CN106527120A - Stability margin configuration method for specified-accuracy PID control system - Google Patents
Stability margin configuration method for specified-accuracy PID control system Download PDFInfo
- Publication number
- CN106527120A CN106527120A CN201611144175.5A CN201611144175A CN106527120A CN 106527120 A CN106527120 A CN 106527120A CN 201611144175 A CN201611144175 A CN 201611144175A CN 106527120 A CN106527120 A CN 106527120A
- Authority
- CN
- China
- Prior art keywords
- omega
- frequency
- margin
- pid
- frequency characteristic
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims abstract description 20
- 235000013399 edible fruits Nutrition 0.000 claims 1
- 238000004458 analytical method Methods 0.000 abstract 1
- 238000012986 modification Methods 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 238000010845 search algorithm Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B11/00—Automatic controllers
- G05B11/01—Automatic controllers electric
- G05B11/36—Automatic controllers electric with provision for obtaining particular characteristics, e.g. proportional, integral, differential
- G05B11/42—Automatic controllers electric with provision for obtaining particular characteristics, e.g. proportional, integral, differential for obtaining a characteristic which is both proportional and time-dependent, e.g. P. I., P. I. D.
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Feedback Control In General (AREA)
Abstract
The present invention discloses a stability margin configuration method for a specified-accuracy PID control system. The method comprises the steps of firstly, establishing a frequency characteristics model of a controlled object; secondly, according to a specified open-loop crossover frequency and a desired amplitude margin, calculating a proportional gain required by a PID controller; thirdly, according to the definition formula of a phase angle margin, searching an open-loop cut-off frequency that meets the desired amplitude margin through the optimizing control algorithm; finally, according to a given formula, calculating the integral gain and the differential gain of the PID controller. Based on above three parameter values of the PID, the specified stability margin of the system is realized. According to the technical scheme of the invention, the difficulty of solving non-linear equations is avoided through the analytic method. Therefore, the PID parameter setting is realized at the specified stability margin.
Description
Technical field
The invention belongs to control method technical field, more particularly to a kind of PID control system with designated precision is stably
Nargin collocation method.
Background technology
As control algolithm is simple, adjustable parameter is few and can meet the performance requirement of most of control systems, so far
The control loop for still having 95% adopts PID controller.Due to PID controller parameter configuration it is whether suitable, it will usually have influence on
The performance of control system, therefore, the parameter tuning problem of PID controller is always the focus of academia and industrial quarters concern.
In numerous setting methods of PID controller, it is broadly divided into that time domain is adjusted and frequency domain is adjusted two classes.Wherein, system stablizes abundant
Degree (including magnitude margin and Phase margin) is an important indicator must being fulfilled in frequency domain setting method.However, due to nothing
Method solves trigonometric function equation, thus system design index is difficult to done with high accuracy.
The content of the invention
In order to meet the design exact requirements of stability margin, the present invention provides one kind and solves cutoff frequency by optimization method
The method for designing of rate:By the solving precision for arranging cut-off frequency, the cutoff frequency of designated precision is obtained using linear search algorithm
Rate, so as to finally calculate three parameters of PID controller.
The technical scheme that the present invention takes is as follows:
A kind of collocation method of the PID control system stability margin with designated precision, comprises the following steps:
S1, sets up the frequency characteristic model of the frequency characteristic model and PID controller of controlled device;
S2, according to specified cross-over frequency ωxWith magnitude margin AmRequire, calculate the proportional gain of PID controller;
S3, based on optimizing algorithm, search meets specifies Phase margin ΦmCut-off frequency ωc;
S4, based on the cut-off frequency ω that the optimizing of step S3 is obtainedc, calculate the storage gain K of PIDiWith differential gain Kd。
Step S1, frequency characteristic G of controlled devicep(j ω) is:
Gp(j ω)=u (ω)+jv (ω) (1)
In formula (1), j is imaginary symbols, and ω is frequency, real parts of the u (ω) for the frequency characteristic of controlled device, and v (ω) is
The imaginary part of the frequency characteristic of controlled device;
The frequency characteristic model of PID controller is:
Gc(j ω)=Kp+X(ω)j (2)
Wherein,For the imaginary part of the frequency characteristic of PID controller, Kp、Ki、KdIt is expressed as PID controls
The proportional gain of device processed, storage gain and the differential gain.
