Gravity Probe B data system description

被引:2
作者
Bennett, Norman R. [1 ]
机构
[1] Lockheed Martin Corp, Bethesda, MD 20817 USA
关键词
data system; software architecture; flight software; ground software; space vehicle; Gravity Probe B;
D O I
10.1088/0264-9381/32/22/224013
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
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.
引用
收藏
页数:33
相关论文
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