Name
Abstract | ||
|---|---|---|
In this paper, a class of uncertain linear systems with unmatched disturbances is considered, where the nominal system representation is allowed to be non-minimum phase. A sliding surface is designed which is dependent on the system output, observed state, and estimated uncertain parameters. A linear coordinate transformation is introduced so that the stability analysis of the reduced-order sliding mode dynamics can be conveniently performed. A robust output feedback sliding mode control (OFSMC) is then designed to drive the considered system state to reach the sliding surface in finite time and maintain a sliding motion thereafter. A simulation example for a high incidence research model (HIRM) aircraft is used to demonstrate the effectiveness of the proposed method. |
Year | DOI | Venue |
|---|---|---|
2022 | 10.1177/01423312211050741 | TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL |
Keywords | DocType | Volume |
Sliding mode control, non-minimum phase, dynamical output feedback, regular form, unmatched disturbances | Journal | 44 |
Issue | ISSN | Citations |
6 | 0142-3312 | 0 |
PageRank | References | Authors |
0.34 | 0 | 4 |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Jiehua Feng | 1 | 0 | 0.34 |
| Dongya Zhao | 2 | 118 | 16.58 |
| xinggang yan | 3 | 471 | 46.12 |
| sarah k spurgeon | 4 | 724 | 71.21 |