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Space Shuttle Avionics: Difference between revisions
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→SM APU/HYD (DISP 86)
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On this display, a summary of various pressure and temperature readings of the APU and hydraulics systems can be accessed. All parameters are meaningful and represent the internal state of the simulation and possible failure modes. | On this display, a summary of various pressure and temperature readings of the APU and hydraulics systems can be accessed. All parameters are meaningful and represent the internal state of the simulation and possible failure modes. | ||
=== PDRS CONTROL (SPEC 94) === | |||
[[File:Shuttle avionics disp94.jpg|600px|PDRS control display of the Space Shuttle]] | |||
Using the PDRS (payload deployment and retrieval system) control utility page, various readings of the RMS arm state can be monitored as well as automatic modes configured. | |||
Most important is the central part of the display where a target position and attitude for the end effector can be entered, and in the operator commanded auto mode, the RMS arm can then be moved to the entered target. | |||
In the lower portion of the screen, ready for latch indicators and the MPM status indicators are displayed. | |||
=== SM PL RETENTION (DISP 97) === | === SM PL RETENTION (DISP 97) === | ||