CN113359477B - Design method of vehicle longitudinal and lateral coupling trajectory tracking controller - Google Patents

Design method of vehicle longitudinal and lateral coupling trajectory tracking controller Download PDF

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CN113359477B
CN113359477B CN202110788124.0A CN202110788124A CN113359477B CN 113359477 B CN113359477 B CN 113359477B CN 202110788124 A CN202110788124 A CN 202110788124A CN 113359477 B CN113359477 B CN 113359477B
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赵健
陈志成
朱冰
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Jilin University
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Abstract

The invention discloses a design method of a vehicle longitudinal and lateral coupling track tracking controller. The method comprises the following steps: firstly, establishing a track tracking model according to the kinematic and dynamic relation between a vehicle and an expected track; designing a track tracking controller coupled in the longitudinal direction and the lateral direction of the vehicle to obtain a complete system control law; the trajectory tracking controller consists of three parts of steady-state-like control, reference dynamic feedforward control and state-dependent error feedback control; compensating system uncertainty disturbance caused by vehicle motion state change by combining with an adaptive law; and step four, realizing the track tracking control of the whole vehicle through a bottom layer control distribution strategy. The invention reliably ensures that the automatic driving vehicle can overcome the disturbance caused by the problems of longitudinal and lateral nonlinear coupling dynamic characteristics, parameter uncertainty and the like of the system, stably and accurately controls the automatic driving vehicle to track the target motion track and expect the longitudinal motion speed, and completes the driving task.

