CN116276962A - Limited time anti-interference control method for universal pneumatic flexible mechanical arm - Google Patents

Limited time anti-interference control method for universal pneumatic flexible mechanical arm Download PDF

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CN116276962A
CN116276962A CN202310005507.5A CN202310005507A CN116276962A CN 116276962 A CN116276962 A CN 116276962A CN 202310005507 A CN202310005507 A CN 202310005507A CN 116276962 A CN116276962 A CN 116276962A
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mechanical arm
flexible mechanical
pneumatic flexible
universal pneumatic
finite time
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赵苓
李卓骏
张金会
王涛
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Tianjin University
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25JMANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
    • B25J9/00Programme-controlled manipulators
    • B25J9/16Programme controls
    • B25J9/1602Programme controls characterised by the control system, structure, architecture
    • B25J9/1605Simulation of manipulator lay-out, design, modelling of manipulator
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25JMANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
    • B25J9/00Programme-controlled manipulators
    • B25J9/16Programme controls
    • B25J9/1628Programme controls characterised by the control loop
    • B25J9/163Programme controls characterised by the control loop learning, adaptive, model based, rule based expert control
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
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Abstract

The limited-time anti-interference control method for the universal pneumatic flexible mechanical arm comprises the following steps: simplifying the universal pneumatic flexible mechanical arm into a connecting rod model by using a D-H method, and performing kinematic analysis to obtain a kinematic analysis model and the positions of the tail end points of the universal pneumatic flexible mechanical arm; based on a kinematic analysis model of the universal pneumatic flexible mechanical arm, establishing a dynamic model of the universal pneumatic flexible mechanical arm by using an Euler-Lagrange method; taking uncertainty of the universal pneumatic flexible mechanical arm as disturbance, and establishing a second-order mathematical model of the pneumatic flexible mechanical arm; designing a finite time expansion state observer to estimate disturbance, and designing a finite time backstepping controller based on a disturbance estimation value to compensate the influence of the disturbance on a system; aiming at the uncertainty of the model, the finite time control method is designed to compensate the influence on the position control precision of the pneumatic flexible mechanical arm, so that the method has stronger robustness and higher control precision.

Description

Limited time anti-interference control method for universal pneumatic flexible mechanical arm
Technical field:
the invention belongs to the field of pneumatic servo systems and the field of anti-interference control, and particularly relates to a limited-time anti-interference control method for a universal pneumatic flexible mechanical arm.
The background technology is as follows:
with rapid development of robot technology, the mechanical arm is widely applied to the field of intelligent manufacturing. In order to meet the requirements of the intelligent manufacturing site on flexibility and flexibility of the mechanical arm, the universal pneumatic flexible mechanical arm driven by pneumatic artificial muscles is designed, and the functions of grabbing, carrying and the like are realized.
The universal pneumatic flexible mechanical arm is a multi-degree-of-freedom connecting rod mechanism connected by a universal joint, and the kinematic analysis model and the dynamic model of the universal pneumatic flexible mechanical arm are established based on the structural characteristics of the universal pneumatic flexible mechanical arm, so that the universal pneumatic flexible mechanical arm has higher research significance and research value; however, the uncertainty of the model in the model has a large influence on the accurate control of the universal pneumatic flexible mechanical arm, and in most of the existing researches, the detailed modeling is rarely performed on the universal pneumatic flexible mechanical arm, and meanwhile, the influence of the uncertainty of the model on the position control of the pneumatic flexible mechanical arm is considered, so that the steady-state performance and the transient-state performance of the system are reduced, and the expected control effect cannot be achieved.
The invention comprises the following steps:
the invention provides a limited-time anti-interference control method for a universal pneumatic flexible mechanical arm, which establishes a kinematic analysis model and a dynamic model of the universal pneumatic flexible mechanical arm, and aims at the uncertainty of the model, the limited-time control method is designed to compensate the influence of the model on the position control precision of the pneumatic flexible mechanical arm, so that the accurate space track tracking of the pneumatic flexible mechanical arm in the limited time is realized.
In order to achieve the above purpose, the technical scheme adopted by the invention is as follows: 1. the limited-time anti-interference control method for the universal pneumatic flexible mechanical arm is characterized by comprising the following steps of:
simplifying the universal pneumatic flexible mechanical arm into a connecting rod model by using a D-H method, and performing kinematic analysis to obtain a kinematic analysis model and the positions of the tail end points of the universal pneumatic flexible mechanical arm;
based on a kinematic analysis model of the universal pneumatic flexible mechanical arm, establishing a dynamic model of the universal pneumatic flexible mechanical arm by using an Euler-Lagrange method;
taking uncertainty of the universal pneumatic flexible mechanical arm as disturbance, and establishing a second-order mathematical model of the pneumatic flexible mechanical arm;
and designing a finite time expansion state observer to estimate disturbance, and designing a finite time backstepping controller based on a disturbance estimated value to compensate the influence of the disturbance on the system.
Preferably, the step of simplifying the universal pneumatic flexible mechanical arm into a connecting rod model by using a D-H method and performing kinematic analysis to obtain the kinematic analysis model and the position of the end point of the universal pneumatic flexible mechanical arm includes:
the mechanical structure based on the universal pneumatic flexible mechanical arm simplifies the universal pneumatic flexible mechanical arm into a six-link model by using a D-H method, and a transfer matrix A is introduced for acquiring the position of the tail end point of the mechanical arm i
Figure SMS_1
Wherein alpha is i-1 Is the torsion angle of the ith-1 connecting rod; d, d i Is the offset distance of the ith link; θ i Is the ith joint angle; according to the transfer matrix, the transfer matrix of each connecting rod of the universal pneumatic flexible mechanical arm is obtained as follows:
Figure SMS_2
Figure SMS_3
Figure SMS_4
multiplying the seven transfer matrices to obtain the position of the tail end point of the mechanical arm as follows:
Figure SMS_5
wherein,,
Figure SMS_6
Figure SMS_7
Figure SMS_8
wherein: p (P) x (t)、P y (t)、P z (t) is the coordinate of X, Y, Z axis of the terminal point in the space coordinate system, c i =cosθ i (t),s i =sinθ i (t),θ i (t) is the deflection angle of the ith joint, where i=1, 2,3,4,5,6, l is the arm link length.
Preferably, the step of establishing the dynamic model of the universal pneumatic flexible mechanical arm by using the euler-lagrangian method based on the kinematic analysis model of the universal pneumatic flexible mechanical arm comprises the following steps:
the Euler-Lagrangian equation is expressed as follows:
Figure SMS_9
based on Euler-Lagrange equation and kinematic analysis, the dynamic model of the universal pneumatic flexible mechanical arm is expressed as:
Figure SMS_10
wherein:
Figure SMS_11
is an inertial matrix, ++>
Figure SMS_12
Is a coriolis force matrix,/->
Figure SMS_13
Is a gravity matrix; m is the mass of the connecting rod; g T =[-g,0,0,0]Is a gravitational acceleration matrix;
Figure SMS_14
is a centroid distance matrix;
wherein: upj = a1a2. Qaj. Ap,
Figure SMS_15
upjk=a1a2..qaj..qak..ap are three intermediate variables;
Figure SMS_16
is two parameter matrices;
based on the driving mode of the universal pneumatic flexible mechanical arm, the dynamic model is transformed, and each element is written into a vector form:
Figure SMS_17
wherein:
Figure SMS_18
Figure SMS_19
Figure SMS_20
wherein θ (t) is the vector representation of the deflection angle, D-1 (t) is the vector representation of Dij, C (t) is the vector representation of Cijk, g (t) is the vector representation of Gi, k0 is the scaling factor of the electrical proportional valve, u0 is the preloaded voltage, L0 is the pneumatic artificial muscle length, R is the force arm, b is the total length of the mesh, N is the number of turns around the outer mesh, ui (t) is the control voltage of the ith joint, where i=1, 2,3,4,5,6; i6 is the identity matrix.
Preferably, the step of establishing the second-order mathematical model of the pneumatic flexible mechanical arm taking the uncertainty of the universal pneumatic flexible mechanical arm as a disturbance includes:
the second-order mathematical model of the universal pneumatic flexible mechanical arm is formed by combining the kinematic analysis model and the dynamic model:
Figure SMS_21
in the method, in the process of the invention,
Figure SMS_22
Figure SMS_23
Figure SMS_24
wherein,,
Figure SMS_25
is D -1 Elements of (t)/(x)>
Figure SMS_26
Is->
Figure SMS_27
Elements b of (b) kk (t)/>
Figure SMS_28
Element f of (2) k Is P x First order partial derivative of (t), g k Is P y First order partial derivative of (t), f kj Is P x First derivative of (t), g kj Is P x (t) a first derivative; omega (t) is the uncertainty of the universal pneumatic flexible mechanical arm.
