The factors leading to the particular design of the Shuttle guidance, navigation and control software are discussed. The derivation of explicit guidance equations satisfying a wide range of different maneuver constraints and steering equations that create attitude steering errors from the guidance solutions is presented, as are navigation equations, and equations for identifying faulty instruments from sets of redundant instrument measurements.
Space Shuttle Ascent Guidance, Navigation, and Control
01.03.1979
Sonstige
Keine Angabe
Englisch
The Space Shuttle ascent guidance and control
AIAA | 1982
|Shuttle ascent guidance and control.
NTRS | 1972
|Tema Archiv | 1989
|SAE Technical Papers | 1989
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