CN109857100B - Composite track tracking control algorithm based on inversion method and fast terminal sliding mode - Google Patents

Composite track tracking control algorithm based on inversion method and fast terminal sliding mode Download PDF

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CN109857100B
CN109857100B CN201910018014.9A CN201910018014A CN109857100B CN 109857100 B CN109857100 B CN 109857100B CN 201910018014 A CN201910018014 A CN 201910018014A CN 109857100 B CN109857100 B CN 109857100B
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胡海兵
郑希鹏
张波
张结文
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Hefei University of Technology
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Abstract

The invention discloses a composite track tracking control algorithm based on an inversion method and a quick terminal sliding mode, which belongs to the technical field of robots and comprises the following steps: the method comprises the following steps of (I) mobile robot kinematic model, (II) control algorithm design, and (III) error yeIs verified by convergence. The invention solves the problem that the convergence speed and the accuracy are difficult to be considered in the track tracking controller designed by the traditional global fast terminal sliding mode technology, not only improves the system error and the output convergence speed, but also reduces the system output error; and the discontinuous items in the traditional sliding mode structure are eliminated, the buffeting phenomenon is avoided, and the output stability is ensured.

Description

Composite track tracking control algorithm based on inversion method and fast terminal sliding mode
Technical Field
The invention relates to the technical field of robots, in particular to a composite track tracking control algorithm based on an inversion method and a fast terminal sliding mode.
Background
With the rapid development of the robot industry, the requirements on the working indexes of the robot are higher and higher, and therefore the tracking precision and stability of the mobile robot are more and more important. The mobile robot is a control system which is not completely constrained, a tracking error system of the track tracking is often a coupled nonlinear system, does not meet the necessary condition of Brockett, and is more complex to the problems of control, planning and the like. Therefore, many scholars have proposed various methods for solving the problem of trajectory tracking of mobile robots. The traditional PID algorithm controller has poor robustness, is insensitive to external interference and has difficult parameter setting. The sliding mode variable structure method has fast response and good robustness, but the discontinuous items in the control law are directly transferred to the output items, so that the inevitable buffeting phenomenon of the system is caused. The iterative learning control algorithm can be that the actual tracking error converges on a predetermined error track, but it generally requires that the initial position is on the predetermined track and the number of iterations affects the final learning result, which has a limit for practical application. The adaptive control can continuously acquire system input, state, output and performance parameters and correspondingly adjust the control law, so that the control performance is optimal, but the parameter selection is complex. The fuzzy control method has certain robustness, but the fuzzy control rule can be influenced by subjective factors of people. Aiming at a mobile robot system, the idea of an inversion method and a global fast terminal sliding mode technology is adopted, so that the system can be converged to a balanced state within limited time, discontinuous items in a traditional sliding mode structure are eliminated, the phenomenon of buffeting is avoided, and the stability of output is ensured.
Disclosure of Invention
Based on the technical problems in the background art, the invention provides a composite track tracking control algorithm based on an inversion method and a fast terminal sliding mode.
The technical scheme adopted by the invention is as follows:
a composite track tracking control algorithm based on an inversion method and a fast terminal sliding mode is characterized by comprising the following steps:
kinematic model of mobile robot
Establishing a pose error coordinate graph by taking a two-degree-of-freedom wheeled mobile robot as a research object;
in the attitude error coordinate diagram, M and M' are the shaft middle points of the two driving wheels; (x, y), (x)r,yr) Is the position of the mobile robot; theta, thetarIs the included angle between the advancing direction of the mobile robot and the x axis; x is the number ofe,yeeThe plane coordinate error and the direction error of the mobile robot are obtained; let P be (x, y, theta)T,q=(v,w)TV and w are the linear velocity and angular velocity of the mobile robot, respectively;
the kinematic equation of the mobile robot is as follows:
Figure GDA0003224422100000021
by Pr=(xr,yrr)TAnd q isr=(vr,wr)TTo represent a position command and a velocity command of the reference mobile robot; in the pose error coordinate diagram, the mobile robot sets the pose P as (x, y, theta)TMove to pose Pr=(xr,yrr)TMoving robot in new coordinate system Xe-YeThe coordinates in (1) are: pe=(xe,yee)TWherein thetae=θr-θ;
Setting new coordinate Xe-YeThe included angle between the coordinate system X and the coordinate system Y is theta, and according to a coordinate transformation formula, an error equation for describing the moving pose can be obtained as follows:
Figure GDA0003224422100000031
the differential equation of the attitude error obtained by the joint type (1) and (2) is as follows:
Figure GDA0003224422100000032
from the above analysis, the trajectory tracking of the kinematic model of the mobile robot, i.e. the seek control input q ═ (v, w)TSo that for any initial error, the system is under the control input, Pe=(xe,yee)TIs bounded, an
Figure GDA0003224422100000033
Design of control algorithm
Is provided with
Figure GDA0003224422100000034
Figure GDA0003224422100000035
Wherein alpha is1>0,β1>0,α2>0,β2> 0, and p1,q1,p2,q2Is positive odd and satisfies p1>q1,p2>q2
From the formula (3)
Figure GDA0003224422100000036
Figure GDA0003224422100000037
By solving the first order linear differential equation (4), it can be known that the time t is finite1Inner, thetaeIs equal to 0, and
Figure GDA0003224422100000038
similarly, solving the first order linear differential equation (5) can know that the time t is finite2Inner, xeIs equal to 0, and
Figure GDA0003224422100000039
for a mobile robotic system, as long as t > max { t1,t2Is then xe=0,θe=0;
Taking according to the inversion method (Back-stepping)
Figure GDA0003224422100000041
Figure GDA0003224422100000042
(a) When theta iseWhen v is 0, v is equal to v1Then the formula (3) can be expressed as
Figure GDA0003224422100000043
The introduction of the new virtual feedback variables is as follows:
Figure GDA0003224422100000044
wherein k is11>0;
Taking Lyapunov function
Figure GDA0003224422100000045
Combining the error differential equation (8) to obtain:
Figure GDA0003224422100000046
so v1The design is as follows:
Figure GDA0003224422100000047
wherein k is12Is greater than 0; will control the rate v1Substituting equation (11) into equation (9) can obtain:
Figure GDA0003224422100000048
as can be seen from the barkalat theorem,
Figure GDA0003224422100000049
respectively tend to zero; because of the fact that
Figure GDA00032244221000000410
Namely, it is
Figure GDA00032244221000000411
From the control rate, w is not constantly equal to zero, and
Figure GDA00032244221000000412
go to zero to obtain ye→ 0; further comprises
Figure GDA00032244221000000413
Knowing xe→0;
(b) When x iseWhen the value is equal to 0, the value w is equal to w2Then, equation (3) can be expressed as:
Figure GDA0003224422100000051
the introduction of the new virtual feedback variables is as follows:
Figure GDA0003224422100000052
taking Lyapunov function
Figure GDA0003224422100000053
Wherein
Figure GDA0003224422100000054
Combining the error differential equation (14) to obtain
Figure GDA0003224422100000055
Therefore w2Is designed as
Figure GDA0003224422100000056
Wherein k is21Is greater than 0; the control rate is substituted for formula (17) or formula (15) to obtain
Figure GDA0003224422100000057
According to the Barbalt's theorem, ye,
Figure GDA0003224422100000058
Approaching to zero; and because of
Figure GDA0003224422100000059
By
Figure GDA00032244221000000510
Then
Figure GDA00032244221000000511
The formula is
Figure GDA00032244221000000512
Equivalence;
(c) taking the comprehensive control rate as
Figure GDA00032244221000000513
Substituted into the formulae (6), (7), (12) and (18)
Figure GDA0003224422100000061
Wherein k is11,k12,k211122Are all positive numbers greater than zero, p1,q1,p2,q2Is positive odd and satisfies p1>q1,p2>q2
(III) pairs of errors yeDemonstration of convergence
(a) For a mobile robotic system, as long as t > max { t1,t2Is then xe=0,θe0, substituted by formula (4) or (5)
Figure GDA0003224422100000062
The combination of formula (3) and formula (21) can give
yew-v+vr=0 (22)
wr-w=0 (23)
Figure GDA0003224422100000063
The combined type (22), (23) and (24) can be obtained
Figure GDA0003224422100000064
Because the system expects an input vr,wrCannot be simultaneously zero, wrIf the value is not equal to zero, the system balance point is ye=0;
(b) Taking Lyapunov function
Figure GDA0003224422100000065
From the formulas (13) and (19)
Figure GDA0003224422100000066
Approaching zero, the combined formulas (9) and (15) can be obtained
Figure GDA0003224422100000067
Figure GDA0003224422100000068
Can obtain the product
Figure GDA0003224422100000071
From this, the error yeThe global asymptote converges to zero.
The invention has the advantages that:
the invention solves the problem that the convergence speed and the accuracy are difficult to be considered in the track tracking controller designed by the traditional global fast terminal sliding mode technology, not only improves the system error and the output convergence speed, but also reduces the system output error; and the discontinuous items in the traditional sliding mode structure are eliminated, the buffeting phenomenon is avoided, and the output stability is ensured.
Drawings
FIG. 1 is a diagram of a pose error coordinate of a mobile robot.
Fig. 2 is a block diagram of a robot tracking control system.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
Examples are given.
Referring to fig. 2, a composite trajectory tracking control algorithm based on an inversion method and a fast terminal sliding mode includes the following steps:
kinematic model of mobile robot
A two-degree-of-freedom wheeled mobile robot is taken as a research object, and a pose error coordinate graph of the two-degree-of-freedom wheeled mobile robot is shown in figure 1.
In FIG. 1, M, M' is the axle midpoint of the two drive wheels; (x, y), (x)r,yr) Is the position of the mobile robot; theta, thetarIs the included angle between the advancing direction of the mobile robot and the x axis; x is the number ofe,yeeThe plane coordinate error and the direction error of the mobile robot are obtained; let P be (x, y, theta)T,q=(v,w)TV and w are the linear velocity and angular velocity of the mobile robot, respectively;
the kinematic equation of the mobile robot is as follows:
Figure GDA0003224422100000081
by Pr=(xr,yrr)TAnd q isr=(vr,wr)TTo represent a position command and a velocity command of the reference mobile robot; in FIG. 1, a mobile machineMan-in-the-pose P ═ (x, y, θ)TMove to pose Pr=(xr,yrr)TMoving robot in new coordinate system Xe-YeThe coordinates in (1) are: pe=(xe,yee)TWherein thetae=θr-θ;
Setting new coordinate Xe-YeThe included angle between the coordinate system X and the coordinate system Y is theta, and according to a coordinate transformation formula, an error equation for describing the moving pose can be obtained as follows:
Figure GDA0003224422100000082
the differential equation of the attitude error obtained by the joint type (1) and (2) is as follows:
Figure GDA0003224422100000083
from the above analysis, the trajectory tracking of the kinematic model of the mobile robot, i.e. the seek control input q ═ (v, w)TSo that for any initial error, the system is under the control input, Pe=(xe,yee)TIs bounded, an
Figure GDA0003224422100000084
Design of control algorithm
Is provided with
Figure GDA0003224422100000091
Figure GDA0003224422100000092
Wherein alpha is1>0,β1>0,α2>0,β2> 0, and p1,q1,p2,q2Is positive odd and satisfies p1>q1,p2>q2
From the formula (3)
Figure GDA0003224422100000093
Figure GDA0003224422100000094
By solving the first order linear differential equation (4), it can be known that the time t is finite1Inner, thetaeIs equal to 0, and
Figure GDA0003224422100000095
similarly, solving the first order linear differential equation (5) can know that the time t is finite2Inner, xeIs equal to 0, and
Figure GDA0003224422100000096
for a mobile robotic system, as long as t > max { t1,t2Is then xe=0,θe=0;
Taking according to the inversion method (Back-stepping)
Figure GDA0003224422100000097
Figure GDA0003224422100000098
(a) When theta iseWhen v is 0, v is equal to v1Then the formula (3) can be expressed as
Figure GDA0003224422100000099
The introduction of the new virtual feedback variables is as follows:
Figure GDA00032244221000000910
wherein k is11>0;
Taking Lyapunov function
Figure GDA00032244221000000911
Combining the error differential equation (8) to obtain:
Figure GDA0003224422100000101
so v1The design is as follows:
Figure GDA0003224422100000102
wherein k is12Is greater than 0; will control the rate v1Substituting equation (11) into equation (9) can obtain:
Figure GDA0003224422100000103
as can be seen from the barkalat theorem,
Figure GDA0003224422100000104
