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논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 발행연도
- 2016.10
- 수록면
- 125 - 133 (9page)
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In this paper, we propose a real-time fault monitoring and dual system design of the countdown time-generating system, which is the main component of the mission control system. The countdown time-generating system produces a countdown signal that is distributed to mission control system devices. The stability of the countdown signal is essential for the main launch-related devices because they perform reserved functions based on the countdown time information received from the countdown time-generating system.
Therefore, a reliable and fault-tolerant design is required for the countdown time-generating system. To ensure system reliability, component devices should be redundant and faults should be monitored in real time to manage the device changeover from Active mode to Standby mode upon fault detection. In addition, designing different methods for mode changeover based on fault classification is necessary for appropriate changeover.
This study presents a real-time fault monitoring and changeover system, which is based on the dual system design of countdown time-generating devices, as well as experiment on real-time fault monitoring and changeover based on fault inputs.
Therefore, a reliable and fault-tolerant design is required for the countdown time-generating system. To ensure system reliability, component devices should be redundant and faults should be monitored in real time to manage the device changeover from Active mode to Standby mode upon fault detection. In addition, designing different methods for mode changeover based on fault classification is necessary for appropriate changeover.
This study presents a real-time fault monitoring and changeover system, which is based on the dual system design of countdown time-generating devices, as well as experiment on real-time fault monitoring and changeover based on fault inputs.
목차
Abstract
Ⅰ. Introduction
Ⅱ. Related works
Ⅲ. Structure and Interface of CT Generating System
Ⅳ. Fault Monitoring and Changeover Software between CT Generating Devices
Ⅴ. Evaluation
Ⅵ. Conclusions
REFERENCES
참고문헌 (12)
참고문헌 신청
[학술지(정기간행물)] - Jong-Ho Kim / 2005 / Description of Lauch Control System in Space Center / Current Industrial and Technological Trends in Aerospace 3 (1) : 108 ~ 120
[학술지(정기간행물)] - Yoo-Soo Han / 2008 / Technical Trend of Time Syncronization Equipment in Naro Space Center / Current Industrial and Technological Trends in Aerospace 6 (1) : 114 ~ 121
[학술대회논문] - Yoo-Soo Han / 2008 / An Introduction to the Launch Vehicle Lift-off Signal Processing Equipment at Naro Space Center / The Korean Society For Aeronautical and Space Science 85 (2) : 1112 ~ 1115
[학술대회논문] - Jeong-Seok Kim / 2014 / The BIT Design for Identifying Malfunction in Avionics / The Korea Society For Aeronautical And Space Sciences : 1711 ~ 1714
[학술지(정기간행물)] - Hae-Dong Park / 2007 / Design and Implementation of Embedded Based DCS Terminal Remote Monitoring System / The Korean Society of Computer and Information : 219 ~ 223
[학술지(정기간행물)] - Yoo-Soo Han / 2008 / Technical Trend of Time Syncronization Equipment in Naro Space Center / Current Industrial and Technological Trends in Aerospace 6 (1) : 114 ~ 121
[학술대회논문] - Yoo-Soo Han / 2008 / An Introduction to the Launch Vehicle Lift-off Signal Processing Equipment at Naro Space Center / The Korean Society For Aeronautical and Space Science 85 (2) : 1112 ~ 1115
[학술대회논문] - Jeong-Seok Kim / 2014 / The BIT Design for Identifying Malfunction in Avionics / The Korea Society For Aeronautical And Space Sciences : 1711 ~ 1714
[학술지(정기간행물)] - Hae-Dong Park / 2007 / Design and Implementation of Embedded Based DCS Terminal Remote Monitoring System / The Korean Society of Computer and Information : 219 ~ 223
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