Adaptive PID control system for industrial turbines
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G05F-001/67
G05B-015/02
G05B-011/42
G05B-013/02
출원번호
US-0313604
(2014-06-24)
등록번호
US-9507365
(2016-11-29)
발명자
/ 주소
Britt, Tena K.
출원인 / 주소
Woodward, Inc.
대리인 / 주소
Fish & Richardson P.C.
인용정보
피인용 횟수 :
1인용 특허 :
24
초록▼
The subject matter of this specification can be embodied in, among other things, a method that includes providing a process controller configured to perform a control algorithm based on at least one first control parameter, providing a parameter controller configured to perform a parameter adjustmen
The subject matter of this specification can be embodied in, among other things, a method that includes providing a process controller configured to perform a control algorithm based on at least one first control parameter, providing a parameter controller configured to perform a parameter adjustment algorithm, providing a turbine having an output sensor, providing to the process controller at least one first control parameter and a first input value, controlling the turbine based on the at least one first control parameter and the first input value, receiving a turbine response value provided by the turbine output sensor, determining at least one second control parameter based on the turbine response value and the parameter adjustment algorithm, providing, to the process controller from the parameter controller, the at least one second control parameter, and controlling the turbine based on the at the least one second control parameter and a second input value.
대표청구항▼
1. A method for operating a turbine comprising: providing a process controller configured to perform a control algorithm based on at least one first control parameter representing a first value selected from a group comprising a proportional gain (P) value, an integral gain (I) value, and a derivati
1. A method for operating a turbine comprising: providing a process controller configured to perform a control algorithm based on at least one first control parameter representing a first value selected from a group comprising a proportional gain (P) value, an integral gain (I) value, and a derivative gain (D) value, the control algorithm is given by the equation: H (s)=P (1+I/s) (Ds+1), wherein s is the Laplace operator;providing a parameter controller configured to perform a parameter adjustment algorithm;providing a turbine having assembled thereto a turbine output sensor in communication with the process controller and the parameter controller;providing, to the process controller, at least one first control parameter and a first input value;controlling, by the process controller, the turbine based on the at least one first control parameter and the first input value;receiving, by the parameter controller, a turbine response value provided by the turbine output sensor;determining, by the parameter controller, at least one second control parameter based on the turbine response value and the parameter adjustment algorithm, the second control parameter representing a second value selected from the group;providing, to the process controller from the parameter controller, the at least one second control parameter;and controlling, by the process controller, the turbine based on the at the least one second control parameter and a second input value. 2. The method of claim 1, further comprising identifying, by the parameter controller, the turbine response value provided by the turbine output sensor. 3. The method of claim 1, wherein at least one of the first input value and the second input value is a value selected from the group consisting of turbine speed, load, temperature, flow, current, voltage, pressure, and vibration. 4. The method of claim 1, wherein the P value is a function of a relative system gain, a relative system deadtime, and a response speed input parameter. 5. The method of claim 1, wherein at least one of the I value and the D value is a function of a measured system response frequency, a relative system gain, a relative system deadtime, and a response speed input parameter. 6. A method for operating a turbine comprising: receiving, at a parameter controller, a turbine response value, the turbine response value based on an input value and at least one first control parameter representing a first value selected from a group comprising a proportional gain (P) value, an integral gain (I) value, and a derivative gain (D) value;providing a process controller configured to perform a control algorithm based on at least one first control parameter, the control algorithm given by the equation: H(s)=P(1+IS)(Ds+1),wherein s is the Laplace operator;determining, by the parameter controller, at least one second control parameter based on the turbine response value and a parameter adjustment algorithm, the second control parameter representing a second value selected from the group; andproviding, by the parameter controller, the at least one second control parameter. 7. The method of claim 6, further comprising providing the parameter controller configured to perform the parameter adjustment algorithm. 8. The method of claim 6, further comprising providing a turbine having assembled thereto a turbine output sensor configured to provide the turbine response value. 9. The method of claim 6, wherein the at least one first control parameter, the at least one second control parameter, and the input value are PID process controller values. 10. The method of claim 6, wherein the turbine response value comprises one or more turbine output values provided by a turbine output sensor. 11. The method of claim 6, wherein the turbine response value is based on an output response of a turbine under the control of the process controller configured with the at least one first control parameter and the input value. 12. The method of claim 6, further comprising identifying, by the parameter controller, the turbine response value provided by a turbine output sensor. 13. The method of claim 6, wherein the input value is a value selected from the group consisting of turbine speed, load, temperature, flow, current, voltage, pressure, and vibration. 14. The method of claim 6, wherein the P value is a function of a relative system gain, a relative system deadtime, and a response speed input parameter. 15. The method of claim 6, wherein at least one of the I value and the D value is a function of a measured system response frequency, a relative system gain, a relative system deadtime, and a response speed input parameter. 16. A turbine parameter controller comprising: an input;an output;memory storing instructions that are executable; andone or more processing devices to execute the instructions to perform operations comprising:receiving a turbine response value at the input, the turbine response value based on an input value and at least one first control parameter representing a first value selected from a group comprising a proportional gain (P) value, an integral gain (I) value, and a derivative gain (D) value;determining at least one second control parameter based on the turbine response value and a parameter adjustment algorithm, the second control parameter representing a second value selected from the group, wherein the at least one second control parameter is provided to a process controller configured to perform a control algorithm given by the equation: H(s)=P(1+IS)(Ds+1),wherein s is the Laplace operator;providing the at least one second control parameter at the output. 