Preferably, the step of designing the finite time expansion state observer estimates the disturbance and designing the finite time backstepping controller based on the disturbance estimation value, and compensating the influence of the disturbance on the system includes:
the finite time extended state observer is:
Figure SMS_29
in the method, in the process of the invention,
Figure SMS_30
and is also provided with
Figure SMS_31
β 1 ,β 2 And beta 3 Positive adjustable parameter e 1 (t)=z 1 (t)-x 1 (t)、e 2 (t)=z 2 (t)-x 2 (t)、e 3 (t)=z 3 (t)-x 3 (t) is an error variable in the finite time extended state observer;
the finite time backstepping controller is:
Figure SMS_32
wherein B is 0 Is a system parameter; k (k) p Is a positive adjustable parameter; sliding die face sigma 1 (t) is designed to:
Figure SMS_33
wherein sigma 2 (t) is sigma 1 The first derivative of (t),
Figure SMS_34
is a virtual variable of the back-stepping method, wherein +.>
Figure SMS_35
Is a slip form surface sigma 1 An error between (t) and 0;
wherein e (t) =x 1 (t)-v 1 (t) is the position error, k of the universal pneumatic flexible mechanical arm 1 、k 2 、k 3 、k 4 、ζ、ξ 1 Adjustable parameters, v, with gamma, p and q being positive 0 (t) is the desired position, v 0 (t) obtaining v via a tracking differentiator 1 (t)。
Preferably, the step of designing the finite time expansion state observer to estimate disturbance and designing the finite time backstepping controller based on the disturbance estimation value to compensate the influence of the disturbance on the system further comprises: and carrying out convergence analysis on the limited-time extended state observer by adopting a Liepunov function and carrying out convergence analysis on the limited-time backstepping controller by adopting the Liepunov function.
Preferably, the convergence analysis of the finite time extended state observer by adopting the Liapunov function specifically includes:
the design of the Lyapunov equation for the finite time extended state observer proves the finite time convergence, and the error system of the finite time extended state observer is given as follows:
Figure SMS_36
design demonstration of required related variables
Figure SMS_37
The derivative is obtained by:
Figure SMS_38
wherein,,
Figure SMS_39
the lyapunov equation was designed as follows:
v(t)=ε T (t)Pε(t)
deriving the lisapunov function equation v (t):
Figure SMS_40
will be
Figure SMS_41
The following is carried into the above formula:
Figure SMS_42
the convergence time satisfies:
Figure SMS_43
wherein:
η 1 ∈(0,r 1 ),η 2 ∈(0,r 2 ) Is two bounded constants; v (e) 0 ) Is the initial value of the lyapunov function;
Figure SMS_44
preferably, the convergence analysis of the finite time back-step controller by using the Liapunov function specifically includes:
two lyapunov functions are designed using the back-stepping method, the first lyapunov function being designed as:
Figure SMS_45
for V 1 (t) derivative and combination
Figure SMS_46
Obtaining:
Figure SMS_47
wherein,,
Figure SMS_48
is a slip form surfaceFirst derivative sigma of (2) 2 (t) and virtual variable alpha 1 An error between (t);
when (when)
Figure SMS_49
When there is +.>
Figure SMS_50
I.e. < ->
Figure SMS_51
The second lyapunov function is designed based on this as:
Figure SMS_52
for V 2 (t) finite time back-step controllers that derive and bring into design are available:
Figure SMS_53
the convergence time satisfies:
Figure SMS_54
compared with the prior art, the invention has the following beneficial effects:
the invention establishes the kinematic analysis model and the dynamic model of the universal pneumatic flexible mechanical arm, and designs the finite time control method to compensate the influence of the model uncertainty on the position control precision of the pneumatic flexible mechanical arm, thereby having stronger robustness, being easy for engineering realization, having higher control precision and ensuring the stable, accurate and fast control performance.
Description of the drawings:
FIG. 1 is a schematic diagram of a limited time anti-interference control method for a universal pneumatic flexible mechanical arm.
FIG. 2 is a flow chart of a method for controlling the limited time anti-interference of a flexible pneumatic mechanical arm according to a preferred embodiment of the present invention.
Fig. 3 is a kinematic analysis diagram of the universal pneumatic flexible mechanical arm of the invention.
Fig. 4 is a graph of position tracking for a gimbaled pneumatic flexible mechanical arm of the present invention.
Fig. 5 is a graph of the state 1 estimated signal of the finite time extended state observer according to the present invention.
The specific embodiment is as follows:
for the purpose of clarifying the technical objects of the present invention, the technical scheme of the present invention is explained in detail with reference to the following drawings and specific embodiments.
Fig. 1 is a schematic diagram of the method of the invention, and illustrates a limited-time anti-interference control method for a universal pneumatic flexible mechanical arm.
The following describes in detail, but not by way of limitation, modeling of a universal pneumatic flexible mechanical arm and a control algorithm designed for model uncertainty of the mechanical arm according to the present invention with reference to fig. 1-4.
A limited-time anti-interference control method for a universal pneumatic flexible mechanical arm comprises the following steps:
s100, simplifying the universal pneumatic flexible mechanical arm into a connecting rod model by using a D-H method, and performing kinematic analysis to obtain a kinematic analysis model and the positions of the tail end points of the universal pneumatic flexible mechanical arm;
s200, based on a kinematic analysis model of the universal pneumatic flexible mechanical arm, establishing a dynamic model of the universal pneumatic flexible mechanical arm by using an Euler-Lagrange method;
s300, taking uncertainty of the universal pneumatic flexible mechanical arm as disturbance, and establishing a second-order mathematical model of the pneumatic flexible mechanical arm;
s400, designing a finite time expansion state observer to estimate disturbance, and designing a finite time backstepping controller based on a disturbance estimated value to compensate the influence of the disturbance on a system. The invention establishes the kinematic analysis model and the dynamic model of the universal pneumatic flexible mechanical arm, and designs the finite time control method to compensate the influence of the model uncertainty on the position control precision of the pneumatic flexible mechanical arm, thereby having stronger robustness, being easy for engineering realization, having higher control precision and ensuring the stable, accurate and fast control performance.
In this embodiment, the step of simplifying the universal pneumatic flexible mechanical arm into the connecting rod model by using the D-H method and performing the kinematic analysis to obtain the kinematic analysis model and the position of the end point of the universal pneumatic flexible mechanical arm includes:
the mechanical structure based on the universal pneumatic flexible mechanical arm is simplified into a six-link model by using a D-H method, and the D-H table is listed as follows:
connecting rod a i a i d i θ i
1 0 0 0 θ 1
2 0 -90° 0 θ 2
3 l 90° 0 θ 3
4 0 -90° 0 θ 4
5 l 90° 0 θ 5
6 0 -90° 0 θ 6
In the above formula, a i Is the i-th link length; alpha i Is the torsion angle of the ith connecting rod; d, d i Is the offset distance of the ith link; θ i Is the i-th joint angle.
In order to obtain the position of the tail end point of the mechanical arm, a transfer matrix A is introduced i
Figure SMS_55
Wherein alpha is i-1 Is the torsion angle of the ith-1 connecting rod; d, d i Is the offset distance of the ith link; θ i Is the ith joint angle; root of Chinese characterAccording to the D-H table and the transfer matrix, the transfer matrix of each connecting rod of the universal pneumatic flexible mechanical arm can be obtained as follows:
Figure SMS_56
Figure SMS_57
Figure SMS_58
multiplying the seven transfer matrices to obtain the position of the tail end point of the mechanical arm as follows:
Figure SMS_59
wherein,,
Figure SMS_60
Figure SMS_61
Figure SMS_62
wherein: p (t) is the position of the end point of the universal pneumatic flexible mechanical arm, px (t), py (t), pz (t) are the coordinates of the end point on the X, Y, Z axis in the spatial coordinate system, ci=cos θi (t), si=sin θi (t), θi (t) is the deflection angle of the ith joint, where i=1, 2,3,4,5,6, l is the mechanical arm link length.
In this embodiment, S200, based on a kinematic analysis model of a universal pneumatic flexible mechanical arm, the step of establishing a dynamic model of the universal pneumatic flexible mechanical arm by using the euler-lagrangian method includes:
the Euler-Lagrangian equation is expressed as follows:
Figure SMS_63
based on Euler-Lagrange equation and kinematic analysis, the dynamic model of the universal pneumatic flexible mechanical arm is expressed as:
Figure SMS_64
wherein:
Figure SMS_65
is an inertial matrix, ++>
Figure SMS_66
Is a coriolis force matrix,/->
Figure SMS_67
Is a gravity matrix; m is the mass of the connecting rod; g T =[-g,0,0,0]Is a gravitational acceleration matrix;
Figure SMS_68
is a centroid distance matrix;
wherein:
Figure SMS_69
U pjk =A 1 A 2 L QA j L QA k LA p is three intermediate variables;
Figure SMS_70
is two parameter matrices;
based on the driving mode of the universal pneumatic flexible mechanical arm, the dynamic model is transformed, and each element is written into a vector form:
Figure SMS_71
wherein:
U 0 (t)=[u 1 (t),u 2 (t),u 3 (t)+u 4 (t),u 4 (t)-u 3 (t),u 5 (t),u 6 (t)] T
Figure SMS_72
Figure SMS_73
wherein θ (t) is a vector representation of the deflection angle, D -1 (t) is D ij Is c (t) is c ijk G (t) is G i Is represented by a vector of k 0 Is the proportionality coefficient of the electric proportioning valve, u 0 To preload the voltage, L 0 The pneumatic artificial muscle is the original length, R is a force arm, b is the total length of the woven mesh, and N is the number of circles of the outer woven mesh; u (u) i (t) is the control voltage of the ith joint, where i = 1,2,3,4,5,6; i 6 Is an identity matrix.
In this embodiment, S300, taking uncertainty of the universal pneumatic flexible mechanical arm as disturbance, the step of establishing a second-order mathematical model of the pneumatic flexible mechanical arm includes:
the second-order mathematical model of the universal pneumatic flexible mechanical arm is formed by combining the kinematic analysis model and the dynamic model:
Figure SMS_74
in the method, in the process of the invention,
Figure SMS_75
Figure SMS_76
Figure SMS_77
wherein,,
Figure SMS_78
is D -1 Elements of (t)/(x)>
Figure SMS_79
Is->
Figure SMS_80
Elements b of (b) kk (t)/>
Figure SMS_81
Element f of (2) k Is P x First order partial derivative of (t), g k Is P y First order partial derivative of (t), f kj Is P x First derivative of (t), g kj Is P x (t) a first derivative; omega (t) is the uncertainty of the universal pneumatic flexible mechanical arm. The invention establishes the kinematic analysis model and the dynamic model of the universal pneumatic flexible mechanical arm, and designs the finite time control method to compensate the influence of the model uncertainty on the position control precision of the pneumatic flexible mechanical arm, thereby having stronger robustness, being easy for engineering realization, having higher control precision and ensuring the stable, accurate and fast control performance.
In this embodiment, the step of designing the finite-time expansion state observer to estimate the disturbance and designing the finite-time backstepping controller based on the disturbance estimation value to compensate the influence of the disturbance on the system includes:
the finite time extended state observer is:
Figure SMS_82
in the method, in the process of the invention,
Figure SMS_83
and is also provided with
Figure SMS_84
And beta 3 is positive, e 1 (t)=z 1 (t)-x 1 (t)、e 2 (t)=z 2 (t)-x 2 (t)、e 3 (t)=z 3 (t)-x 3 (t) is an error variable in the finite time extended state observer;
the finite time backstepping controller is:
Figure SMS_85
wherein B is 0 Is a system parameter; k (k) p Is a positive adjustable parameter; sliding die face sigma 1 (t) is designed to:
Figure SMS_86
wherein sigma 2 (t) is sigma 1 The first derivative of (t),
Figure SMS_87
is a virtual variable of the back-stepping method, wherein +.>
Figure SMS_88
Is a slip form surface sigma 1 An error between (t) and 0;
wherein e (t) =x 1 (t)-v 1 (t) is the position error, k of the universal pneumatic flexible mechanical arm 1 、k 2 、k 3 、k 4 、ζ、ξ 1 Adjustable parameters, v, with gamma, p and q being positive 0 (t) is the desired position, v 0 (t) obtaining v via a tracking differentiator 1 (t)。
Preferably, the step of designing the finite time expansion state observer to estimate disturbance and designing the finite time backstepping controller based on the disturbance estimation value to compensate the influence of the disturbance on the system further comprises: s500, carrying out convergence analysis on the finite time expansion state observer by adopting a Liepunov function and carrying out convergence analysis on the finite time backstepping controller by adopting the Liepunov function.
In this embodiment, S501 performs convergence analysis on the finite time extended state observer by using a li-apunov function, and specifically includes:
the design of the Lyapunov equation for the finite time extended state observer proves the finite time convergence, and the error system of the finite time extended state observer is given as follows:
Figure SMS_89
design demonstration of required related variables
Figure SMS_90
The derivative is obtained by:
Figure SMS_91
wherein,,
Figure SMS_92
the lyapunov equation was designed as follows:
v(t)=ε T (t)Pε(t)
deriving the lisapunov function equation v (t):
Figure SMS_93
will be
Figure SMS_94
The following is carried into the above formula:
Figure SMS_95
the convergence time satisfies:
Figure SMS_96
wherein:
η 1 ∈(0,r 1 ),η 2 ∈(0,r 2 ) Is two bounded constants; v (e) 0 ) Is the initial value of the lyapunov function;
Figure SMS_97
thus demonstrating a limited time convergence of ε (t).
In this embodiment, S502 performs convergence analysis on the finite time backstepping controller by using a li-apunov function, which specifically includes:
two design lyapunov functions are designed using the back-stepping method, the first lyapunov function being designed as:
Figure SMS_98
for V 1 (t) derivative and combination
Figure SMS_99
Obtaining:
Figure SMS_100
wherein,,
Figure SMS_101
for the first derivative sigma of the slide surface 2 (t) and virtual variable alpha 1 An error between (t);
when (when)
Figure SMS_102
When there is +.>
Figure SMS_103
I.e. < ->
Figure SMS_104
The second lyapunov function is designed based on this as:
Figure SMS_105
for V 2 (t) finite time back-step controllers that derive and bring into design are available:
Figure SMS_106
the convergence time satisfies:
Figure SMS_107
thus, a limited time convergence of the limited time backstepping controller can be obtained. Therefore, the limited-time anti-interference control method for the universal pneumatic flexible mechanical arm is stable and effective.
In a further preferred embodiment of the invention, in order to verify that the limited-time anti-interference control method for the universal pneumatic flexible mechanical arm provided by the invention has better control performance, the verification of the invention is provided, so that the universal pneumatic flexible mechanical arm has higher control precision and better anti-interference capability under the control method provided by the invention, and the method specifically comprises the following steps:
the initial position of the end of the universal pneumatic flexible mechanical arm is set to be (0, 67.5). The universal pneumatic flexible mechanical arm is driven by 12 McKibben type pneumatic artificial muscles, an electric proportional valve voltage signal is given to an industrial personal computer board card configured through an experimental platform, the electric proportional valve controls the internal air pressure of the pneumatic artificial muscles, so that the universal pneumatic flexible mechanical arm generates corresponding deflection, the deflection angle is collected by an angle sensor, and the position of an end effector is obtained through space position analysis and is used as the output of the system.
The control target is set as follows:
the two step signals are respectively used as expected signals of two shafts of the end effector of the universal pneumatic flexible mechanical arm, and the amplitudes are respectively: v 01 =18cm、v 02 =11.25cm;
The position curve of the output of the universal pneumatic flexible mechanical arm is shown in fig. 4 given the different desired position signals of the two axes. Wherein, the solid line represents the expected position signals input by two shafts, and the amplitude is 18cm and 11.25cm respectively; the dashed lines represent the actual position outputs of the two axes at the desired positions of 18cm and 11.25cm, respectively. As can be seen from fig. 4, the actual positions of the two axes of the universal pneumatic flexible mechanical arm can accurately track the desired position without overshoot.
The desired position signals on the two axes are v 01 =18cm、v 02 When 11.25cm, the finite time extended state observer outputs the position x 1 Estimate z of (t) 1 (t) is shown in FIG. 4. Wherein z is 11 (t) represents the output position x for the first axis at an 18cm desired position signal input 11 An estimated curve of (t); z 12 (t) represents the output position x for the second axis at 11.25cm desired position signal input 12 An estimated curve of (t). As can be seen from fig. 5, the finite time extended state observer can quickly and stably estimate the actual output position x when different desired position signals are inputted to both axes 1 (t)。
Variations and modifications of the above embodiments will occur to those skilled in the art to which the invention pertains from the foregoing disclosure and teachings. Therefore, the present invention is not limited to the above-described embodiments, but is intended to be capable of modification, substitution or variation in light thereof, which will be apparent to those skilled in the art in light of the present teachings.

Claims (8)

1. The limited-time anti-interference control method for the universal pneumatic flexible mechanical arm is characterized by comprising the following steps of:
simplifying the universal pneumatic flexible mechanical arm into a connecting rod model by using a D-H method, and performing kinematic analysis to obtain a kinematic analysis model and the positions of the tail end points of the universal pneumatic flexible mechanical arm;
based on a kinematic analysis model of the universal pneumatic flexible mechanical arm, establishing a dynamic model of the universal pneumatic flexible mechanical arm by using an Euler-Lagrange method;
taking uncertainty of the universal pneumatic flexible mechanical arm as disturbance, and establishing a second-order mathematical model of the pneumatic flexible mechanical arm;
and designing a finite time expansion state observer to estimate disturbance, and designing a finite time backstepping controller based on a disturbance estimated value to compensate the influence of the disturbance on the system.
2. The method for controlling the limited-time anti-interference of the universal pneumatic flexible mechanical arm according to claim 1, wherein the step of simplifying the universal pneumatic flexible mechanical arm into a connecting rod model by using a D-H method and performing kinematic analysis to obtain a kinematic analysis model and the position of the end point of the universal pneumatic flexible mechanical arm comprises the following steps:
the mechanical structure based on the universal pneumatic flexible mechanical arm simplifies the universal pneumatic flexible mechanical arm into a six-link model by using a D-H method, and a transfer matrix A is introduced for acquiring the position of the tail end point of the mechanical arm i
Figure QLYQS_1
Wherein a is i-1 Is the torsion angle of the ith-1 connecting rod; d, d i Is the offset distance of the ith link; θ i Is the ith joint angle; according to the transfer matrix, the transfer matrix of each connecting rod of the universal pneumatic flexible mechanical arm is obtained as follows:
Figure QLYQS_2
Figure QLYQS_3
Figure QLYQS_4
multiplying the seven transfer matrices to obtain the position of the tail end point of the mechanical arm as follows:
Figure QLYQS_5
wherein,,
Figure QLYQS_6
Figure QLYQS_7
Figure QLYQS_8
wherein: p (P) x (t)、P y (t)、P z (t) is the coordinate of X, Y, Z axis in the spatial coordinate system of the terminal point, C i =cosθ i (t),S i =sinθ i (t),θ i (t) is the angle of deflection of the ith joint, where i=1, 2,3,4,5,6,
Figure QLYQS_9
is the length of the connecting rod of the mechanical arm.
3. The method for controlling the limited-time anti-interference of the universal pneumatic flexible mechanical arm according to claim 1, wherein the step of establishing the dynamic model of the universal pneumatic flexible mechanical arm by using the euler-lagrangian method based on the kinematic analysis model of the universal pneumatic flexible mechanical arm comprises the following steps:
the Euler-Lagrangian equation is expressed as follows:
Figure QLYQS_10
based on Euler-Lagrange equation and kinematic analysis, the dynamic model of the universal pneumatic flexible mechanical arm is expressed as:
Figure QLYQS_11
wherein:
Figure QLYQS_12
is an inertial matrix, ++>
Figure QLYQS_13
Is a matrix of the coriolis force,
Figure QLYQS_14
is a gravity matrix; m is the mass of the connecting rod; g T =[-g,0,0,0]Is a gravitational acceleration matrix;
Figure QLYQS_15
is a centroid distance matrix;
wherein: u (U) pj =A 1 A 2 ...QA j ...A p ,
Figure QLYQS_16
U pjk =A 1 A 2 ...QA j ...QA k ...A p Is three intermediate variables;
Figure QLYQS_17
is two parameter matrices;
based on the driving mode of the universal pneumatic flexible mechanical arm, the dynamic model is transformed, and each element is written into a vector form:
Figure QLYQS_18
wherein:
U 0 (t)=[u 1 (t),u 2 (t),u 3 (t)+u 4 (t),u 4 (t)-u 3 (t),u 5 (t),u 6 (t)] T ,
Figure QLYQS_19
Figure QLYQS_20
wherein θ (t) is a vector representation of the deflection angle, D -1 (t) is D ij Is C (t) is C ijk G (t) is G i Is represented by a vector of k 0 Is the proportionality coefficient of the electric proportioning valve, u 0 To preload the voltage, L 0 Is the original length of pneumatic artificial muscle, R is the force arm, b is the total length of the woven mesh, N is the number of circles around the outer woven mesh, u i (t) is the control voltage of the ith joint, where i = 1,2,3,4,5,6; i 6 Is an identity matrix.
4. The method for controlling finite time anti-interference of a universal pneumatic flexible mechanical arm according to claim 1, wherein the step of taking uncertainty of the universal pneumatic flexible mechanical arm into consideration as disturbance and establishing a second-order mathematical model of the pneumatic flexible mechanical arm comprises the steps of:
the second-order mathematical model of the universal pneumatic flexible mechanical arm is formed by combining the kinematic analysis model and the dynamic model:
Figure QLYQS_21
in the method, in the process of the invention,
Figure QLYQS_22
Figure QLYQS_23
wherein,,
Figure QLYQS_24
is D -1 Elements of (t)/(x)>
Figure QLYQS_25
Is->
Figure QLYQS_26
Elements b of (b) kk (t) is->
Figure QLYQS_27
Element f of (2) k Is P x First order partial derivative of (t), g k Is P y First order partial derivative of (t), f kj Is P x First derivative of (t), g kj Is P x (t) a first derivative; omega (t) is the uncertainty of the universal pneumatic flexible mechanical arm.
