Compact aero-thermo model real time linearization based state estimator

Patent metadata

Field	Value
Publication number	US-9915206-B2
Application number	US-201414765672-A
Country	US
Kind code	B2
Filing date	Mar 14, 2014
Priority date	Mar 15, 2013
Publication date	Mar 13, 2018
Grant date	Mar 13, 2018

Abstract

Systems and methods for controlling a fluid based engineering system are disclosed. The systems and methods may include a model processor for generating a model output, the model processor including a set state module for setting dynamic states of the model processor, the dynamic states input to an open loop model based on the model operating mode. The model processor may further include an estimate state module for determining an estimated state of the model based on a prior state model output and the current state model of the open loop model the estimate state module using online linearization and gain calculation to determine estimator gain for determining the estimated state of the model.

First claim

What is claimed is:

1. A control system, comprising:
an actuator for positioning a control device comprising a control surface, wherein the actuator positions the control surface in order to control a model state;
a control law for directing the actuator as a function of a model output; and
a model processor for generating the model output, the model processor comprising:
an input object for processing model input and setting a model operating mode;
a set state module for setting dynamic states of the model processor, the dynamic states input to an open loop model based on the model operating mode;
wherein the open loop model generates a current state model as a function of the dynamic states and the model input, wherein a constraint on the current state model is based on a series of cycle synthesis modules, each member of the series of cycle synthesis modules modeling a component of a cycle of the control device and comprising a series of utilities, the utilities based on mathematical abstractions of physical properties associated with the component;
an estimate state module for determining an estimated state of the model based on a prior state model output and the current state model of the open loop model, the estimate state module using online linearization and gain calculation to determine estimator gain for determining the estimated state of the model; and
an output object for processing the estimated state of the model to determine the model output.

2. The control system of claim 1 , wherein online linearization and gain calculation comprises obtaining partial derivatives based on the current state model.

3. The control system of claim 2 , wherein the partial derivatives based on the current state model are a Jacobian matrix.

4. The control system of claim 2 , wherein online linearization and gain calculation further comprises constructing a linear system for gain design using the partial derivatives based on the current state model.

5. The control system of claim 4 , wherein online linearization and gain calculation further comprises determining the estimator gain based on the linear system for gain design.

6. The control system of claim 1 , wherein the estimator gain is used in minimizing error vectors of the current state model.

7. The control system of claim 6 , wherein the estimate state model uses numerical integration to determine the estimated state of the model based on a prior state and a current state derivative.

8. The control system of claim 1 , wherein the control device is a gas turbine engine.

9. The control system of claim 8 , wherein the one or more cycle synthesis modules are based on one or more mathematical abstractions of physical processes associated with components of a thermodynamic cycle of the gas turbine engine.

10. A method for controlling a control device, the method comprising:
generating a model output using a model processor, the model processor comprising:
an input object for processing model input and setting a model operating mode;
a set state module for setting dynamic states of the model processor, the dynamic states input to an open loop model based on the model operating mode;
wherein the open loop model generates a current state model as a function of the dynamic states and the model input, wherein a constraint on the current state model is based on a series of cycle synthesis modules, each member of the series of cycle synthesis modules modeling a component of a cycle of the control device and comprising a series of utilities, the utilities based on mathematical abstractions of physical properties associated with the component;
an estimate state module for determining an estimated state of the model based on a prior state model output and the current state model of the open loop model the estimate state module using online linearization and gain calculation to determine estimator gain for determining the estimated state of the model; and
an output object for processing the estimated state of the model to determine a model output;

directing an actuator associated with the control device as a function of the model output using a control law; and
positioning the control device comprising a control surface using the actuator, wherein the actuator positions the control surface in order to control the model state.

11. The method of claim 10 , wherein online linearization and gain calculation comprises obtaining partial derivatives based on the current state model.

12. The method of claim 11 , wherein online linearization and gain calculation further comprises constructing a linear system for gain design using the partial derivatives based on the current state model.

13. The method of claim 12 , wherein online linearization and gain calculation further comprises determining the estimator gain based on the linear system for gain design.

14. The method of claim 10 , wherein the estimator gain is used in minimizing error vectors of the current state model.

15. The method of claim 14 , wherein the estimate state model uses numerical integration to determine the estimated state of the model based on a prior state and a current state derivative.

16. A gas turbine engine comprising:
a fan;
a compressor section downstream of the fan;
a combustor section downstream of the compressor section;
a turbine section downstream of the combustor section;
an actuator for positioning the gas turbine engine, wherein the actuator positions a control surface of an element of the gas turbine engine in order to control a model state;
a control law for directing the actuator as a function of a model output;
a model processor for generating the model output, the model processor comprising:
an input object for processing model input and setting a model operating mode;
a set state module for setting dynamic states of the model processor, the dynamic states input to an open loop model based on the model operating mode;
wherein the open loop model generates a current state model as a function of the dynamic states and the model input, wherein a constraint on the current state model is based on a series of cycle synthesis modules, each member of the series of cycle synthesis modules modeling a component of a cycle of the gas turbine engine and comprising a series of utilities, the utilities based on mathematical abstractions of physical properties associated with the component;
an estimate state module for determining an estimated state of the model based on a prior state model output and the current state model of the open loop model the estimate state module using online linearization and gain calculation to determine estimator gain for determining the estimated state of the model; and
an output object for processing the estimated state of the model to determine the model output.

17. The gas turbine engine of claim 16 , wherein online linearization and gain calculation comprises obtaining partial derivatives based on the current state model.

18. The gas turbine engine of claim 17 , wherein online linearization and gain calculation further comprises constructing a linear system for gain design using the partial derivatives based on the current state model.

19. The gas turbine engine of claim 18 , wherein online linearization and gain calculation further comprises determining the estimator gain based on the linear system for gain design.

20. The gas turbine engine of claim 16 , wherein the estimator gain is used in minimizing error vectors of the current state model.

Assignees

• United Technologies Corp

Inventors

• Karpman Boris
• Meisner Richard P
• Dhingra Manuj

Classifications

• F05D2240/35

  Combustors or associated equipment · CPC title

• G05D7/0629

  characterised by the type of regulator means · CPC title

• F04D29/321

  for axial flow compressors · CPC title

• F04D29/325

  for axial flow fans (blade mountings F04D29/34, blades F04D29/38) · CPC title

• F02C3/04

  having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) · CPC title