). This paper discusses a problem of forming reasonable generalizations, representations and descriptions in various software development processes through the prism of poor-quality (rash, unconsidered, uncertain and harmful) abstractions. To do this, emphasis is made on an induced strategic connection between the required abstraction and its compact specific formulation based on existing research and the author's introspective experience. A software aim point and characteristic preservation of the solution integrity is the subject of the best formulation and a program module or code associated with it. Moreover, a personal attitude expressed by personal interest, motivation and creativity, is proclaimed to be a fundamental factor in successful software development.

헤어 태도.헤어 관여의 중요도와 연령에 따른 차이 (Hairdo Attitude.Hairdo Involvement Importances and Differences Depending on Age)

  • 이혜원;김미영
    • 복식문화연구
    • /
    • 제15권6호
    • /
    • pp.917-928
    • /
    • 2007
  • The purposes of this study were to investigate the hairdo attitude and hairdo involvement importances and differences depending on age. For the experimental work, questionnaires for research are prepared and asked to people who are women living in Seoul and Kyoung-Ki Do. They are collected from September to October 2006. 406 questionnaires are used in the analysis. The collected data were 'analyzed by using SPSS 12.0 software with factor analysis, Cronbach's alpha, paired T-test, and T-test. The results of this study were as follows; To analyze differences in the hairdo attitude and the hair involvement depending on different age groups, two groups were identified: one group of women aged $20{\sim}35$, and the other group of those aged $45{\sim}60$. 1. When the hairdo attitude factors were prioritized, orientations toward 'constancy' and 'consciousness of others' were found to be most critical, followed by those toward 'leader's fashion conformity' and 'distinct individuality'. When the hairdo involvement factors were prioritized, 'interests and pleasure in hairdo' were found to be most important, followed by 'symbolic representation', 'risk awareness', 'coordination of hairdo', and 'fashionableness'. 2. When difference in the hairdo attitude was analyzed, a significant difference was shown in orientations toward 'leader's fashion conformity' and 'consciousness of others'. 3. As for the hairdo involvement of the groups, a significant difference was found only in 'coordination of hairdo', signalling that the younger women put more focus on the coordination.

  • PDF

공중물체의 자세제어 및 안정화를 위한 밸런스 빔 제어기(신건설장비) 구현 (An Implementation of Balance Beam Controller(New Construction Machinery) for an Attitude Control and Stabilization of an Unstructured Object)

  • 이건영;김진오
    • 대한전기학회논문지:시스템및제어부문D
    • /
    • 제52권1호
    • /
    • pp.38-44
    • /
    • 2003
  • In this study, the balance beam control subsystem, new type of construction machinery using the mechanism of CMG (control moment gyro), for the attitude control of an unstructured object such as a beam carried by a tower crane, is designed and implemented. The balance beam controller consists of a wheel spinning at high speed and an outer gimbal for controlling the attitude of the wheel. Two motors, one for the wheel and the other for the gimbal, are used. Applying force to the spin axis of the wheel, as an input of the system, leads the torque about the axis because of the gyro effects. This torque is used to control the attitude of the unstructured object in this study. For the stabilizer function, in addition, holding the load at the current position, the attitude of the wheel is freed by cutting the power applied to the gimbal motor of the balance beam controller, which result in the braking force to stop the load by gyro effect. The works presented here include the mechanical system of the balance beam controller, the remote controller, the servo controller and the control software for the system. We also present experimental results to show that the system we proposed is useful as a new construction machinery which can control the attitude of the beam hanging from a tower crane.

FLIGHT SOFTWARE DEVELOPMENT FOR THE KODSAT

  • Choi Eun-Jung;Park Suk-June;Kang Suk-Joo;Seo Min-Suk;Chae Jang-Soo;Oh Tae-Sik
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
    • /
    • 한국우주과학회 2004년도 한국우주과학회보 제13권2호
    • /
    • pp.364-367
    • /
    • 2004
  • This paper presents the flight software of KoDSat (KSLV-l Demonstration Satellite) which performs demonstrating the KSLV-l (Korea Space Launch Vehicle-l)'s satellite launch capability. The KoDSat Flight Software executes in a single-processor, multi-function flight computer on the spacecraft, the OBC (On Board Computer). The flight software running on the single processor is responsible for all real-time processing associated with: processor startup and hardware initialization, task scheduling, RS422 handling function, command and data handling including uplink command and down-link telemetry, attitude determination and control, battery state of charge monitoring and control, thermal control processing.

  • PDF