Step S2, it is intended that cross-over frequency be ωx, then meet and specify magnitude margin AmProportional gain by formula (3) count
Calculate:
Wherein u (ωx) for ω=ωxWhen controlled device frequency characteristic real part, v (ωx) for ω=ωxWhen controlled device
The imaginary part of frequency characteristic.
In step S3, it is intended that Phase margin be ΦmMeet nonlinear equation (4):
u(ωc) for ω=ωcWhen controlled device frequency characteristic real part, v (ωc) for ω=ωcWhen controlled device frequency
The imaginary part of characteristic;Wherein X (ωc) computing formula be formula (5):
Solving precision ε is set, and by optimizing algorithm, search meets the cut-off frequency ω of solving precision εc.More preferably, pass through
Two way classification is searching for ωc。
More preferably, the cut-off frequency ω of solving precision ε is met using dichotomizing searchc, comprise the following steps:
S001:The region of search [ω is setL ωR] (ω during initializationL=ωx, ωR=0), interval midpoint is taken for ωc=
0.5(ωL+ωR);
S002:By ωcNonlinear equation (4) is updated to, the value on the right of nonlinear equation (4) is calculated;
S003:Judge the absolute value of difference of the value on nonlinear equation (4) left side and the value on the right whether less than default precision
ε;If less than default precision ε, based on gained ωc, turn to step S4;S004 is performed otherwise;
S004:If value is worth less than the left side on the right of nonlinear equation (4), ω is takenL=ωc;Conversely, ωR=ωc;Return
S001。
The storage gain K of PID controller described in step S4iWith differential gain KdCalculated based on formula (6):
Wherein,Compared with prior art, the present invention's has
Beneficial effect includes:The solution of nonlinear equation is searched for by optimized algorithm, it is to avoid the difficulty of direct solution nonlinear equation, can
Obtain the balance between solving precision and solving complexity, meet the needs of engineering design, can under the conditions of designated precision,
PID control system stability margin configuration is carried out, the configuration required precision of PID control system stability margin is met.
Specific embodiment
PID control system stability margin collocation method with designated precision, takes following steps to calculate pid parameter, can
To obtain desired stability margin (magnitude margin Am and Phase margin Φm):
A kind of collocation method of the PID control system stability margin with designated precision, comprises the following steps:
S1, sets up the frequency characteristic model of the frequency characteristic model and PID controller of controlled device;
S2, according to specified cross-over frequency ωxWith magnitude margin AmRequire, calculate the proportional gain of PID controller;
S3, based on optimizing algorithm, search meets specifies Phase margin ΦmCut-off frequency ωc;
S4, based on the cut-off frequency ω that the optimizing of step S3 is obtainedc, calculate the storage gain K of PIDiWith differential gain Kd。
Step S1, frequency characteristic G of controlled devicep(j ω) is:
Gp(j ω)=u (ω)+jv (ω) (1)
In formula (1), j is imaginary symbols, and ω is frequency, real parts of the u (ω) for the frequency characteristic of controlled device, and v (ω) is
The imaginary part of the frequency characteristic of controlled device;
The frequency characteristic model of PID controller is:
Gc(j ω)=Kp+X(ω)j (2)
Wherein,For the imaginary part of the frequency characteristic of PID controller, Kp、Ki、KdIt is expressed as PID controls
The proportional gain of device processed, storage gain and the differential gain.
Step S2, it is intended that cross-over frequency be ωx, then meet and specify magnitude margin AmProportional gain by formula (3) count
Calculate:
u(ωx) for ω=ωxWhen controlled device frequency characteristic real part, v (ωx) for ω=ωxWhen controlled device frequency
The imaginary part of characteristic.
In step S3, it is intended that Phase margin be ΦmMeet nonlinear equation (4):
u(ωc) for ω=ωcWhen controlled device frequency characteristic real part, v (ωc) for ω=ωcWhen controlled device frequency
The imaginary part of characteristic;Wherein X (ωc) computing formula be formula (5):
Solving precision ε is set, and by optimizing algorithm, search meets the cut-off frequency ω of solving precision εc。
The present embodiment, searches for ω using two way classificationc:
S001:The region of search [ω is setL ωR] (ω during initializationL=ωx, ωR=0), interval midpoint is taken for ωc=
0.5(ωL+ωR);
S002:By ωcIt is updated to nonlinear equation (4), the value on the right of accounting equation (4);
S003:Whether the absolute value of the difference of decisive equation (4) left and right value is less than default precision ε;Turn if condition is met
To S005;S004 is performed otherwise;
S004:If value takes ω less than the left side on the right of equation (4)L=ωc;Conversely, ωR=ωc;Return S001;
S005:Using gained ωc, based on equation below, calculate the storage gain K of the PID controlleriAnd the differential gain
Kd:
In formula,
So, when three parameters of PID controller are arranged according to above-mentioned requirements, the stability margin required by design objective
Required precision can just be met.
