Hu, Qinglei, Meng, Yao, Wang, Chenliang and Zhang, Youmin (2017) Adaptive Backstepping Control for Air-Breathing Hypersonic Vehicles with Input Nonlinearities. Aerospace Science and Technology . pp. 1-27. ISSN 12709638 (In Press)
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Official URL: http://dx.doi.org/10.1016/j.ast.2017.12.001
Abstract
This paper addresses the control problem of air-breathing hypersonic vehicles subject to input nonlinearities, aerodynamic uncertainties and flexible modes. An adaptive backstepping controller and a dynamic inverse controller are developed for the altitude subsystem and the velocity subsystem, respectively, where the former eliminates the problem of “explosion of terms” inherent in backstepping control. Moreover, a modified smooth inverse of the dead-zone is proposed to compensate for the dead-zone effects and reduce the computational burden. Based on this smooth inverse, an input nonlinear pre-compensator is designed to handle input saturation and dead-zone nonlinearities, which leads to a simpler control design for the altitude subsystem subject to these two input nonlinearities. It is proved that the proposed controllers can guarantee that all closed-loop signals are bounded and the tracking errors converge to an arbitrarily small residual set. Simulation results are carried out to demonstrate the effectiveness of the proposed control scheme.
| Divisions: | Concordia University > Gina Cody School of Engineering and Computer Science > Mechanical, Industrial and Aerospace Engineering |
|---|---|
| Item Type: | Article |
| Refereed: | Yes |
| Authors: | Hu, Qinglei and Meng, Yao and Wang, Chenliang and Zhang, Youmin |
| Journal or Publication: | Aerospace Science and Technology |
| Date: | 12 December 2017 |
| Funders: |
|
| Digital Object Identifier (DOI): | 10.1016/j.ast.2017.12.001 |
| Keywords: | hypersonic vehicle; flexible modes; input nonlinearities; dead-zone; input saturation |
| ID Code: | 983309 |
| Deposited By: | Danielle Dennie |
| Deposited On: | 14 Dec 2017 01:52 |
| Last Modified: | 08 Dec 2018 01:00 |
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