.png){kind=icon}
返回
Gravity Probe B data system description
.png){kind=icon}
PRE
AI
DOI：10.1088/0264-9381/32/22/224013.png)
.png){kind=icon}
原文求助.png){kind=icon}
分享.png){kind=icon}
收藏
摘要
En 中文
The Gravity Probe B data system, developed, integrated, and tested by Lockheed Missiles & Space Company, and later Lockheed Martin Corporation, included flight and ground command, control, and communications software. The development was greatly facilitated, conceptually and by the transfer of key personnel, through Lockheed's earlier flight and ground test software development for the Hubble Space Telescope (HST). Key design challenges included the tight mission timeline (17 months, 9 days of on-orbit operation), the need to tune the system once on-orbit, and limited 2 Kbps real-time data rates and ground asset availability. The result was a completely integrated space vehicle and Stanford mission operations center, which successfully collected and archived 97% of the 'guide star valid' data to support the science analysis. Lessons learned and incorporated from the HST flight software development and on-orbit support experience, and Lockheed's independent research and development effort, will be discussed.
Keyword:
data system
software architecture
flight software
ground software
space vehicle
Gravity Probe B
AI总结
对已上传原文的论文进行重点信息的提取，主要内容包括：简要概述、研究摘要、背景介绍、关键亮点、图文解析、展望与总结。
期刊
IF:
3.7
论文数:
1.3W
被引数:
3.0W
.png){kind=icon}