Those skilled in the art the present invention can be modified or modification design but without departing from the present invention think of
Think and scope.Therefore, if these modifications of the present invention and modification belong to the technical scope of the claims in the present invention and its equivalent
Within, then the present invention is also intended to comprising these changes and modification.
Claims (6)
1. a kind of collocation method of the PID control system stability margin with designated precision, its feature are comprised the following steps:
S1, sets up the frequency characteristic model of the frequency characteristic model and PID controller of controlled device;
S2, according to specified cross-over frequency ωxWith magnitude margin AmRequire, calculate the proportional gain of PID controller;
S3, based on optimizing algorithm, search meets specifies Phase margin ΦmCut-off frequency ωc;
S4, calculates the storage gain K of PIDiWith differential gain Kd。
2. the PID control system stability margin degree collocation method with designated precision according to claim 1, its feature exist
In:Frequency characteristic G of controlled devicep(j ω) is:
Gp(j ω)=u (ω)+jv (ω) (1)
In formula (1), j is imaginary symbols, and ω is frequency, real parts of the u (ω) for the frequency characteristic of controlled device, and v (ω) is controlled
The imaginary part of the frequency characteristic of object;
The frequency characteristic model of PID controller is:
Gc(j ω)=Kp+X(ω)j (2)
Wherein,For the imaginary part of the frequency characteristic of PID controller, Kp、KiAnd KdIt is expressed as PID controller
Proportional gain, storage gain and the differential gain.
3. the PID control system stability margin collocation method with designated precision according to claim 1, its feature exist
In:
The cross-over frequency specified is ωx, then meet and specify magnitude margin AmProportional gain by formula (3) calculate:
u(ωx) for ω=ωxWhen controlled device frequency characteristic real part, v (ωx) for ω=ωxWhen controlled device frequency characteristic
Imaginary part.
4. the PID control system stability margin collocation method with designated precision according to claim 1, its feature exist
In:
In step S3, it is intended that Phase margin be ΦmMeet nonlinear equation (4):
Wherein X (ωc) computing formula be formula (5):
Solving precision ε is set, and by optimizing algorithm, search meets the cut-off frequency ω of solving precision εc。
5. the PID control system stability margin collocation method with designated precision according to claim 4, its feature exist
In:
The cut-off frequency ω of solving precision ε is met using dichotomizing searchc, comprise the following steps:
S001:The region of search [ω is setL ωR], interval midpoint is taken for ωc=0.5 (ωL+ωR);
S002:By ωcNonlinear equation (4) is updated to, the value on the right of nonlinear equation (4) is calculated;
S003:Judge the absolute value of difference of the value on nonlinear equation (4) left side and the value on the right whether less than default precision ε;Such as
Fruit is less than default precision ε, based on gained ωc, then turn to step S4;S004 is performed otherwise;
S004:If value is worth less than the left side on the right of nonlinear equation (4), ω is takenL=ωc;Conversely, ωR=ωc;Return S001.
6. the PID control system stability margin collocation method with designated precision according to claim 1, its feature exist
In:The storage gain K of PID controller described in step S4iWith differential gain KdCalculated based on formula (6):
Wherein,
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611144175.5A CN106527120A (en) | 2016-12-13 | 2016-12-13 | Stability margin configuration method for specified-accuracy PID control system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611144175.5A CN106527120A (en) | 2016-12-13 | 2016-12-13 | Stability margin configuration method for specified-accuracy PID control system |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106527120A true CN106527120A (en) | 2017-03-22 |
Family
ID=58343185
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201611144175.5A Pending CN106527120A (en) | 2016-12-13 | 2016-12-13 | Stability margin configuration method for specified-accuracy PID control system |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106527120A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110032171A (en) * | 2019-04-23 | 2019-07-19 | 北京航天飞腾装备技术有限责任公司 | One kind being based on cutoff frequency control loop design method |
CN111812967A (en) * | 2020-05-27 | 2020-10-23 | 浙江中控技术股份有限公司 | PID control parameter setting method based on stability margin and dynamic response index |
CN113157503A (en) * | 2021-03-19 | 2021-07-23 | 山东英信计算机技术有限公司 | Heat dissipation debugging method and related device |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108594676A (en) * | 2018-04-04 | 2018-09-28 | 河海大学常州校区 | A kind of industry controlled process characteristic parameter Fast Identification Method |
-
2016
- 2016-12-13 CN CN201611144175.5A patent/CN106527120A/en active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108594676A (en) * | 2018-04-04 | 2018-09-28 | 河海大学常州校区 | A kind of industry controlled process characteristic parameter Fast Identification Method |
Non-Patent Citations (4)
Title |
---|
任丰原 等: "ATM网络拥塞控制中PID控制器的设计", 《计算机学报》 * |
张富强 等: "满足幅值裕度和相角裕度的PID 参数域", 《天津科技大学学报》 * |
王亚刚 等: "基于频域辨识的自整定PID 控制器", 《自动化仪表》 * |
黄静静 等: "《MATLAB与数学实验》", 31 July 2015 * |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110032171A (en) * | 2019-04-23 | 2019-07-19 | 北京航天飞腾装备技术有限责任公司 | One kind being based on cutoff frequency control loop design method |
CN110032171B (en) * | 2019-04-23 | 2020-06-12 | 北京航天飞腾装备技术有限责任公司 | Control loop design method based on cut-off frequency |
CN111812967A (en) * | 2020-05-27 | 2020-10-23 | 浙江中控技术股份有限公司 | PID control parameter setting method based on stability margin and dynamic response index |
CN113157503A (en) * | 2021-03-19 | 2021-07-23 | 山东英信计算机技术有限公司 | Heat dissipation debugging method and related device |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105093931B (en) | A kind of aero-engine Control of Nonlinear Systems device design method | |
WO2020024548A1 (en) | Pid controller design method | |
CN106681150A (en) | Fractional-order PID controller parameter optimizing and setting method based on closed-loop reference model | |
CN106527120A (en) | Stability margin configuration method for specified-accuracy PID control system | |
CN103293956A (en) | Method for setting fractional-order PID (proportion, integration and differentiation) controller for parameter uncertainty system which is controlled object | |
CN105549395B (en) | Ensure the mechanical arm servo-drive system dead time compensation control method of mapping | |
CN108489015B (en) | Air conditioning system temperature control method based on pole allocation and Pade approximation | |
CN104991444B (en) | Non-linearity PID self-adaptation control method based on Nonlinear Tracking Differentiator | |
CN110531612A (en) | A kind of parameter tuning method of Fractional Order PID Controller | |
CN105182741A (en) | Non-overshot fractional order time-varying sliding mode control method | |
CN105159311B (en) | A kind of design method of automatic pilot for strapdown seeker | |
CN103324093A (en) | Multi-model adaptive control system and control method thereof | |
CN109507870A (en) | The fractional order proportional integration or proportional plus derivative controller design method of structure adaptive | |
CN107102555A (en) | A kind of calm one order inertia adds the linear active disturbance rejection controller design method of dead-time system | |
CN108801081B (en) | Nonsingular rolling instruction generation algorithm for BTT missile | |
CN103454921A (en) | Tangent linearization method of flight control system nonlinear tracking controller design | |
CN108170032A (en) | A kind of method for improving piezo-stack type driver positioning accuracy | |
CN106292285B (en) | A kind of fuzzy adapted PI control device parameter determination method | |
CN103809446A (en) | Method for designing flutter-suppression composite frequency robust controller for multi-loop model cluster of aircraft | |
Chowdary et al. | Robust controller design for first order plus time delay systems using kharitonov theorem | |
Nguyen | Adaptive control for linear uncertain systems with unmodeled dynamics revisited via optimal control modification | |
CN112152530A (en) | Model reference adaptive flux linkage identification parameter setting method | |
CN103777523A (en) | Aircraft multi-loop model cluster composite PID (proportion integration differentiation) robust controller design method | |
CN103809442A (en) | Method for designing composite frequency robust controller for multi-loop model cluster of aircraft | |
Lu et al. | Design of a hybrid adaptive CMAC with supervisory controller for a class of nonlinear system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |