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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
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2013
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Article
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Fig 12
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Research Article
Direct Surge Margin Control for Aeroengines Based on Improved SVR Machine and LQR Method
Figure 12
Effects of the ILQR control at the design point.
(a)
Response curves of fan surge margin
(b)
Response curves of compressor corrected speed
(c)
Response curves of nozzle area
(d)
Response curves of main fuel flow