CN104090490A - Input shaper closed-loop control method based on chaotic particle swarm optimization algorithm - Google Patents

Input shaper closed-loop control method based on chaotic particle swarm optimization algorithm Download PDF

Info

Publication number
CN104090490A
CN104090490A CN201410317759.2A CN201410317759A CN104090490A CN 104090490 A CN104090490 A CN 104090490A CN 201410317759 A CN201410317759 A CN 201410317759A CN 104090490 A CN104090490 A CN 104090490A
Authority
CN
China
Prior art keywords
particle
chaos
input shaper
swarm optimization
optimization algorithm
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.)
Granted
Application number
CN201410317759.2A
Other languages
Chinese (zh)
Other versions
CN104090490B (en
Inventor
蔡力钢
许博
刘志峰
张森
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.)
Beijing University of Technology
Original Assignee
Beijing University of Technology
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 Beijing University of Technology filed Critical Beijing University of Technology
Priority to CN201410317759.2A priority Critical patent/CN104090490B/en
Publication of CN104090490A publication Critical patent/CN104090490A/en
Application granted granted Critical
Publication of CN104090490B publication Critical patent/CN104090490B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The invention relates to an input shaper closed-loop control method based on a chaotic particle swarm optimization algorithm and belongs to the technical field of methods for drive control in the coaxial transmission machine start process. In order to solve the buffeting problem in the coaxial transmission machine start process, closed-loop control is performed on a transmission mechanism with the control method, and the effectiveness and the feasibility of the control method are proved by experimental results. In an offline state, a double-pulse input shaper is optimized through the chaotic particle swarm optimization algorithm, optimization parameters of the double-pulse input shaper are obtained, and then a PD closed-loop actuating mechanism is controlled through the optimized input shaper. The input shaper parameter self-tuning control algorithm based on chaotic particle swarm optimization is provided for solving the buffeting problem in the coaxial transmission printing machine start process. Due to the control, a system can respond fast without vibration while torsional vibration of the system is substantially suppressed.

Description

A kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm
Technical field
The present invention relates to a kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm, belong to the driving control method technical field of coaxial gearing start-up course.
Background technology
Coaxial transmission printer is in start-up course, owing to adopting major axis to connect, between axle and axle, transmission range is long, system stiffness is low, load quality can twist vibration when heavily etc. the impact of factors has caused startup, phenomenon of torsional vibration has not only affected the stable state time of start-up course, and also can bring very large impact to transmission shaft, thereby affect the serviceable life of printing machine.
For above reason, adopted the method for input shaper to carry out time-domain filtering to system, yet zero traditional vibration input shaper need Accurate Model, between parameter, influences each other, the difficulty of adjusting.The present invention introduces Chaos particle swarm optimization algorithm controller parameter is optimized, and by system process is passed to letter, converts, realized system signal online acquisition, offline optimization, kept compared with highland precision simultaneously.
Summary of the invention
The object of the present invention is to provide a kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm, for coaxial gearing start-up course, there is buffeting problem, the control method that the present invention proposes is carried out PD control to gear train, and through the results show validity and the feasibility of this control method.
For achieving the above object, the technical solution adopted in the present invention is a kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm, under the state of off-line, use Chaos particle swarm optimization algorithm to be optimized the input shaper of dipulse, obtain its optimized parameter, then use the optimum input shaper obtaining to PD actuating mechanism controls, the method comprises following concrete steps
S1 moves with simple PD parameter adjustment actuating mechanism, remains unchanged later, and system input speed signal x (t), driving device system motion, uses scrambler to collect its rate curve v (t) and final stabilized speed u from system output shaft;
S2, according to the stabilized speed u of system output shaft, adopts Chaos particle swarm optimization algorithm to obtain the parameter of dipulse input shaper, and the frequency-domain expression of dipulse input shaper is a wherein iand t ibe respectively amplitude and the corresponding time lag thereof of pulse train, by time optimal, can make t 1=0, must formula be: for making system output reach stabilized speed u, add equation of constraint A 1+ A 2=1, A i> 0;
The process of described Chaos particle swarm optimization algorithm is as follows,
S2.1 initialization also arranges input shaper correlation parameter; Comprise A 1, A 2and t 2span, due to A 1+ A 2=1, A i> 0, therefore A 2span [0~1], A 1=1-A 2; t 2choose important because excessive t 2span can make Chaos particle swarm optimization algorithm precocious, be absorbed in local minimum, yet can miss optimum solution when too small span is optimized, first according to the model of system, carry out the delay time of estimating signal, the time delay of many matter rotatable platform is less, therefore given t 2span be [0~5].
Chaos-Particle Swarm Optimization correlation parameter is set; Comprise and determine population scale m=30, particle search space dimensionality D=2 (is A 2, t 2two particles), iterations k is 30 to the maximum, and the maximum step number n of Chaos Search is 10, search volume scope x i k ∈ [ x min , x max ] ( x min = [ 0,0 ] , x max = [ 1,5 ] , According to A 2, t 2scope is determined), study factor c 1=c 2=2, inertia weight scope w min=0.6, i particle personal best particle is wherein for all in optimum (being global optimum), the position of each particle of random initializtion and speed;
S2.2 successively as input shaper parameter, carries out emulation to gathering the speed curve movement of returning using the position vector of each particle successively, obtains simulation curve; According to simulation curve, calculate the fitness value of each particle, and using it as the foundation of weighing particle position quality; Fitness function is set is
min J = ∫ 0 ∞ | v ( t ) - u | dt + ftr
In formula, the instantaneous velocity that v (t) is simulation curve, u is the final stabilized speed of system output shaft, and ftr is a larger penalty value, and specific definition is
ftr = k t false t r true
Wherein, t rfor the simulation curve rise time, when not reaching the rise time within the appointment emulation cycle, ftr is a larger penalty value; When the time reaches the rise time, ftr value is t r;
S2.3 calculates the fitness value of each particle according to fitness function, if the fitness value of this particle is less than particle self fitness value in the past, by the current location of this particle, replace if this particle fitness value is less than the fitness value before population, with the position of this particle, replace
S2.4 upgrades the speed of each particle and position, the k time circulation time, and now i particle position vector is x i k = ( x i 1 k , x i 2 k . . . , x iD k ) , Flying speed is v i k = ( v i 1 k , v i 2 k , . . . v iD k ) , Current particle personal best particle is p id k = ( p i 1 k , p i 2 k , . . . , p id k , . . . p iD k ) , Current global optimum position is p gd k = ( p g 1 k , p g 2 k , . . . , p gd k , . . . p gD k ) (d=1,2..., D), the k+1 time circulation time, i particle rapidity iterative equation is v id k + 1 = wv id k + c 1 r 1 ( p id k - x id k ) + c 2 r 2 ( p gd k - x id k ) , Position vector iterative equation x id k + 1 = x id k + v id k + 1 .
S2.5 calculates the fitness value of each particulate, retains 20% best best particle in colony;
S2.6 carries out chaos Local Search to best particle, and upgrades with
The process of described chaos local search algorithm is as follows,
S2.6.1 loop initialization n=0, d=1;
S2.6.2 uses i particle position vector d dimension variable, obtain according to the following formula Chaos Variable d=1,2 ... D, wherein x max, dand x min, dit is the search bound of d dimension variable;
S2.6.3 calculates the Chaos Variable of lower step iteration d=1,2,3...D;
S2.6.4 is according to Chaos Variable obtain position vector if d=D, turns S2.6.5, otherwise d=d+1 turns S2.6.2;
S2.6.5 is according to new position vector obtain fitness value, compare with original position vector, if fitness value is better or Chaos Search has reached greatest iteration step number, using reposition vector as Chaos Search result, otherwise put k=k+1, turn S2.6.2.
S2.7, when k reaches after the iterations of setting, finishes rolling optimization process, output parameter optimal value.Otherwise, forward step S2.8 to.
S2.8 shrinks region of search by formula below to each space variable of vector:
x min,d=max{x min,d,x g,d-r*(x max,d-x min,d)}
x max,d=min{x man,j,x g,d-r*(x max,d-x min,d)}
X wherein g, drepresent current the value of d dimension variable, r is the random number of [0,1];
S2.9, when k reaches after the iterations of setting, finishes rolling optimization process, output parameter optimal value; Otherwise in the space after contraction, random remaining 80% the particulate that produces in colony, turns S2.2;
S3 uses the optimum reshaper obtaining to carry out PD control to topworks.
Compared with prior art, beneficial effect of the present invention is: the present invention is directed to the Torsional Vibration in coaxial transmission printer tool start-up course, proposed a kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm.When being controlled at the torsional oscillation that has significantly suppressed system, this realizes the quick without vibration response of system.
Accompanying drawing explanation
Fig. 1 is this control method application system structured flowchart.
Fig. 2 is chaotic particle swarm optimization procedure chart.
Fig. 3 is the Optimized model figure under simulink.
Fig. 4 a is original PD system start up curve figure.
Fig. 4 b is original PD system start up curve Fourier transform figure.
Fig. 5 a is the PD system start up curve figure of tape input reshaper.
Fig. 5 b is the PD system start up curve Fourier transform figure of tape input reshaper.
Embodiment
The present invention is a kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm, with reference to Fig. 1, after input signal enters mechanical system in online situation, gather output shaft speed curve movement, according to collection application of curve Chaos particle swarm optimization algorithm offline optimization, go out again the parameter of input shaper, then the input shaper of optimization is controlled to PD mechanical system motion, the frequency that can filter like this resonance of enabling signal Zhong Yu topworks, the system that realized when significantly having suppressed Torsional vibration is fast without vibration response.
As shown in Figure 2, the bridge linking between Chaos particle swarm optimization algorithm and simulink model is that particle (is the A in input shaper formula to the optimization method of Chaos-Particle Swarm Optimization off-line 2, t 2).Optimizing process is as follows, produces at random population, by the particle in this population successively assignment to the parameter A in simulink mode input reshaper 2, t 2, the simulink model of operation control system then, obtains the fitness value of this particle, finally judges whether to exit algorithm, if do not exit, the speed of particle and position is upgraded, to A 2, t 2upgrade.
Fig. 3 is the Optimized model figure under simulink, and the rate signal of collection obtains simulation curve after input shaper module, then obtains fitness value through fitness function module.
Fig. 4 a is primal system start up curve figure, is the response that multimass PD closed loop rotation system is inputted the step signal that amplitude is 8600, and system oscillation exists always, and overshoot is about 13.953%; Fig. 4 b is original PD system start up curve Fourier transform figure, can obviously find out and have a low frequency vibration point.
Fig. 5 a is the PD system start up curve figure of tape input reshaper, and under the step signal excitation of same amplitude, the overshoot of system is only 3.488%, and vibration is inhibited, and the adjustment time is only 700ms; Fig. 5 b is the PD system start up curve Fourier transform figure of tape input reshaper, finds out low frequency vibration point elimination.

Claims (3)

1. the input shaper closed loop control method based on Chaos particle swarm optimization algorithm, it is characterized in that: under the state of off-line, use particle swarm optimization algorithm to be optimized the input shaper of dipulse, obtain its optimized parameter, then use the optimum input shaper obtaining to PD actuating mechanism controls, the method comprises following concrete steps
S1 moves with simple PD parameter adjustment actuating mechanism, remains unchanged later, and system input speed signal x (t), driving device system motion, uses scrambler to collect its rate curve v (t) and final stabilized speed u from system output shaft;
S2, according to the stabilized speed u of system output shaft, adopts Chaos particle swarm optimization algorithm to obtain the parameter of dipulse input shaper, and the frequency-domain expression of dipulse input shaper is a wherein iand t ibe respectively amplitude and the corresponding time lag thereof of pulse train, by time optimal, can make t 1=0, must formula be: for making system output reach stabilized speed u, add equation of constraint A 1+ A 2=1, A i> 0;
The process of described Chaos particle swarm optimization algorithm is as follows,
S2.1 initialization also arranges input shaper correlation parameter; Comprise A 1, A 2and t 2span, due to A 1+ A 2=1, A i> 0, therefore A 2span [0~1], A 1=1-A 2; t 2choose important because excessive t 2span can make particle cluster algorithm precocious, be absorbed in local minimum, yet can miss optimum solution when too small span is optimized, first according to the model of system, carry out the delay time of estimating signal, the time delay of many matter rotatable platform is less, therefore given t 2span be [0~5];
Population correlation parameter is set; The scale that comprises definite population is counted m=30, particle search space dimensionality D=2, i.e. A 2, t 2two particles, iterations k is 30 to the maximum, search volume scope study factor c 1=c 2=2, inertia weight scope w min=0.6, i particle personal best particle is wherein for all in optimum, the position of each particle of random initializtion and speed;
S2.2 successively as input shaper parameter, carries out emulation to gathering the speed curve movement of returning using the position vector of each particle successively, obtains simulation curve; According to simulation curve, calculate the fitness value of each particle, and using it as the foundation of weighing particle position quality; Fitness function is set is
min J = ∫ 0 ∞ | v ( t ) - u | dt + ftr
In formula, the instantaneous velocity that v (t) is simulation curve, u is the final stabilized speed of system output shaft, and ftr is a larger penalty value, and specific definition is
ftr = k t false t r true
Wherein, t rfor the simulation curve rise time, when not reaching the rise time within the appointment emulation cycle, ftr is a larger penalty value; When the time reaches the rise time, ftr value is t r;
S2.3 calculates the fitness value of each particle according to fitness function, if the fitness value of this particle is less than particle self fitness value in the past, by the current location of this particle, replace if this particle fitness value is less than the fitness value before population, with the position of this particle, replace
S2.4 upgrades the speed of each particle and position, the k time circulation time, and now i particle position vector is x i k = ( x i 1 k , x i 2 k . . . , x iD k ) , Flying speed is v i k = ( v i 1 k , v i 2 k , . . . v iD k ) , Current particle personal best particle is p id k = ( p i 1 k , p i 2 k , . . . , p id k , . . . p iD k ) , Current global optimum position is p gd k = ( p g 1 k , p g 2 k , . . . , p gd k , . . . p gD k ) (d=1,2..., D), the k+1 time circulation time, i particle rapidity iterative equation is v id k + 1 = wv id k + c 1 r 1 ( p id k - x id k ) + c 2 r 2 ( p gd k - x id k ) , Position vector iterative equation x id k + 1 = x id k + v id k + 1 ;
S2.5 calculates the fitness value of each particulate, retains 20% best best particle in colony;
S2.6 carries out chaos Local Search to best particle, and upgrades with
The process of described chaos local search algorithm is as follows,
S2.6.1 loop initialization n=0, d=1;
S2.6.2 uses i particle position vector d dimension variable, obtain according to the following formula Chaos Variable d=1,2 ... D, wherein x max, dand x min, dit is the search bound of d dimension variable;
S2.6.3 calculates the Chaos Variable of lower step iteration d=1,2,3...D;
S2.6.4 is according to Chaos Variable obtain position vector if d=D, turns S2.6.5, otherwise d=d+1 turns S2.6.2;
S2.6.5 is according to new position vector obtain fitness value, compare with original position vector, if fitness value is better or Chaos Search has reached greatest iteration step number, using reposition vector as Chaos Search result, otherwise put k=k+1, turn S2.6.2;
S2.7, when k reaches after the iterations of setting, finishes rolling optimization process, output parameter optimal value; Otherwise, forward step S2.8 to;
S2.8 shrinks region of search by formula below to each space variable of vector:
x min,d=max{x min,d,x g,d-r*(x max,d-x min,d)},0<r<1
x max,d=min{x man,j,x g,d-r*(x max,d-x min,d)},0<r<1
X wherein g, d, represent current the value of d dimension variable;
S2.9, when k reaches after the iterations of setting, finishes rolling optimization process, output parameter optimal value; Otherwise in the space after contraction, random remaining 80% the particulate that produces in colony, turns S2.2;
S3 uses the optimum reshaper obtaining to carry out PD control to topworks.
2. a kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm according to claim 1, is characterized in that: described in for all in optimum be global optimum.
3. a kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm according to claim 1, is characterized in that: described search volume scope x min=[0,0], x max=[1,5], according to A 2, t 2scope is determined.
CN201410317759.2A 2014-07-04 2014-07-04 A kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm Active CN104090490B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410317759.2A CN104090490B (en) 2014-07-04 2014-07-04 A kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410317759.2A CN104090490B (en) 2014-07-04 2014-07-04 A kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm

Publications (2)

Publication Number Publication Date
CN104090490A true CN104090490A (en) 2014-10-08
CN104090490B CN104090490B (en) 2018-11-02

Family

ID=51638212

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410317759.2A Active CN104090490B (en) 2014-07-04 2014-07-04 A kind of input shaper closed loop control method based on Chaos particle swarm optimization algorithm

Country Status (1)

Country Link
CN (1) CN104090490B (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105447589A (en) * 2015-10-15 2016-03-30 国家电网公司 Control method and apparatus for reducing NOx emission load of coal-fired unit
CN106597851A (en) * 2016-12-15 2017-04-26 南京航空航天大学 Robust fault-tolerant control method for small unmanned aerial vehicle flight control system
CN106647283A (en) * 2017-01-23 2017-05-10 无锡信捷电气股份有限公司 Auto-disturbance rejection position servo system optimization design method based on improved CPSO
CN106816877A (en) * 2017-03-10 2017-06-09 国网江苏省电力公司常州供电公司 A kind of distribution network voltage containing photovoltaic falls detection compensation method
CN106950831A (en) * 2017-03-06 2017-07-14 湖北工业大学 A kind of reactive-load compensation method for offline optimization/switch online
CN107729706A (en) * 2017-11-29 2018-02-23 湖南科技大学 A kind of kinetic model construction method of Nonlinear Mechanical Systems
CN107944594A (en) * 2017-09-30 2018-04-20 华南理工大学 One kind is based on SPSS and RKELM microgrid short-term load forecasting methods
CN108919652A (en) * 2018-10-10 2018-11-30 北京工商大学 A kind of adaptive anti-interference reforming control method and system
CN109117751A (en) * 2018-07-24 2019-01-01 南京信息工程大学 Random resonant weak signal detection method based on adaptive Chaos particle swarm optimization algorithm
CN110109350A (en) * 2019-03-29 2019-08-09 广东工业大学 A kind of power capture optimization method of wave-power device that catching flame algorithm based on chaos moth
CN111123705A (en) * 2019-12-18 2020-05-08 南京航空航天大学 Design method for active vibration control of propeller and transmission shaft system

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6505085B1 (en) * 1999-03-04 2003-01-07 Massachusetts Institute Of Technology Method and apparatus for creating time-optimal commands for linear systems
CN101816822A (en) * 2010-05-27 2010-09-01 天津大学 Setting method of functional electrical stimulation PID (Proportion Integration Differentiation) parameter double source characteristic fusion particle swarm
CN101980470B (en) * 2010-10-03 2013-12-04 鲁东大学 Chaotic particle swarm optimization-based OFDM system resource allocation algorithm
CN103885338A (en) * 2014-03-21 2014-06-25 北京工业大学 Input reshaper parameter self-tuning control method based on particle swarm optimization algorithm

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6505085B1 (en) * 1999-03-04 2003-01-07 Massachusetts Institute Of Technology Method and apparatus for creating time-optimal commands for linear systems
CN101816822A (en) * 2010-05-27 2010-09-01 天津大学 Setting method of functional electrical stimulation PID (Proportion Integration Differentiation) parameter double source characteristic fusion particle swarm
CN101980470B (en) * 2010-10-03 2013-12-04 鲁东大学 Chaotic particle swarm optimization-based OFDM system resource allocation algorithm
CN103885338A (en) * 2014-03-21 2014-06-25 北京工业大学 Input reshaper parameter self-tuning control method based on particle swarm optimization algorithm

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105447589B (en) * 2015-10-15 2019-07-23 国家电网公司 A kind of control method and device lowering coal unit NOx discharge
CN105447589A (en) * 2015-10-15 2016-03-30 国家电网公司 Control method and apparatus for reducing NOx emission load of coal-fired unit
CN106597851A (en) * 2016-12-15 2017-04-26 南京航空航天大学 Robust fault-tolerant control method for small unmanned aerial vehicle flight control system
CN106597851B (en) * 2016-12-15 2019-04-30 南京航空航天大学 A kind of robust Fault-Tolerant Control method of small drone flight control system
CN106647283A (en) * 2017-01-23 2017-05-10 无锡信捷电气股份有限公司 Auto-disturbance rejection position servo system optimization design method based on improved CPSO
CN106950831A (en) * 2017-03-06 2017-07-14 湖北工业大学 A kind of reactive-load compensation method for offline optimization/switch online
CN106816877A (en) * 2017-03-10 2017-06-09 国网江苏省电力公司常州供电公司 A kind of distribution network voltage containing photovoltaic falls detection compensation method
CN107944594A (en) * 2017-09-30 2018-04-20 华南理工大学 One kind is based on SPSS and RKELM microgrid short-term load forecasting methods
CN107944594B (en) * 2017-09-30 2021-11-23 华南理工大学 Short-term load prediction method based on spearman grade and RKELM microgrid
CN107729706A (en) * 2017-11-29 2018-02-23 湖南科技大学 A kind of kinetic model construction method of Nonlinear Mechanical Systems
CN109117751A (en) * 2018-07-24 2019-01-01 南京信息工程大学 Random resonant weak signal detection method based on adaptive Chaos particle swarm optimization algorithm
CN109117751B (en) * 2018-07-24 2021-10-19 南京信息工程大学 Stochastic resonance weak signal detection method based on adaptive chaotic particle swarm optimization
CN108919652B (en) * 2018-10-10 2021-07-27 北京工商大学 Adaptive anti-interference shaping control method and system
CN108919652A (en) * 2018-10-10 2018-11-30 北京工商大学 A kind of adaptive anti-interference reforming control method and system
CN110109350A (en) * 2019-03-29 2019-08-09 广东工业大学 A kind of power capture optimization method of wave-power device that catching flame algorithm based on chaos moth
CN111123705A (en) * 2019-12-18 2020-05-08 南京航空航天大学 Design method for active vibration control of propeller and transmission shaft system

Also Published As

Publication number Publication date
CN104090490B (en) 2018-11-02

Similar Documents

Publication Publication Date Title
CN104090490A (en) Input shaper closed-loop control method based on chaotic particle swarm optimization algorithm
CN103885338A (en) Input reshaper parameter self-tuning control method based on particle swarm optimization algorithm
CN104915498B (en) High speed platform kinematic parameter automatic setting method based on Model Identification and equivalent-simplification
CN104533701B (en) A kind of automatic setting method of Turbine Governor System control parameter
CN106094859B (en) A kind of online real-time flight quality estimating of unmanned plane and parameter adjustment method
CN105843270A (en) Helicopter multi-frequency vibration active control method
JP5816826B2 (en) Motor drive device
US9274514B2 (en) Motor control apparatus
CN104993766A (en) Two-mass system resonance suppression method
CN102944994A (en) Robust fuzzy control method for hydraulic loop based on uncertain discrete model
JP6050865B1 (en) Servo control device with function to optimize control gain online with evaluation function
CN105703691A (en) Servo control device having automatic filter adjustment function based on experimental modal analysis
Pan et al. A review on self-recovery regulation (SR) technique for unbalance vibration of high-end equipment
CN104090596A (en) Five-stage S-curve acceleration and deceleration control method based on particle swarm optimization algorithm
CN105186959A (en) Parameter setting method of sliding mode controller of servo system
CN104852639A (en) Parameter self-tuning speed controller of permanent magnet synchronous motor based on neural network
CN103312248B (en) Method for compensating inflection point error of linear acceleration to deceleration based on DSP (Digital Signal Processor)
Toha et al. PID and inverse-model-based control of a twin rotor system
Xu et al. Rotor dynamic balancing control method based on fuzzy auto-tuning single neuron PID
CN105978400A (en) Ultrasonic motor control method
CN104950667A (en) Multi-rate prediction control method applied to train active suspension system
CN102967427B (en) Vortex-induced vibration testing device control system and control method based on force feedback principle
JP5407435B2 (en) Motor control device
Solberg Susceptibility of quadcopter flight to turbulence
CN111251901B (en) PR (pulse repetition) jitter suppression method based on stationary point calibration

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant