Abstract
An approach to refine H∞-optimal controller for the 4-block H∞ control problem is proposed. The H∞norm of the sub-layers can, therefore, be improved by this approach. Furthermore, a simulation concerning the rotorcraft flight control on time responses is provided. The simulation results bestow a promissing progress both in frequency domain and in the time domain without the inflation of the McMillan degree of the controller.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992 |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 818-824 |
| Number of pages | 7 |
| ISBN (Electronic) | 0780300475, 9780780300477 |
| DOIs | |
| Publication status | Published - 1992 Jan 1 |
| Event | 1st IEEE Conference on Control Applications, CCA 1992 - Dayton, United States Duration: 1992 Sep 12 → 1992 Sep 16 |
Publication series
| Name | Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992 |
|---|
Conference
| Conference | 1st IEEE Conference on Control Applications, CCA 1992 |
|---|---|
| Country | United States |
| City | Dayton |
| Period | 92-09-12 → 92-09-16 |
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All Science Journal Classification (ASJC) codes
- Electrical and Electronic Engineering
- Control and Optimization
- Computer Science (miscellaneous)
- Control and Systems Engineering
- Aerospace Engineering
- Industrial and Manufacturing Engineering
Cite this
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Refined H∞-optimal approach to rotorcraft flight control - A simulation on time responses. / Young, Jieh-Shian; Lin, Chin E.
Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992. Institute of Electrical and Electronics Engineers Inc., 1992. p. 818-824 269742 (Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
TY - GEN
T1 - Refined H∞-optimal approach to rotorcraft flight control - A simulation on time responses
AU - Young, Jieh-Shian
AU - Lin, Chin E.
PY - 1992/1/1
Y1 - 1992/1/1
N2 - An approach to refine H∞-optimal controller for the 4-block H∞ control problem is proposed. The H∞norm of the sub-layers can, therefore, be improved by this approach. Furthermore, a simulation concerning the rotorcraft flight control on time responses is provided. The simulation results bestow a promissing progress both in frequency domain and in the time domain without the inflation of the McMillan degree of the controller.
AB - An approach to refine H∞-optimal controller for the 4-block H∞ control problem is proposed. The H∞norm of the sub-layers can, therefore, be improved by this approach. Furthermore, a simulation concerning the rotorcraft flight control on time responses is provided. The simulation results bestow a promissing progress both in frequency domain and in the time domain without the inflation of the McMillan degree of the controller.
UR - http://www.scopus.com/inward/record.url?scp=33747859488&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=33747859488&partnerID=8YFLogxK
U2 - 10.1109/CCA.1992.269742
DO - 10.1109/CCA.1992.269742
M3 - Conference contribution
AN - SCOPUS:33747859488
T3 - Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992
SP - 818
EP - 824
BT - Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992
PB - Institute of Electrical and Electronics Engineers Inc.
ER -