Abstract
This paper introduces a novel concept termed Smart Mesoflaps for Aeroelastic Recirculation Transpiration (SMART) for controlling shock/boundary-layer interactions (SBLI) in supersonic jet inlets. The control strategy for a subsystem of the SMART project, subject to hysteresis and actuator saturation, is presented. A Hysteresis Compensation scheme, as well as results from experimental application of HC to the SMART system are presented next. A generalized error governing scheme for PID controllers to compensate for actuator saturations is also developed. Finally, the PID with HC and the error governing method is experimentally applied to a benchtop SMART subsystem and is shown to be successful at preventing excessive control efforts.
| Original language | English (US) |
|---|---|
| Title of host publication | IFAC Proceedings Volumes (IFAC-PapersOnline) |
| Editors | Gabriel Ferrate, Eduardo F. Camacho, Luis Basanez, Juan. A. de la Puente |
| Publisher | IFAC Secretariat |
| Pages | 205-210 |
| Number of pages | 6 |
| Edition | 1 |
| ISBN (Print) | 9783902661746 |
| DOIs | |
| State | Published - 2002 |
| Externally published | Yes |
| Event | 15th World Congress of the International Federation of Automatic Control, 2002 - Barcelona, Spain Duration: Jul 21 2002 → Jul 26 2002 |
Publication series
| Name | IFAC Proceedings Volumes (IFAC-PapersOnline) |
|---|---|
| Number | 1 |
| Volume | 15 |
| ISSN (Print) | 1474-6670 |
Other
| Other | 15th World Congress of the International Federation of Automatic Control, 2002 |
|---|---|
| Country/Territory | Spain |
| City | Barcelona |
| Period | 7/21/02 → 7/26/02 |
Bibliographical note
Funding Information:1 This work is supported by DARPA under contract F49620-98-1-0490
Publisher Copyright:
Copyright © 2002 IFAC.
Keywords
- Actuators
- Aerospace control
- Control design
- Error analysis
- Error control
- Flow control
- Hysteresis
- PID controllers
- Saturation