A simplified dynamic model is presented of the Space Shuttle Main Engine (SSME) dynamics valid within the range of operation of the engine. This model is obtained by linking the linearized point models obtained at 25 different operating points of SSME. The simplified model was developed for use with a model-based diagnostic scheme for failure detection and diagnostics studies, as well as control design purposes.
A simplified dynamic model of Space Shuttle Main Engine
1991 American Control Conference ; 1991 ; Boston, MA, United States
1991-01-01
Conference paper
No indication
English