Abstract
This paper presents the control strategy used in a novel concept termed Smart Mesoflaps for Aeroelastic Recirculation Transpiration (SMART) aimed at controlling shock/boundary-layer interactions (SBLI) in supersonic jet inlets. A basic PID controller used initially effectively meets the performance requirements. However, this sometimes results in actuation saturation, which can be very damaging to the SMART hardware. Therefore, a generalized error governing scheme for PID controllers is developed to compensate for actuator saturations. This method can be generalized to any stable process controlled by a PID, and has advantages over traditional anti-windup controllers. The PID 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) |
|---|---|
| Pages (from-to) | 346-351 |
| Number of pages | 6 |
| Journal | Proceedings of the American Control Conference |
| Volume | 1 |
| State | Published - 2002 |
| Externally published | Yes |
| Event | 2002 American Control Conference - Anchorage, AK, United States Duration: May 8 2002 → May 10 2002 |