Abstract
Aneffective technique is applied to the suppression of vibrations inflexible rotor-bearing systems with small gyroscopic effects. A balanced linear-quadratic-Gaussian(LQG) controller design procedure is implemented. The size of thecontroller is reduced in two stages by using (i) abalanced model reduction, and (ii) an LQG balanced reduction. Thecondition for a gyroscopic matrix is developed that allows oneto ignore the rotor gyroscopic effects in the process ofthe controller design, although they are included in the rotordynamics. The approach is illustrated on a typical rotor-bearing system represented by a 48 degree-of-freedom finite element model.
| Original language | American English |
|---|---|
| Journal | Journal of Engineering for Gas Turbines and Power |
| Volume | 119 |
| DOIs | |
| State | Published - Apr 1 1997 |
Disciplines
- Mechanical Engineering