2814310

Model Identification for the Space Shuttle Main Engine High Pressure Oxidizer Turbopump

Brown, Joseph R. ; Irwin, R. Dennis ; Mitchell, J. Ross

Department of Electrical and Computer, Ohio University

1992

1-3 Mar 1992

575

578

Accelerometers; Differential equations; Engines; NASA; Poles and zeros; Signal to noise ratio; Space shuttles; Strain measurement; System testing; Transfer functions;

English

ieee

System Theory, 1992. Proceedings. SSST/CSA 92. The 24th Southeastern Symposium on and The 3rd Annual Symposium on Communications, Signal Processing Expert Systems, and ASIC VLSI Design

0094-2898

0-8186-2665-8

conf

10.1109/SSST.1992.712373

712373