Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Nonlinear Control of Aircraft Engines Using a Generalized Gronwall-Bellman Lemma Approach J. Eng. Gas Turbines Power. 2012;134(9): doi: / Comparison of transient response of state signals, x0=[−0.2−0.3]T Figure Legend:

Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Nonlinear Control of Aircraft Engines Using a Generalized Gronwall-Bellman Lemma Approach J. Eng. Gas Turbines Power. 2012;134(9): doi: / Comparison of transient response for \|x(t) ‖ with theoretical bound. Right corner is the magnified view of the state norm evolution for controlled and uncontrolled systems. Figure Legend:

Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Nonlinear Control of Aircraft Engines Using a Generalized Gronwall-Bellman Lemma Approach J. Eng. Gas Turbines Power. 2012;134(9): doi: / Comparison of transient response of state signals, x0=[−0.2−0.3]T Figure Legend:

Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Nonlinear Control of Aircraft Engines Using a Generalized Gronwall-Bellman Lemma Approach J. Eng. Gas Turbines Power. 2012;134(9): doi: / Comparison of regulation performance of output signals Figure Legend:

Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Nonlinear Control of Aircraft Engines Using a Generalized Gronwall-Bellman Lemma Approach J. Eng. Gas Turbines Power. 2012;134(9): doi: / Tracking performance of the proposed design. Also shown is the performance for corresponding linearized systems (a) PCN2R, (b) P56/P25, (c) P16/P56. Figure Legend: