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Space Shuttle Avionics: Difference between revisions
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→VERT SIT 1 (2) (OPS 305)
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The display is kept largely similar to the original version but does not display the automatic flight control settings of the real Shuttle since the FG version is supposed to be piloted during TAEM and has no routines for automatic aerodynamical flight. | The display is kept largely similar to the original version but does not display the automatic flight control settings of the real Shuttle since the FG version is supposed to be piloted during TAEM and has no routines for automatic aerodynamical flight. | ||
=== RTLS TRAJ 2 (OPS 601) === | |||
[[File:Shuttle avionics rtls.jpg|thumb|RTLS TRAJ 2 display of the Space Shuttle]] | |||
For the powered stage of an RTLS abort, this display provides a set of sample trajectories to guide maneuvering. It is a representation of horizontal velocity component against altitude with a zero line in the center, i.e. at the left end of the display, the Shuttle is flying back to the launch site. | |||
A set of predictors estimate the future state of the Shuttle, and the display also allows to read the remaining propellant, throttle setting and to activate single engine roll control (SERC). | |||
=== TIME (SPEC 2) === | === TIME (SPEC 2) === | ||