Abstract
This paper introduces an experimental solution for H∞ weighting function selection by exploiting an experimental planning method which has been used in quality control. Conducting matrix experiments using special matrices, called orthogonal arrays, allows the effects of several weighting parameters to be determined efficiently so that the resulting H∞ controller can satisfy many design specifications simultaneously in the environment for which the controller is designed. To show the feasibility and efficiency of this methodology, a flight control system for an airplane is designed to satisfy 11 performance specifications simultaneously, while the airplane is undergoing a large shift in c.g. position.
| Original language | English |
|---|---|
| Pages (from-to) | 2516-2520 |
| Number of pages | 5 |
| Journal | Proceedings of the American Control Conference |
| Volume | 3 |
| Publication status | Published - 1994 |
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All Science Journal Classification (ASJC) codes
- Electrical and Electronic Engineering
Cite this
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Experimental design of H∞ weighting functions for flight control systems. / Yang, Ciann-Dong; Ju, Hann Shing; Liu, Shin Whar.
In: Proceedings of the American Control Conference, Vol. 3, 1994, p. 2516-2520.Research output: Contribution to journal › Article
TY - JOUR
T1 - Experimental design of H∞ weighting functions for flight control systems
AU - Yang, Ciann-Dong
AU - Ju, Hann Shing
AU - Liu, Shin Whar
PY - 1994
Y1 - 1994
N2 - This paper introduces an experimental solution for H∞ weighting function selection by exploiting an experimental planning method which has been used in quality control. Conducting matrix experiments using special matrices, called orthogonal arrays, allows the effects of several weighting parameters to be determined efficiently so that the resulting H∞ controller can satisfy many design specifications simultaneously in the environment for which the controller is designed. To show the feasibility and efficiency of this methodology, a flight control system for an airplane is designed to satisfy 11 performance specifications simultaneously, while the airplane is undergoing a large shift in c.g. position.
AB - This paper introduces an experimental solution for H∞ weighting function selection by exploiting an experimental planning method which has been used in quality control. Conducting matrix experiments using special matrices, called orthogonal arrays, allows the effects of several weighting parameters to be determined efficiently so that the resulting H∞ controller can satisfy many design specifications simultaneously in the environment for which the controller is designed. To show the feasibility and efficiency of this methodology, a flight control system for an airplane is designed to satisfy 11 performance specifications simultaneously, while the airplane is undergoing a large shift in c.g. position.
UR - http://www.scopus.com/inward/record.url?scp=0028584946&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0028584946&partnerID=8YFLogxK
M3 - Article
VL - 3
SP - 2516
EP - 2520
JO - Proceedings of the American Control Conference
JF - Proceedings of the American Control Conference
SN - 0743-1619
ER -