Feedback control system and method that selectively utilizes observer estimates

• US 7,630,820 B2
• Filed: 04/24/2007
• Issued: 12/08/2009
• Est. Priority Date: 04/24/2007
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Ling, Richard, Sims, Jay R.
• Primary Examiner(s): ARTHUR JEANGLAUDE, GERTRUDE
• Application Number:
  US11/739,461
• Publication Number:
  US 20080270003A1
• Time in Patent Office: 959 Days
• Field of Search: 701/53, 701/54, 701/61, 701/100, 701/101, 477/30, 477/54, 60/392.81, 607/73
• US Class Current: 701/100
• CPC Class Codes: F02C 9/28 Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed F02C9/30 - F02C9/38, F02C9/44 take precedence
• CPC Class Codes: F05D 2270/44 active, predictive, or anticipative
• CPC Class Codes: F05D 2270/54 by electronic means, e.g. electronic tubes, transistors or IC's within an electronic circuit
• CPC Class Codes: F05D 2270/708 with comparison tables
• CPC Class Codes: F05D 2270/71 synthesized, i.e. parameter computed by a mathematical model

Abstract

A system and method implements improved machine performance, most preferably for gas turbine engines. The system and method implement a control law that receives sensed operational parameter feedback signals. For each sensed engine operational parameter, the feedback signals that are supplied to the control law selectively comprise the sensor signal representative of the engine operational parameter, if the sensor signal is valid, or an observer estimate of the sensed engine operational parameter, if the sensor signal is invalid.

Claims

1. A control system for a gas turbine engine including a plurality of actuators, the system comprising:

an engine control law adapted to receive input commands and a plurality of feedback signals, each feedback signal representative of a sensed engine operational parameter, the engine control operable, in response to the input commands and the plurality of feedback signals, to supply engine actuator commands;

a gas turbine engine observer adapted to receive the engine actuator commands and a plurality of sensor signals, each sensor signal representative of one of the sensed engine operational parameters, the gas turbine engine observer operable, in response to the engine actuator commands and the plurality of sensor signals, to supply estimates of each of the sensed engine operational parameters; and

a feedback signal selection function adapted to receive the estimates of the sensed engine operational parameters and the plurality of sensor signals, the feedback signal selection function configured to selectively supply each of the feedback signals representative of a sensed engine operational parameter as either (i) the sensor signal representative thereof or (ii) the estimate thereof.

2. The system of claim 1, further comprising:

a sensor fault determination function coupled to receive the plurality of sensor signals and operable, in response thereto, to (i) determine if each of the sensor signals is invalid and (ii) supply feedback control signals representative of the determination to the feedback signal selection function,

wherein the feedback signal selection function is responsive to the feedback control signals such that each of the feedback signals supplied thereby to the control law is (i) the sensor signal representative of the sensed engine operational parameter if the sensor signal is valid and (ii) the estimate of the sensed engine operational parameter if the sensor signal is invalid.

3. The system of claim 2, further comprising:

a residual generator coupled to receive the estimates and the sensor signals and operable, in response thereto, to generate residuals, each residual representative of a difference between an estimate and a sensor signal.

4. The system of claim 3, wherein:

the gas turbine engine observer includes a non-linear component map model of the gas turbine engine;

the gas turbine engine observer is further configured to generate a plurality of state biases, each state bias being generated as a function of one of the generated residuals;

the non-linear component map model is coupled to receive at least a subset of the state biases; and

the non-linear component map model is configured to be updated in response to the state biases received thereby.

5. The system of claim 4, further comprising:

an observer mode select function operable to selectively supply one or more of the state biases to the non-linear component map model.

6. The system of claim 5, wherein the observer mode select function is coupled to receive a mode control signal representative of sensor signals that are invalid and is operable, in response thereto, to supply state biases associated with the sensor signals that are valid to the non-linear component map model.

7. The system of claim 5, further comprising:

a plurality of ambient condition sensors, each ambient condition sensor operable to (i) sense an ambient condition associated with the gas turbine engine and (ii) supply an ambient condition signal representative thereof,

wherein the gas turbine engine observer is further configured to correct at least a portion of the generated residuals based on the one or more determined ambient operating conditions.

8. The system of claim 5, wherein the gas turbine engine observer further includes a plurality of piecewise linear gains and is further operable to selectively apply one of the plurality of piecewise linear gains to each of the generated residuals.

9. The method of claim 8, further comprising:

a plurality of ambient condition sensors, each ambient condition sensor operable to (i) sense an ambient condition associated with the gas turbine engine and (ii) supply an ambient condition signal representative thereof,

wherein the gas turbine engine observer is further configured to correct the applied piecewise linear gain based on the one or more determined ambient operating conditions.

10. The system of claim 1, further comprising:

a plurality of engine sensors, each engine sensor configured to sense one of the engine operational parameters and supply a sensor signal representative the sensed engine operational parameter.

11. The system of claim 1, wherein the sensed engine operational parameters include (i) parameters representative of engine performance and (ii) parameters representative of controlled engine parameters.

12. A method of controlling a gas turbine engine having engine actuators, the method comprising the steps of:

sensing engine operational parameters and supplying, for each sensed engine operational parameter, a sensor signal representative thereof;

generating a gas turbine engine observer, the gas turbine engine observer responsive to engine actuator commands and at least some of the sensed engine operational parameters to supply estimates of each sensed engine operational parameter;

supplying engine actuator commands from an engine control law to the gas turbine engine observer and to the engine actuators;

determining if each of the sensor signals is invalid; and

for each of the sensed engine operational parameters, supplying a feedback signal representative thereof to the engine control law, the supplied feedback signal being (i) the sensor signal representative of the engine operational parameter if the sensor signal is valid and (ii) the estimate of the sensed engine operational parameter if the sensor signal is invalid.

13. The method of claim 12, further comprising:

for each of the sensed engine operational parameters, comparing the estimate supplied by the gas turbine engine observer to the sensor signal to generate residuals.

14. The method of claim 13, wherein the gas turbine engine observer includes a non-linear component map model of the gas turbine engine, and wherein the method further comprises:

generating a plurality of state biases, each state bias being generated as a function of a residual; and

updating the non-linear component map model using at least a subset of the generated state biases.

15. The method of claim 14, further comprising:

updating the non-linear component map model using the generated state biases associated with the sensor signals that are valid.

16. The method of claim 13, further comprising:

determining one or more ambient conditions associated with the gas turbine engine; and

correcting at least a portion of the generated residuals based on the one or more determined ambient operating conditions.

17. The method of claim 13, further comprising:

selectively applying one of a plurality of piecewise linear gains to each of the generated residuals.

18. The method of claim 17, further comprising:

determining one or more ambient conditions associated with the gas turbine engine; and

correcting the applied piecewise linear gain based on the one or more determined ambient operating conditions.

19. The method of claim 12, wherein the engine operational parameters include (i) parameters representative of engine performance and (ii) parameters representative of controlled engine parameters.

20. A gas turbine engine system, comprising:

a gas turbine engine including a plurality of actuators and a plurality of sensors, each sensor operable to sense an engine operational parameter and supply a sensor signal representative thereof, and

an engine controller coupled to the gas turbine engine adapted to receive input commands and a plurality of feedback signals, each feedback signal representative of a sensed engine operational parameter, the engine controller operable, in response to the input commands and the plurality of feedback signals, to supply at least engine actuator commands to the plurality of engine actuators, the engine controller including;

an engine control law adapted to receive the input commands and the plurality of feedback signals and operable, in response thereto, to supply the engine actuator commands,

a gas turbine engine observer adapted to receive the engine actuator commands and at least a portion of the sensor signals and operable, in response thereto, to supply estimates of each of the sensed engine operational parameters; and

a feedback signal selection function adapted to receive the estimates of the sensed engine operational parameters and each of the sensor signals, the feedback signal selection function configured to selectively supply each of the feedback signals representative of a sensed engine operational parameter as either (i) the sensor signal representative thereof or (ii) the estimate thereof.

21. A control system for a machine including a plurality of actuators, the system comprising:

a control law adapted to receive input commands and a plurality of feedback signals, each feedback signal representative of a sensed machine operational parameter, the control law operable, in response to the input commands and the plurality of feedback signals, to supply machine actuator commands;

a machine observer adapted to receive the machine actuator commands and a plurality sensor signals, each sensor signal representative of one of the sensed machine operational parameters, the machine observer operable, in response to the machine actuator commands and the sensor signals, to supply estimates of each of the sensed machine operational parameters; and

a feedback signal selection function adapted to receive the estimates of the sensed machine operational parameters and the plurality of sensor signals, the feedback signal selection function configured to selectively supply each of the feedback signals representative of a sensed machine operational parameter as either (i) the sensor signal representative thereof or (ii) the estimate thereof.