Back to Search
Start Over
Identification of the Space Shuttle Main Engine dynamic models from firing data
- Publication Year :
- 1992
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1992.
-
Abstract
- A multi-input multi-output system identification technique is used to obtain linearized point models of the Space Shuttle Main Engine (SSME) at five different operating conditions (power levels) from the engine firing data. This study demonstrates that the open-loop dynamics of the SSME can be successfully modeled from the engine firing data. The identified linear models may be used for fault detection studies and control system design and development.
- Subjects :
- Spacecraft Propulsion And Power
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Notes :
- NAG3-1006
- Publication Type :
- Report
- Accession number :
- edsnas.19920071398
- Document Type :
- Report