respectively tend to zero; because of the fact that
Figure GDA0003224422100000105
Namely, it is
Figure GDA0003224422100000106
From the control rate, w is not constantly equal to zero, and
Figure GDA0003224422100000107
go to zero to obtain ye→ 0; further comprises
Figure GDA0003224422100000108
Knowing xe→0;
(b) When x iseWhen the value is equal to 0, the value w is equal to w2Then, equation (3) can be expressed as:
Figure GDA0003224422100000109
the introduction of the new virtual feedback variables is as follows:
Figure GDA00032244221000001010
taking Lyapunov function
Figure GDA00032244221000001011
Wherein
Figure GDA00032244221000001012
Combining the error differential equation (14) to obtain
Figure GDA00032244221000001013
Therefore w2Is designed as
Figure GDA0003224422100000111
Wherein k is21Is greater than 0; the control rate is substituted for formula (17) or formula (15) to obtain
Figure GDA0003224422100000112
Determined by BarbaltIn principle, y ise,
Figure GDA0003224422100000113
Approaching to zero; and because of
Figure GDA0003224422100000114
By
Figure GDA0003224422100000115
Then
Figure GDA0003224422100000116
The formula is
Figure GDA0003224422100000117
Equivalence;
(c) taking the comprehensive control rate as
Figure GDA0003224422100000118
Substituted into the formulae (6), (7), (12) and (18)
Figure GDA0003224422100000119
Wherein k is11,k12,k211122Are all positive numbers greater than zero, p1,q1,p2,q2Is positive odd and satisfies p1>q1,p2>q2
(III) pairs of errors yeDemonstration of convergence
(a) For a mobile robotic system, as long as t > max { t1,t2Is then xe=0,θe0, substituted by formula (4) or (5)
Figure GDA00032244221000001110
The combination of formula (3) and formula (21) can give
yew-v+vr=0 (22)
wr-w=0 (23)
Figure GDA00032244221000001111
The combined type (22), (23) and (24) can be obtained
Figure GDA0003224422100000121
Because the system expects an input vr,wrCannot be simultaneously zero, wrIf the value is not equal to zero, the system balance point is ye=0;
(b) Taking Lyapunov function
Figure GDA0003224422100000122
From the formulas (13) and (19)
Figure GDA0003224422100000123
Approaching zero, the combined formulas (9) and (15) can be obtained
Figure GDA0003224422100000124
Figure GDA0003224422100000125
Can obtain the product
Figure GDA0003224422100000126
From this, the error yeThe global asymptote converges to zero.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.

Claims (1)

1. A composite track tracking control algorithm based on an inversion method and a fast terminal sliding mode is characterized by comprising the following steps:
kinematic model of mobile robot
Establishing a pose error coordinate graph by taking a two-degree-of-freedom wheeled mobile robot as a research object;
in the attitude error coordinate diagram, M and M' are the shaft middle points of the two driving wheels; (x, y), (x)r,yr) Is the position of the mobile robot; theta, thetarIs the included angle between the advancing direction of the mobile robot and the x axis; x is the number ofe,yeeThe plane coordinate error and the direction error of the mobile robot are obtained; let P be (x, y, theta)T,q=(v,w)TV and w are the linear velocity and angular velocity of the mobile robot, respectively;
the kinematic equation of the mobile robot is as follows:
Figure FDA0003224422090000011
by Pr=(xr,yrr)TAnd q isr=(vr,wr)TTo represent a position command and a velocity command of the reference mobile robot; in the pose error coordinate diagram, the mobile robot sets the pose P as (x, y, theta)TMove to pose Pr=(xr,yrr)TMoving robot in new coordinate system Xe-YeThe coordinates in (1) are: pe=(xe,yee)TWherein thetae=θr-θ;
Setting new coordinate Xe-YeThe included angle between the coordinate system X and the coordinate system Y is theta, and description can be obtained according to a coordinate transformation formulaThe error equation of the moving pose is as follows:
Figure FDA0003224422090000012
the differential equation of the attitude error obtained by the joint type (1) and (2) is as follows:
Figure FDA0003224422090000013
