Abstract
The feasibility of using piezoelectric materials as dual-purpose structural elements/actuators for vibration suppression in large space structures was demonstrated. Positive position feedback (PPF) as a vibration suppression control strategy was implemented. Using the strain sensor which measures the elastic deformation for control was successfully demonstrated. Multi-mode vibration suppression was achieved with dramatic reduction in dynamic response. No destabilizing effects were observed due to either the spillover or the actuator dynamics. A better synthesis theory which provides procedures for the selection of gains for strong structure/control coupling should be developed. A true active member needs to be developed and incorporated into more complicated experiments.
| Original language | English |
|---|---|
| Pages (from-to) | 809-829 |
| Number of pages | 21 |
| Journal | NASA Conference Publication |
| Issue number | pt 2 |
| Publication status | Published - 1987 |
| Externally published | Yes |