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EP1538319A1
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Apparatus for model predictive control of aircraft gas turbine engines
Assignee: General Electric Co
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Filing: 2003-12-05
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Granted: —
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Expires: 2023-12-05
Abstract
Abstract A method of designing the operations and controls of a aircraft gas turbine engine (10) includes generating an operations model for the gas turbine include at least one objective function, defining operations and control constraints for the operations model of the gas turbine, and providing an online dynamic optimizer/controller that dynamically optimizes and controls operation of the gas turbine using model predictive control based on the operations model and the operations and control constraints using an Extended Kalman Filter for estimation.
Inventors
- 👤 Brent Jerome Brunell
Bibliographic Details
Application Number
—
Jurisdiction
EP
Data Source
google_patents
Last Synchronized
2026-10-30 13:40
CPC Classifications
G; G05; G05B; G05B13/00; G05B13/02; G05B13/04; G05B13/042; F; F02; F02C; F02C9/00; F05; F05D; F05D2270/00; F05D2270/40; F05D2270/44
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
98 words
A system for designing the operations and controls of an aircraft gas
turbine engine (10), said system comprising: a computing unit with an input unit for generating an operations model
for the aircraft gas turbine engine to include at least one objective function
and for defining operations and controls constraints for the operations model
of the aircraft gas turbine engine; and a dynamic online optimizer/controller configured to dynamically
optimize and control operation of the gas turbine using model predictive
control based on the operations model and the operations and control
constraints using an Extended Kalman Filter for estimation.
Claim 2
Dependent Claim
64 words
A system according to Claim 1, wherein said optimizer/controller is
configured to perform the following steps in a loop: (A) estimating the current
engine (10) state and applicable constraints; (B) for a given control/simulation
time period, determining a control action by optimizing an objective function
based on the operation model while respecting the applicable constraints; (C)
executing the control action determined in step (B).
Claim 3
Dependent Claim
19 words
A system in accordance with Claim 1 wherein said optimizer/controller
is configured to compute the gradient of J wherein
Claim 4
Dependent Claim
29 words
A system in accordance with Claim 3 wherein said optimizer/controller
is configured to traverse the gradient in a negative direction until a number of
steps equals a predetermined number.
Claim 5
Dependent Claim
24 words
A system in accordance with Claim 3 wherein said optimizer/controller
is configured to traverse the gradient in a negative direction until J is
minimized.
Claim 6
Dependent Claim
29 words
A system in accordance with Claim 3 wherein said optimizer/controller
is configured to traverse the gradient in a negative direction until an elapsed
time exceeds a predetermined time interval.
References Cited (Backward Citations)
US4215412A
Cited
EP0315307A2
Cited
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