from the above analysis, the trajectory tracking of the kinematic model of the mobile robot, i.e. the seek control input q ═ (v, w)TSo that for any initial error, the system is under the control input, Pe=(xe,yee)TIs bounded, an
Figure FDA0003224422090000021
Design of control algorithm
Is provided with
Figure FDA0003224422090000022
Figure FDA0003224422090000023
Wherein alpha is1>0,β1>0,α2>0,β2> 0, and p1,q1,p2,q2Is positive odd and satisfies
p1>q1,p2>q2
From the formula (3)
Figure FDA0003224422090000024
Figure FDA0003224422090000025
By solving the first order linear differential equation (4), it can be known that the time t is finite1Inner, thetaeIs equal to 0, and
Figure FDA0003224422090000026
similarly, solving the first order linear differential equation (5) can know that the time t is finite2Inner, xeIs equal to 0, and
Figure FDA0003224422090000027
for a mobile robotic system, as long as t > max { t1,t2Is then xe=0,θe=0;
Taking according to the inversion method (Back-stepping)
Figure FDA0003224422090000028
Figure FDA0003224422090000029
(a) When theta iseWhen v is 0, v is equal to v1Then the formula (3) can be expressed as
Figure FDA00032244220900000210
The introduction of the new virtual feedback variables is as follows:
Figure FDA0003224422090000031
wherein k is11>0;
Taking Lyapunov function
Figure FDA0003224422090000032
Combining the error differential equation (8) to obtain:
Figure FDA0003224422090000033
so v1The design is as follows:
Figure FDA0003224422090000034
wherein k is12Is greater than 0; will control the rate v1Substituting equation (11) into equation (9) can obtain:
Figure FDA0003224422090000035
as can be seen from the barkalat theorem,
Figure FDA0003224422090000036
respectively tend to zero; because of the fact that
Figure FDA0003224422090000037
Namely, it is
Figure FDA0003224422090000038
From the control rate, w is not constantly equal to zero, and
Figure FDA0003224422090000039
go to zero to obtain ye→ 0; further comprises
Figure FDA00032244220900000310
Knowing xe→0;
(b) When x iseWhen the value is equal to 0, the value w is equal to w2Then, equation (3) can be expressed as:
Figure FDA00032244220900000311
the introduction of the new virtual feedback variables is as follows:
Figure FDA00032244220900000312
taking Lyapunov function
Figure FDA00032244220900000313
Wherein
Figure FDA0003224422090000041
Combining the error differential equation (14) to obtain
Figure FDA0003224422090000042
Therefore w2Is designed as
Figure FDA0003224422090000043
Wherein k is21Is greater than 0; the control rate is substituted for formula (17) or formula (15) to obtain
Figure FDA0003224422090000044
According to the Barbalt's theorem, ye,
Figure FDA0003224422090000045
Approaching to zero; and because of
Figure FDA0003224422090000046
By
Figure FDA0003224422090000047
Then
Figure FDA0003224422090000048
The formula is
Figure FDA0003224422090000049
Equivalence;
(c) taking the comprehensive control rate as
Figure FDA00032244220900000410
Substituted into the formulae (6), (7), (12) and (18)
Figure FDA00032244220900000411
Wherein k is11,k12,k211122Are all positive numbers greater than zero, p1,q1,p2,q2Is positive odd and satisfies
p1>q1,p2>q2
(III) pairs of errors yeDemonstration of convergence
(a) For a mobile robotic system, as long as t > max { t1,t2Is then xe=0,θe0, substituted by formula (4) or (5)
Figure FDA0003224422090000051
Combination formula (3) and formula (2)1) Can obtain
yew-v+vr=0 (22)
wr-w=0 (23)
Figure FDA0003224422090000052
The combined type (22), (23) and (24) can be obtained
Figure FDA0003224422090000053
Because the system expects an input vr,wrCannot be simultaneously zero, wrIf the value is not equal to zero, the system balance point is ye=0;
(b) Taking Lyapunov function
Figure FDA0003224422090000054
From the formulas (13) and (19)
Figure FDA0003224422090000055
Approaching zero, the combined formulas (9) and (15) can be obtained
Figure FDA0003224422090000056
Figure FDA0003224422090000057
Can obtain the product
Figure FDA0003224422090000058
From this, the error yeGlobalAsymptotically converging to zero.
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