REG NASA-LLIS-0209-1992 Lessons Learned - Time Correlation Between Multiple Telemetry Systems.pdf
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1、Lessons Learned Entry: 0209Lesson Info:a71 Lesson Number: 0209a71 Lesson Date: 1992-11-13a71 Submitting Organization: KSCa71 Submitted by: Lisa L. MusgraveSubject: Time Correlation Between Multiple Telemetry Systems Description of Driving Event: The Space Shuttle Main Engine (SSME) telemetry system
2、does not show absolute Greenwich Mean Time (GMT), but rather, the number of controller cycles since change in mode. Approximate timing had been established (during the STS 51-L launch process) by aligning the first guidance cycle after engine start with the engine start command time determined by an
3、alysis of the General Purpose Computer (GPC) event times. This aligned the SSME event times to the GPC event times to within a few tens of milliseconds, sufficient for normal flight analysis but insufficient for determining event sequencing for a system failure, which involves an interaction between
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