Publication Date:
2019-07-13
Description:
This brief paper summarizes the approach the authors will take in designing a feedback controller for the F-100 turbofan engine. The technique to be utilized simultaneously realizes dominant closed-loop eigenvalues, approximates specified modal behavior, and achieves low eigensystem sensitivity with respect to certain plant parameter variations.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
Joint Automatic Control Conference; Jun 17, 1979 - Jun 21, 1979; Denver, CO
Format:
text
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