5. The method for controlling finite time anti-interference of a universal pneumatic flexible mechanical arm according to claim 1, wherein the step of designing the finite time extended state observer to estimate the disturbance and designing the finite time backstepping controller based on the disturbance estimated value to compensate the influence of the disturbance on the system comprises:
the finite time extended state observer is:
Figure QLYQS_28
in the method, in the process of the invention,
Figure QLYQS_29
and is also provided with
Figure QLYQS_30
β 1 ,β 2 And beta 3 Positive adjustable parameter e 1 (t)=z 1 (t)-x 1 (t)、e 2 (t)=z 2 (t)-x 2 (t)、e 3 (t)=z 3 (t)-x 3 (t) is an error variable in the finite time extended state observer;
the finite time backstepping controller is:
Figure QLYQS_31
wherein B is 0 Is a system parameter; k (k) p Is a positive adjustable parameter; sliding die face sigma 1 (t) is designed to:
Figure QLYQS_32
wherein sigma 2 (t) is sigma 1 The first derivative of (t),
Figure QLYQS_33
is a virtual variable of a back-stepping method, wherein
Figure QLYQS_34
Is a slip form surface sigma 1 An error between (t) and 0;
wherein e (t) =x 1 (t)-v 1 (t) is the position error, k of the universal pneumatic flexible mechanical arm 1 、k 2 、k 3 、k 4 、ζ、ξ 1 Adjustable parameters, v, with gamma, p and q being positive 0 (t) is the desired position, v 0 (t) obtaining v via a tracking differentiator 1 (t)。
6. The method for controlling finite time anti-interference of a universal pneumatic flexible mechanical arm according to claim 1, wherein the step of designing the finite time extended state observer to estimate disturbance and designing the finite time backstepping controller based on the disturbance estimated value to compensate the influence of disturbance on the system further comprises: and carrying out convergence analysis on the limited-time extended state observer by adopting a Liepunov function and carrying out convergence analysis on the limited-time backstepping controller by adopting the Liepunov function.
7. The method for controlling finite time anti-interference of a universal pneumatic flexible mechanical arm according to claim 6, wherein the method for performing convergence analysis on the finite time extended state observer by using a liaeprunov function specifically comprises:
the design of the Lyapunov equation for the finite time extended state observer proves the finite time convergence, and the error system of the finite time extended state observer is given as follows:
Figure QLYQS_35
design demonstration of required related variables
Figure QLYQS_36
The derivative is obtained by:
Figure QLYQS_37
wherein,,
Figure QLYQS_38
Δ(t)=[0 0 -g(t)] T
the lyapunov equation was designed as follows:
v(t)=ε T (t)Pε(t)
deriving the lisapunov function equation v (t):
Figure QLYQS_39
will be
Figure QLYQS_40
λ min (P)||ε(t)|| 2 ≤v≤λ max (P)||ε(t)|| 2 The following is carried into the above formula:
Figure QLYQS_41
the convergence time satisfies:
Figure QLYQS_42
wherein:
η 1 ∈(0,r 1 ),η 2 ∈(0,r 2 ) Is two bounded constants; v (e) 0 ) Is the initial value of the lyapunov function;
Figure QLYQS_43
8. the method for finite time anti-interference control of a universal pneumatic flexible mechanical arm according to claim 6, wherein the finite time backstepping controller is subjected to convergence analysis by adopting a lisapunov function, and specifically comprises the following steps:
two lyapunov functions are designed using the back-stepping method, the first lyapunov function being designed as:
Figure QLYQS_44
for V 1 (t) derivative and combination
Figure QLYQS_45
Obtaining:
Figure QLYQS_46
wherein,,
Figure QLYQS_47
for the first derivative sigma of the slide surface 2 (t) and virtual variable alpha 1 An error between (t);
when (when)
Figure QLYQS_48
When there is +.>
Figure QLYQS_49
I.e. < ->
Figure QLYQS_50
The second lyapunov function is designed based on this as:
Figure QLYQS_51
for V 2 (t) finite time back-step controllers that derive and bring into design are available:
Figure QLYQS_52
the convergence time satisfies:
Figure QLYQS_53
CN202310005507.5A 2023-01-04 2023-01-04 Limited time anti-interference control method for universal pneumatic flexible mechanical arm Pending CN116276962A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117590754A (en) * 2024-01-18 2024-02-23 北京理工大学 Intelligent learning output regulation and control method of robot system
CN117885103A (en) * 2024-03-14 2024-04-16 山东大学 Flexible mechanical arm control method and system based on reduced-order expanded state observer

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117590754A (en) * 2024-01-18 2024-02-23 北京理工大学 Intelligent learning output regulation and control method of robot system
CN117590754B (en) * 2024-01-18 2024-05-03 北京理工大学 Intelligent learning output regulation and control method of robot system
CN117885103A (en) * 2024-03-14 2024-04-16 山东大学 Flexible mechanical arm control method and system based on reduced-order expanded state observer
CN117885103B (en) * 2024-03-14 2024-05-17 山东大学 Flexible mechanical arm control method and system based on reduced-order expanded state observer

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