Abstract
A direct decentralized approach to the design of integrated flight/propulsion control (IFPC) systems is considered in order to reduce complexity and validation drawbacks of centralized designs. The imposed triangular decentralized structure on the IFPC controller allows for separate evaluation of the engine controller as well as for the evaluation of the achievable performance of the overall IFPC system. H∞ techniques which require the solution to Riccati-like equations are used to develop the design method. This method is applied to an aircraft aero-propulsive model and the results indicate that the approach may be a vital alternative to other techniques appearing in the literature.
| Original language | English (US) |
|---|---|
| Pages | 1866-1872 |
| Number of pages | 7 |
| State | Published - Jan 1 1998 |
| Event | Guidance, Navigation, and Control Conference and Exhibit, 1998 - Boston, United States Duration: Aug 10 1998 → Aug 12 1998 |
Other
| Other | Guidance, Navigation, and Control Conference and Exhibit, 1998 |
|---|---|
| Country | United States |
| City | Boston |
| Period | 8/10/98 → 8/12/98 |
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ASJC Scopus subject areas
- Aerospace Engineering
- Control and Systems Engineering
- Electrical and Electronic Engineering
Cite this
Decentralized design for integrated flight/propulsion control of aircraft. / Chen, Zhenyang; Voulgaris, Petros G.
1998. 1866-1872 Paper presented at Guidance, Navigation, and Control Conference and Exhibit, 1998, Boston, United States.Research output: Contribution to conference › Paper
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TY - CONF
T1 - Decentralized design for integrated flight/propulsion control of aircraft
AU - Chen, Zhenyang
AU - Voulgaris, Petros G
PY - 1998/1/1
Y1 - 1998/1/1
N2 - A direct decentralized approach to the design of integrated flight/propulsion control (IFPC) systems is considered in order to reduce complexity and validation drawbacks of centralized designs. The imposed triangular decentralized structure on the IFPC controller allows for separate evaluation of the engine controller as well as for the evaluation of the achievable performance of the overall IFPC system. H∞ techniques which require the solution to Riccati-like equations are used to develop the design method. This method is applied to an aircraft aero-propulsive model and the results indicate that the approach may be a vital alternative to other techniques appearing in the literature.
AB - A direct decentralized approach to the design of integrated flight/propulsion control (IFPC) systems is considered in order to reduce complexity and validation drawbacks of centralized designs. The imposed triangular decentralized structure on the IFPC controller allows for separate evaluation of the engine controller as well as for the evaluation of the achievable performance of the overall IFPC system. H∞ techniques which require the solution to Riccati-like equations are used to develop the design method. This method is applied to an aircraft aero-propulsive model and the results indicate that the approach may be a vital alternative to other techniques appearing in the literature.
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M3 - Paper
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SP - 1866
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