1. 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):094502-094502-6. doi:10.1115/1.4007011 Comparison of transient response of state signals, x0=[−0.2−0.3]T Figure Legend:

2. 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):094502-094502-6. doi:10.1115/1.4007011 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:

3. 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):094502-094502-6. doi:10.1115/1.4007011 Comparison of transient response of state signals, x0=[−0.2−0.3]T Figure Legend:

4. 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):094502-094502-6. doi:10.1115/1.4007011 Comparison of regulation performance of output signals Figure Legend:

5. 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):094502-094502-6. doi:10.1115/1.4007011 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: