CN113972899B - Novel operational amplification compensation circuit for inertial link and control system thereof - Google Patents

Novel operational amplification compensation circuit for inertial link and control system thereof Download PDF

Info

Publication number
CN113972899B
CN113972899B CN202111230810.2A CN202111230810A CN113972899B CN 113972899 B CN113972899 B CN 113972899B CN 202111230810 A CN202111230810 A CN 202111230810A CN 113972899 B CN113972899 B CN 113972899B
Authority
CN
China
Prior art keywords
link
control system
compensation circuit
inertia
inertial
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.)
Active
Application number
CN202111230810.2A
Other languages
Chinese (zh)
Other versions
CN113972899A (en
Inventor
宁宗祺
毛耀
黄永梅
朗朗
陈兴龙
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Institute of Optics and Electronics of CAS
Original Assignee
Institute of Optics and Electronics of CAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Institute of Optics and Electronics of CAS filed Critical Institute of Optics and Electronics of CAS
Priority to CN202111230810.2A priority Critical patent/CN113972899B/en
Publication of CN113972899A publication Critical patent/CN113972899A/en
Application granted granted Critical
Publication of CN113972899B publication Critical patent/CN113972899B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03FAMPLIFIERS
    • H03F3/00Amplifiers with only discharge tubes or only semiconductor devices as amplifying elements
    • H03F3/45Differential amplifiers

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Feedback Control In General (AREA)

Abstract

The invention discloses a novel operational amplification compensation circuit aiming at an inertia link and a control system thereof, and belongs to the field of automatic control. The phase lag caused by the inertia links affects the dynamic response capability of the control system. To compensate for the effects of inertial links, a closed loop control system is conventionally employed. The invention provides a novel operational amplification compensation circuit aiming at an inertia link. The circuit comprises an in-phase amplified proportional integral link A(s) and a negative feedback inertia link B(s), and can compensate phase lag without a sensor and improve the bandwidth of a control system. Since the influence of sensor noise is avoided, a high compensation capability can be obtained by increasing the gain. And the compensation capacity of the amplifier can be freely adjusted by a pair of resistors in the operational amplifier, and the amplifier is simple and convenient to design. Meanwhile, the circuit can be realized through a small amount of operational amplifiers, and the cost is extremely low.

Description

Novel operational amplification compensation circuit for inertial link and control system thereof
Technical Field
The invention belongs to the field of automatic control, and particularly relates to a novel operational amplification compensation circuit aiming at an inertia link and a control system thereof.
Background
Inertial links are common in control systems. For example, an inertia link of a current response due to an equivalent resistance of the inductive motor and an armature inductance, an inertia link due to various mechanical structures, and the like. For control systems, inertia loops can cause phase lag and affect control bandwidth. Therefore, to improve the dynamic response capability of the system, it is important to compensate for the dynamic response capability.
Conventional compensation methods are typically based on closed loop control systems. And feeding back the sensor signal to the control unit for closed loop correction. However, factors such as noise from the sensor can limit the bandwidth of the closed loop control system, thereby preventing further improvement in the dynamic response capability of the system. At the same time, the use of sensors also adds undoubtedly to the cost and complexity of the system.
Aiming at the situation, the invention provides a novel operational amplification compensation circuit aiming at an inertia link. Aiming at phase lag caused by inertia links, the circuit can compensate the phase lag without a sensor and improve the bandwidth of a control system. Since the influence of sensor noise is avoided, a high compensation capability can be obtained by increasing the gain. And the compensation capacity of the amplifier can be freely adjusted by a pair of resistors in the operational amplifier, and the amplifier is simple and convenient to design. Meanwhile, the circuit can be realized by using an operational amplifier of the AD8676, and the cost is extremely low.
Disclosure of Invention
The invention aims at: and the operational amplifier compensates an inertia link in the control system on the basis of no need of a sensor, so that the dynamic response capability of the system is improved.
The invention adopts the technical scheme that:
the novel operational amplification compensation circuit for the inertia link comprises an in-phase amplification proportional integral link A(s) and a negative feedback inertia link B(s), wherein the compensation circuit is connected in series before an inertia hysteresis link of a controlled object so as to compensate the inertia hysteresis;
the gain of the negative feedback inertial link B(s) of the compensation circuit is 1, and the time constant is the same as the phase lag of the controlled object, namely:
Figure BDA0003315864280000021
the gain of the proportional-integral link A(s) is designed to be K, and the time constant of the gain is the same as the phase lag of the controlled object, namely:
Figure BDA0003315864280000022
wherein τ 0 A phase constant representing the inertial hysteresis of the controlled object;
the proportional-integral link A(s) comprises an operational amplifierAmplifier, a first resistor R 1 A second resistor R 2 And a capacitance C;
the negative feedback inertia link B(s) comprises an operational amplifier, two second resistors R 2 And a capacitance C;
when R is 2 =NR 1 In this case, the phase lag of the system can be reduced to 1/N.
The invention also provides the following technical scheme:
the control system comprises the novel operational amplification compensation circuit aiming at the inertia link, wherein the compensation circuit is connected in series before the inertia hysteresis link of a controlled object in the control system, so that the inertia hysteresis is compensated;
after the compensation, the final response characteristics of the control system are as follows:
Figure BDA0003315864280000023
wherein τ' 0 =1/K, r(s) and y(s) represent an input control signal and an output response signal of the system, respectively; when 1/K is less than tau 0 When the method is used, the phase lag can be reduced, and the response bandwidth of the system is improved;
wherein,,
τ 0 =R 2 C (3)
τ′ 0 =R 1 C (4)。
according to the technical scheme, 1/K is 1/K 0 The phase lag can be greatly reduced, and the response bandwidth of the system can be improved; and due to tau 0 =R 2 C,τ′ 0 =R 1 C, thus, when R 2 =NR 1 When the phase delay of the system is reduced to 1/N of the original phase delay, the circuit design can be effectively supplemented with the phase delay generated by an inertia link, and the circuit is very concise.
Compared with the prior art, the invention has the following advantages:
(1) No sensor is needed, so that the influence of noise on the compensation circuit is avoided;
(2) The design is simple and convenient, and the compensation effect can be controlled by adjusting a group of gains;
(3) The design cost is low, and the compensation of inertial hysteresis is realized through a small number of operational amplifiers.
Drawings
FIG. 1 is a block diagram of a novel operational amplifier compensation circuit for inertial links according to the present invention;
FIG. 2 is a schematic diagram of experimental verification;
FIG. 3 shows the effect of the present invention on inertial member compensation at different values of N.
Detailed Description
The invention is further described below with reference to the drawings and detailed description.
FIG. 1 is a block diagram showing a novel operational amplification compensation circuit for inertial links, the novel operational amplification compensation circuit comprises a proportional-integral link A(s) with in-phase amplification and a negative feedback inertial link B(s), and the compensation circuit is connected in series before an inertial hysteresis link of a controlled object so as to compensate the inertial hysteresis;
the gain of the negative feedback inertial link B(s) of the compensation circuit is 1, and the time constant is the same as the phase lag of the controlled object, namely:
Figure BDA0003315864280000031
the gain of the proportional-integral link A(s) is designed to be K, and the time constant of the gain is the same as the phase lag of the controlled object, namely:
Figure BDA0003315864280000032
wherein τ 0 A phase constant representing the inertial hysteresis of the controlled object;
the proportional-integral link A(s) comprises an operational amplifier, a first resistor R 1 A second resistor R 2 And a capacitance C;
the negative feedback inertial link B(s) comprises an operational amplifierAmplifier, two second resistors R 2 And a capacitance C;
when R is 2 =NR 1 In this case, the phase lag of the system can be reduced to 1/N.
The invention also provides a control system comprising the novel operational amplification compensation circuit, wherein the compensation circuit is connected in series before an inertia hysteresis link of a controlled object in the control system, so that the inertia hysteresis is compensated;
after the compensation, the final response characteristics of the control system are as follows:
Figure BDA0003315864280000033
wherein τ' 0 =1/K, r(s) and y(s) represent an input control signal and an output response signal of the system, respectively; s is the Laplace operator; when 1/K is less than tau 0 When the method is used, the phase lag can be reduced, and the response bandwidth of the system is improved;
wherein,,
τ 0 =R 2 C (3)
τ′ 0 =R 1 C (4)
the design principle, process and effect of the novel operational amplification compensation circuit aiming at the inertia link are described as follows:
step 1: determining the time constant tau of an inertial link existing in the system by means of sweep frequency or manual parameter checking and the like 0
Step 2: a compensation circuit is built according to fig. 1 and connected in series to the control circuit.
Step 3: determining the resistance R according to equation (3) 2 And parameters of capacitance C.
Step 4: the desired compensation effect is determined. If the control bandwidth is increased by N times and the phase lag is reduced to 1/N, R is reduced 2 =NR 1
In order to verify the effect of the invention, a set of direct current torque motor control system is built. The invention is composed of a controller, a compensation circuit, a motor driver, a current sensor and a working computer. The dynamic response characteristic of the current is calculated by calculating the ratio of the signal sent by the controller and the feedback signal of the current sensor in the working computer. By means of the system, the current dynamic response characteristics of the motor are compared without using a compensation circuit and without using the compensation circuit, so that the effectiveness of the invention is demonstrated.
When the compensation circuit is not used, the current dynamic response characteristic of the motor is shown as a solid line in fig. 3. It can be seen that the current characteristic of the armature acts as an inertia link due to the armature inductance and the equivalent resistance, and the response bandwidth is about 99Hz. N is respectively taken as N by adjusting the resistor R1 1 =5,N 2 =10. As can be seen from the two dashed lines in FIG. 3, when N 1 At=5, the response bandwidth of the current is increased by about 5 times. And when N 2 At 10, the response bandwidth is improved by about 10 times, where the error source of the bandwidth is mainly the sampling lag of the controller. In conclusion, the experimental results are consistent with theoretical analysis, and the effectiveness of the invention is proved.
The foregoing is merely a specific embodiment of the present invention, but the scope of the present invention is not limited thereto, and these examples are for illustrative purposes only and are not intended to limit the scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof. Various alternatives and modifications can be made by those skilled in the art without departing from the scope of the invention, and such alternatives and modifications are intended to fall within the scope of the invention.

Claims (2)

1. A novel operational amplification compensation circuit for inertial links is characterized in that,
the compensation circuit comprises an in-phase amplified proportional integral link A(s) and a negative feedback inertia link B(s), and is connected in series before an inertia hysteresis link of a controlled object so as to compensate the inertia hysteresis;
the gain of the negative feedback inertial link B(s) of the compensation circuit is 1, and the time constant is the same as the phase lag of the controlled object, namely:
Figure FDA0003315864270000011
the gain of the proportional-integral link A(s) is designed to be K, and the time constant of the gain is the same as the phase lag of the controlled object, namely:
Figure FDA0003315864270000012
wherein τ 0 A phase constant representing the inertial hysteresis of the controlled object;
the proportional-integral link A(s) comprises an operational amplifier, a first resistor R 1 A second resistor R 2 And a capacitance C;
the negative feedback inertia link B(s) comprises an operational amplifier, two second resistors R 2 And a capacitance C;
when R is 2 =NR 1 In this case, the phase lag of the system can be reduced to 1/N.
2. A control system comprising a novel operational amplification compensation circuit for an inertial link according to claim 1, wherein the compensation circuit is connected in series before an inertial hysteresis link of a controlled object in the control system, thereby compensating for the inertial hysteresis;
after the compensation, the final response characteristics of the control system are as follows:
Figure FDA0003315864270000013
wherein τ' 0 =1/K, r(s) and y(s) represent an input control signal and an output response signal of the system, respectively; when 1/K is less than tau 0 When the method is used, the phase lag can be reduced, and the response bandwidth of the system is improved;
wherein,,
τ 0 =R 2 C (3)
τ 0 ′=R 1 C (4)。
CN202111230810.2A 2021-10-22 2021-10-22 Novel operational amplification compensation circuit for inertial link and control system thereof Active CN113972899B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202111230810.2A CN113972899B (en) 2021-10-22 2021-10-22 Novel operational amplification compensation circuit for inertial link and control system thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202111230810.2A CN113972899B (en) 2021-10-22 2021-10-22 Novel operational amplification compensation circuit for inertial link and control system thereof

Publications (2)

Publication Number Publication Date
CN113972899A CN113972899A (en) 2022-01-25
CN113972899B true CN113972899B (en) 2023-06-30

Family

ID=79587790

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202111230810.2A Active CN113972899B (en) 2021-10-22 2021-10-22 Novel operational amplification compensation circuit for inertial link and control system thereof

Country Status (1)

Country Link
CN (1) CN113972899B (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05301576A (en) * 1992-04-27 1993-11-16 Mitsubishi Electric Corp Electric-driven power steering control device
JP2003011831A (en) * 2001-06-28 2003-01-15 Nsk Ltd Controller for electric power steering device
CN201168594Y (en) * 2008-01-16 2008-12-24 桂林电子科技大学 Six-side top superhard material hydraulic press power adjust control system
JP2009166715A (en) * 2008-01-17 2009-07-30 Nsk Ltd Electric power steering device
CN104111664A (en) * 2014-07-18 2014-10-22 零八一电子集团有限公司 Method for overcoming motor dead zone and improving radar tracking precision in speed ring
CN110034568A (en) * 2019-05-14 2019-07-19 江苏师范大学 A kind of control method of railway power regulator
CN112433471A (en) * 2020-11-24 2021-03-02 北京麦格纳材科技有限公司 High-precision self-gain compensation control method and control circuit thereof

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05301576A (en) * 1992-04-27 1993-11-16 Mitsubishi Electric Corp Electric-driven power steering control device
JP2003011831A (en) * 2001-06-28 2003-01-15 Nsk Ltd Controller for electric power steering device
CN201168594Y (en) * 2008-01-16 2008-12-24 桂林电子科技大学 Six-side top superhard material hydraulic press power adjust control system
JP2009166715A (en) * 2008-01-17 2009-07-30 Nsk Ltd Electric power steering device
CN104111664A (en) * 2014-07-18 2014-10-22 零八一电子集团有限公司 Method for overcoming motor dead zone and improving radar tracking precision in speed ring
CN110034568A (en) * 2019-05-14 2019-07-19 江苏师范大学 A kind of control method of railway power regulator
CN112433471A (en) * 2020-11-24 2021-03-02 北京麦格纳材科技有限公司 High-precision self-gain compensation control method and control circuit thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
基于PID算法的塑料挤出机温度控制***研究;李月英;齐仁龙;;合成树脂及塑料(第06期);62-65 *

Also Published As

Publication number Publication date
CN113972899A (en) 2022-01-25

Similar Documents

Publication Publication Date Title
US7051058B2 (en) Method and device for filtering a signal
EP2105810A2 (en) Apparatus and method for controlling a system
US20160344326A1 (en) Motor control device
JPH06197578A (en) Parameter identifier
US5853064A (en) Steering system for a motor vehicle
CN113972899B (en) Novel operational amplification compensation circuit for inertial link and control system thereof
JP6364832B2 (en) Vibration suppression control device for vehicle
CN113428219A (en) System and method for controlling automobile safety based on transfer function quick response
EP3784895B1 (en) Speed control method for an internal combustion engine
EP1457846B1 (en) Improving stability and response of control systems
JP4982905B2 (en) Control method and control apparatus
KR102568747B1 (en) test system
CN113364391B (en) Motor control system and vibration suppression method thereof
CN113949318B (en) Novel inductive motor counter potential compensation circuit based on operational amplifier
JP2005223960A (en) Controller of motor
JP4151401B2 (en) Servo control device
CN115629536B (en) PID controller parameter setting method suitable for first-order time lag integral system
RU193236U1 (en) Self-adjusting speed control system
CN115016250B (en) Servo speed control method of improved anti-saturation structure
JP4420158B2 (en) Motor speed control device
KR102056740B1 (en) Gear actuator control method and apparatus
CN108254147A (en) Shake table feedback signal frequency-division section amplitude modulation system
JP2885544B2 (en) Dead time compensation controller
CN112558462A (en) Active series correction circuit and method thereof
JPH0527804A (en) Optimum process controller

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant