A Simplified Dynamic Model of the Space Shuttle Main Engine | Zendy

Ahmet Duyar | Zendy; Vasfi Eldem | Zendy; Walter C. Merrill | Zendy; Ten-Huei Guo | Zendy

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A Simplified Dynamic Model of the Space Shuttle Main Engine

Author(s) -

Ahmet Duyar,

Vasfi Eldem,

Walter C. Merrill,

Ten-Huei Guo

Publication year - 1994

Publication title -

journal of dynamic systems measurement and control

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.528

H-Index - 89

eISSN - 1528-9028

pISSN - 0022-0434

DOI - 10.1115/1.2899286

Subject(s) - space shuttle , range (aeronautics) , operating point , nonlinear system , point (geometry) , nonlinear model , control theory (sociology) , computer science , space (punctuation) , simulation , control (management) , engineering , aerospace engineering , mathematics , electronic engineering , physics , geometry , quantum mechanics , artificial intelligence , operating system

This paper presents a simplified model 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 twenty five differenc operating points of the 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.

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