NASA NTRS · 19890066697
Identification of Space Shuttle Main Engine dynamics
Abstract
System identification techniques are used to represent the dynamic behavior of the Space Shuttle Main Engine. The transfer function matrices of the linearized models of both the closed loop and the open loop system are obtained by using the recursive maximum likelihood method.
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Duyar, Ahmet, Guo, Ten-Huei, Merrill, Walter C.. 1989-01-01. Identification of Space Shuttle Main Engine dynamics. https://ntrs.nasa.gov/citations/19890066697
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