درباره ما
MSFC-RQMT-3255
GLOVEBOX INTEGRATED MICROGRAVITY ISOLATION TECHNOLOGY (G-LIMIT) GROUND TELEMETRY DATA DISPLAY SOFTWARE REQUIREMENTS SPECIFICATION (SWRS)
| contributor author | MSFC - NASA - MSFC - Marshall Space Flight Center | |
| date accessioned | 2017-09-04T15:28:51Z | |
| date available | 2017-09-04T15:28:51Z | |
| date copyright | 04/15/2002 | |
| date issued | 2002 | |
| identifier other | NVWHFBAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/30056 | |
| description abstract | Experiment telemetry from the Microgravity Science Glovebox shall be displayed in three methods. 1. Payloads and Components Real-Time Automated Test System (PACRATS) shall receive data from the ground MLC Server and display all Health and Status data, all Power On Self Test (POST) data, and all 1Hz data with the exception of the 25Hz packet. 2. A COTS product, Matlab (www.mathworks.com) shall be used by the investigator to display the 25Hz data from the 1Hz packet. A program called "pusher" shall request and receive the 25Hz data from the duplicate ground MLC, format it in an appropriate format for Matlab to read and display after an experiment has completed, and write the data to an ASCII text file. 3. A duplicate Crew Interface Software (CIS) Flight Laptop Application (FLA) shall request, receive, and display data in order to duplicate the actual CIS FLA. Refer to Figure 1 for a complete Ground Display Data Flow diagram. | |
| language | English | |
| title | MSFC-RQMT-3255 | num |
| title | GLOVEBOX INTEGRATED MICROGRAVITY ISOLATION TECHNOLOGY (G-LIMIT) GROUND TELEMETRY DATA DISPLAY SOFTWARE REQUIREMENTS SPECIFICATION (SWRS) | en |
| type | standard | |
| page | 32 | |
| status | Active | |
| tree | MSFC - NASA - MSFC - Marshall Space Flight Center:;2002 | |
| contenttype | fulltext |
