Limits of Achievable Performance and Controller Design for the Structural Control Benchmark Problem
Fernando J. D'Amato (Aeronautics and Astronautics, Purdue University)
Mario A. Rotea (Aeronautics and Astronautics, Purdue University)
paper (PDF, 928KB); abstract
| | DAmato |
|
| J1 | 0.213185 |
| J2 | 0.321359 |
| J3 | 0.711925 |
| J4 | 0.708761 |
| J5 | 0.685900 |
| J6 | 0.336429 | 0.379659 |
| J7 | 0.537429 | 0.639790 |
| J8 | 1.027169 | 1.477814 |
| J9 | 1.078193 | 1.390909 |
| J10 | 1.150598 | 1.682684 |
| uRMS | 0.227793 |
| amRMS | 1.227761 |
| xmRMS | 0.932621 |
| uMAX | 0.978243 | 0.711873 |
| amMAX | 5.810519 | 4.341325 |
| xmMAX | 3.461559 | 2.453171 |
|
| | ElCentro | Hachinohe |
|
Numbers in this face represent violated constraints.
Numbers in this face are the larger of the ElCentro/Hachinohe values.
The Kanai-Tajimi results were performed using wg =37.3 rads/sec, zg =0.3, Tf =300 secs.
Page designed by
Erik A. Johnson
(JohnsonE@usc.edu).