17. The controller of claim 16, wherein the at least one first control parameter, the at least one second control parameter and the input value are PID process controller values. 18. The controller of claim 16, wherein the turbine response value comprises one or more turbine output values provided by a turbine output sensor. 19. The method of claim 16, wherein the turbine response value is based on an output response of a turbine under the control of the process controller configured with the at least one first control parameter and the input value. 20. The controller of claim 16, further comprising identifying the turbine response value provided by a turbine output sensor. 21. The controller of claim 16, wherein the input value is a value selected from the group comprising: turbine speed, load, temperature, flow, current, voltage, pressure, and vibration. 22. The controller of claim 16, wherein the P value is a function of a relative system gain, a relative system deadtime, and a response speed input parameter. 23. The controller of claim 16, wherein at least one of the I value and the D value is a function of a measured system response frequency, a relative system gain, a relative system deadtime, and a response speed input parameter. 24. A turbine system comprising: a process controller configured to perform a control algorithm based on at least one first control parameter representing a first value selected from a group comprising a proportional gain (P) value, an integral gain (I) value, and a derivative gain (D) value, the control algorithm is given by the equation: H(s)=P(1+I/s) (Ds+1), wherein s is the Laplace operator;a parameter controller configured to perform a parameter adjustment algorithm;a turbine having assembled thereto a turbine output sensor in communication with the process controller and the parameter controller;wherein the parameter adjustment algorithm is configured to perform operations comprising: providing, to the process controller, at least one first control parameter and a first input value;controlling, by the process controller, the turbine based on the at least one first control parameter and the first input value;receiving, by the parameter controller, a turbine response value provided by the turbine output sensor;determining, by the parameter controller, at least one second control parameter based on the turbine response value and the parameter adjustment algorithm, the second control parameter representing a second value selected from the group;providing, to the process controller from the parameter controller, the at least one second control parameter; andcontrolling, by the process controller, the turbine based on the at the least one second control parameter and a second input value. 25. The system of claim 24, further comprising identifying, by the parameter controller, the turbine response value provided by the turbine output sensor. 26. The system of claim 24, wherein at least one of the first input value and the second input value is a value selected from the group comprising: turbine speed, load, temperature, flow, current, voltage, pressure, and vibration. 27. The system of claim 24, wherein the P value is a function of a relative system gain, a relative system deadtime, and a response speed input parameter. 28. The system of claim 24, wherein at least one of the I value and the D value is a function of a measured system response frequency, a relative system gain, a relative system deadtime, and a response speed input parameter. 29. A non-transitory computer readable medium storing instructions that, when executed by one or more processors, cause the one or more processors to perform operations comprising: receiving, at a parameter controller, a turbine response value, the turbine response value based on an input value and at least one first control parameter representing a first value selected from a group comprising a proportional gain (P) value, an integral gain (I) value, and a derivative gain (D) value;providing a process controller configured to perform a control algorithm based on at least one first control parameter, the control algorithm given by the equation: H(s)=P(1+IS)(Ds+1),wherein s is the Laplace operator;determining, by the parameter controller, at least one second control parameter based on the turbine response value and a parameter adjustment algorithm, the second control parameter representing a second value selected from the group;and providing, by the parameter controller, the at least one second control parameter. 30. The non-transitory computer readable medium of claim 29, further comprising providing the parameter controller configured to perform the parameter adjustment algorithm. 31. The non-transitory computer readable medium of claim 29, further comprising providing a turbine having assembled thereto a turbine output sensor configured to provide the turbine response value. 32. The non-transitory computer readable medium of claim 29, wherein the at least one first control parameter, the at least one second control parameter, and the input value are PID process controller values. 33. The non-transitory computer readable medium of claim 29, wherein the turbine response value comprises one or more turbine output values provided by a turbine output sensor. 34. The non-transitory computer readable medium of claim 29, wherein the turbine response value is based on an output response of a turbine under the control of the process controller configured with the at least one first control parameter and the input value. 35. The non-transitory computer readable medium of claim 29, further comprising identifying, by the parameter controller, the turbine response value provided by a turbine output sensor. 36. The non-transitory computer readable medium of claim 29, wherein the input value is a value selected from the group consisting of turbine speed, load, temperature, flow, current, voltage, pressure, and vibration. 37. The non-transitory computer readable medium of claim 29, wherein the P value is a function of a relative system gain, a relative system deadtime, and a response speed input parameter. 38. The non-transitory computer readable medium of claim 29, wherein at least one of the I value and the D value is a function of a measured system response frequency, a relative system gain, a relative system deadtime, and a response speed input parameter.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (24)
Lin, Feng; Zaremba, Alexander T; Badreddine, Bader; Sun, Jing, Adaptive PID control method and system for internal combustion engine rotation speed pulsation damping.
Yee, David K.; Corr, II, Robert Anthony; Nickolas, Sarento George, Design and control strategy for catalytic combustion system with a wide operating range.
McCarty William L. (West Chester FL) Wescott Kermit R. (Winter Springs FL), Gas turbine control system having maximum instantaneous load-pickup limiter.
Thatcher, Jonathan Carl; Schaberg, Scott; Disch, Mark, Methods and systems for providing real-time comparison with an alternate control strategy for a turbine.
Smith, Carlos A.; Sanjuan, Marco E., System and method to avoid oscillatory behavior in proportional-integral-derivative (PID) controllers by using fuzzy inference and modified/active damping.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.