Description

Design method of vehicle longitudinal and lateral coupling trajectory tracking controller
Technical Field
The invention belongs to the technical field of automobiles, and particularly relates to a design method of a vehicle longitudinal and lateral coupling track tracking controller.
Background
Due to breakthrough of key technologies such as perception, computer hardware, software and the like, in recent years, the automatic automobile driving technology has received great attention and development, and is considered to be an effective solution capable of effectively improving the driving safety of the automobile and reducing the fuel consumption rate. Among the related researches, trajectory tracking control is one of the most important core problems for realizing automatic driving of automobiles. The basic task of trajectory tracking is to ensure that the vehicle safely and stably tracks the desired trajectory automatically and accurately at a set speed.
However, the vehicle has many difficulties in tracking the track. First, the design of vehicle controllers relies on models that adequately reflect the key behavioral characteristics of trajectory tracking control. Too complex models will increase the design difficulty of the controller, and too simple models will result in a weak performance of the controller. Secondly, when the vehicle tracks, the system does not model the disturbance, the uncertainty of the parameters and other problems, which will affect the performance of the vehicle controller. Finally, in the tracking process, the longitudinal dynamics and the lateral dynamics of the vehicle have obvious nonlinear coupling dynamics characteristic relation due to factors such as tire force coupling and load transfer variation. This non-linear coupling dynamics characteristic relationship will deteriorate the robustness and accuracy of the controller.
Disclosure of Invention
The invention provides a design method of a vehicle longitudinal and lateral coupling track tracking controller, which reliably ensures that an automatic driving vehicle can overcome the disturbance caused by the problems of longitudinal and lateral nonlinear coupling dynamic characteristics, parameter uncertainty and the like of a system, stably and accurately controls the automatic driving vehicle to track a target motion track and expect longitudinal motion speed, and completes a driving task.
The technical scheme of the invention is described as follows by combining the attached drawings:
a design method for a vehicle longitudinal and lateral coupling trajectory tracking controller comprises the following steps:
step one, establishing a track tracking model containing system parameter uncertainty and vehicle longitudinal and lateral nonlinear coupling dynamics characteristic relation according to the kinematics and dynamics relation between a vehicle and an expected track;
designing a track tracking controller coupled in the longitudinal direction and the lateral direction of the vehicle to obtain a complete system control law; the trajectory tracking controller consists of three parts of steady-state-like control, reference dynamic feedforward control and state-dependent error feedback control;
compensating system uncertainty disturbance caused by vehicle motion state change by combining with an adaptive law;
and step four, realizing the track tracking control of the whole vehicle through a bottom layer control distribution strategy.
The specific method of the first step is as follows:
11) assuming that the left wheel and the right wheel are stressed symmetrically, a simplified vehicle dynamic model is established as follows:
Figure GDA0003327707550000021
Figure GDA0003327707550000022
Figure GDA0003327707550000023
in the formula, m represents the mass of the whole vehicle; v. ofxRepresenting a vehicle longitudinal speed; v. ofyRepresenting a vehicle lateral speed;
Figure GDA0003327707550000024
a differential representing a longitudinal speed of the vehicle;
Figure GDA0003327707550000025
a differential representing the lateral velocity of the vehicle; ω represents the yaw angular velocity of the vehicle;
Figure GDA0003327707550000026
represents the derivative of the yaw rate of the vehicle; fuxRepresenting an equivalent longitudinal force applied at the vehicle center of mass; cwxRepresenting a longitudinal wind resistance coefficient of the vehicle; cwyRepresenting a lateral wind resistance coefficient of the vehicle; i iszRepresenting the moment of inertia of the vehicle; lfRepresenting the distance of the center of mass to the front axle of the vehicle; lrRepresenting the distance of the center of mass to the rear axle of the vehicle; fyfIndicating the lateral force to which the front wheel tyre is subjected; fyrIndicating the lateral force to which the rear wheel tire is subjected;
12) during the tracking process of the vehicle, the tire is in a linear area, and the lateral force of the tire is approximately represented as:
Figure GDA0003327707550000027
Figure GDA0003327707550000028
in the formula, CfRepresenting tire front wheel side sheet stiffness; crRepresenting tire rear wheel cornering stiffness; alpha is alphafRepresenting a tire front wheel side slip angle; alpha is alpharIndicating a tire rear wheel side slip angle; fyfIndicating the lateral force to which the front wheel tyre is subjected; fyrIndicating the lateral force to which the rear wheel tire is subjected; beta represents the vehicle centroid slip angle; deltafIndicating a vehicle front wheel steering angle; lfRespectively representing the distances of the center of mass to the front axle of the vehicle; lrRepresenting the distance of the center of mass to the rear axis; v. ofxRepresenting vehicle longitudinal speed, ω representing vehicle yaw angular velocity;
13) assuming that the actual values of the vehicle system parameters during trajectory tracking are known, the complete vehicle dynamics model is represented as:
Figure GDA0003327707550000029
Figure GDA00033277075500000210
Figure GDA00033277075500000211
in the formula, m represents the mass of the whole vehicle; v. ofxRepresenting a vehicle longitudinal speed; v. ofyRepresenting a vehicle lateral speed;
Figure GDA00033277075500000212
a differential representing a longitudinal speed of the vehicle;
Figure GDA00033277075500000213
a differential representing the lateral velocity of the vehicle; ω represents the yaw angular velocity of the vehicle;
Figure GDA00033277075500000214
represents the derivative of the yaw rate of the vehicle; fuxRepresenting an equivalent longitudinal force applied at the vehicle center of mass; beta represents the vehicle centroid slip angle; deltafIndicating a vehicle front wheel steering angle;
Figure GDA0003327707550000031
ρiactual values representing system parameters;
Figure GDA0003327707550000032
ideal values representing the variation of system parameters with the vehicle motion state; rhooiStandard values for system parameters are expressed and are expressed as:
Figure GDA0003327707550000033
in the formula, CwyRepresenting a longitudinal wind resistance coefficient of the vehicle; cwyRepresenting a lateral wind resistance coefficient of the vehicle; i iszRepresenting the moment of inertia of the vehicle; m represents the mass of the whole vehicle; lfRepresenting the distance of the center of mass to the front axle of the vehicle; lrRepresenting the distance of the center of mass to the rear axle of the vehicle; cfRepresenting tire front wheel cornering stiffness; crRepresenting tire rear wheel cornering stiffness;
14) the vehicle kinematic model is:
Figure GDA0003327707550000034
Figure GDA0003327707550000035
Figure GDA0003327707550000036
in the formula, xeIndicating a vehicle longitudinal tracking error; y iseIndicating a vehicle lateral tracking error;
Figure GDA0003327707550000037
a differential representing a longitudinal tracking error of the vehicle;
Figure GDA0003327707550000038
a differential representing a vehicle lateral tracking error; v. ofxdRepresenting a desired vehicle longitudinal speed; v. ofxRepresenting an actual vehicle longitudinal speed;
Figure GDA0003327707550000039
a differential representing an actual vehicle yaw angle;
Figure GDA00033277075500000310
a derivative representing a desired vehicle yaw angle;
Figure GDA00033277075500000311
representing an error between the desired yaw angle and the actual yaw angle;
Figure GDA00033277075500000312
representing the differential error between the desired yaw angle and the actual yaw angle; v. ofyRepresenting a vehicle lateral speed; omegadRepresenting a desired vehicle yaw angular velocity; omega represents the true vehicle yaw angular velocity; rρA road curvature representing a target trajectory;
15) deriving a vehicle kinematic model to obtain:
Figure GDA00033277075500000313
Figure GDA00033277075500000314
Figure GDA00033277075500000315
in the formula, xeIndicating a vehicle longitudinal tracking error; y iseIndicating a vehicle lateral tracking error;
Figure GDA00033277075500000316
a differential representing a longitudinal tracking error of the vehicle;
Figure GDA00033277075500000317
a differential representing a vehicle lateral tracking error;
Figure GDA00033277075500000318
a second derivative representing a longitudinal tracking error of the vehicle;
Figure GDA00033277075500000319
a second derivative representing a vehicle lateral tracking error; v. ofxdRepresenting a desired vehicle longitudinal speed;
Figure GDA0003327707550000041
a differential representing a desired vehicle longitudinal speed; v. ofxRepresenting a vehicle longitudinal speed;
Figure GDA0003327707550000042
a differential representing a longitudinal speed of the vehicle; v. ofyRepresenting a vehicle lateral speed;
Figure GDA0003327707550000043
a differential representing the lateral velocity of the vehicle;
Figure GDA0003327707550000044
a derivative representing a yaw angular velocity of the desired vehicle;
Figure GDA0003327707550000045
represents the derivative of true vehicle yaw angular velocity; ω represents the yaw angular velocity of the vehicle;
Figure GDA0003327707550000046
representing an error between the desired yaw angle and the actual yaw angle;
Figure GDA0003327707550000047
representing the differential error between the desired yaw angle and the actual yaw angle;
Figure GDA0003327707550000048
representing the error second derivative between the desired yaw angle and the actual yaw angle;
Figure GDA0003327707550000049
a second derivative representing an actual vehicle yaw angle;
Figure GDA00033277075500000410
a second derivative representing a desired vehicle yaw angle;
16) using longitudinal and lateral tracking errors as state variables of the system, i.e. x1=[xe ye]T
Figure GDA00033277075500000411
Figure GDA00033277075500000412
The equivalent longitudinal force applied at the vehicle center of mass and the front wheel steering angle serve as control variables of the system, i.e. u ═ Fuxδf]TSubstituting the vehicle dynamics model into the vehicle kinematics model to obtain a vehicle longitudinal and lateral coupling nonlinear trajectory tracking model containing system parameter uncertainty:
Figure GDA00033277075500000413
Figure GDA00033277075500000414
y=x1 (18)
in the formula, x1And x2State variables representing the system; u represents a control variable of the system; y represents the system output, F1(x1)=02×1Representing a first order system variable matrix; g1(x1)=I2×2Representing a first order system state matrix;
Figure GDA00033277075500000415
Figure GDA00033277075500000416
representing a second-order system variable matrix;
Figure GDA00033277075500000417
representing a second order system control matrix; p1And P2Is a system parameter matrix, f2,1(x)、g2,1(x) Representing the local basis function of the system, f2(x)、g2(x) And represents the system overall basis function:
P1=[ρ1 ρ2 ρ3ρ4 ρ6 ρ7]T,P2=[ρ5 ρ8]T,g2(x)=[g2,2(x) g2,3(x)]T,
f2(x)=[f2,2(x) f2,3(x) f2,4(x) f2,5(x) f2,6(x) f2,7(x)]T,
Figure GDA00033277075500000418
Figure GDA00033277075500000419
Figure GDA00033277075500000420
Figure GDA00033277075500000421
in the formula, P1And P2Is a system parameter matrix, pi(i ═ 1,2, … 8) represents the true values of the system parameters; f. of2,j(x)(j=1,2,…7)、g2,k(x) (k ═ 1,2,3) represents the system local basis function; f. of2(x)、g2(x) Representing the system overall basis function; v. ofxRepresenting a vehicle longitudinal speed; v. ofyRepresenting a vehicle lateral speed; v. ofxdRepresenting a desired vehicle longitudinal speed;
Figure GDA0003327707550000051
a differential representing a desired vehicle longitudinal speed;
Figure GDA0003327707550000052
representing an error between the desired yaw angle and the actual yaw angle;
Figure GDA0003327707550000053
representing the differential error between the desired yaw angle and the actual yaw angle; ω represents the yaw angular velocity of the vehicle; x is the number ofeIndicating a vehicle longitudinal tracking error; y iseIndicating a vehicle lateral tracking error; beta represents the vehicle centroid slip angle; and m represents the mass of the whole vehicle.
The specific method of the second step is as follows:
21) the system output y is derived until the occurrence of the control input u:
Figure GDA0003327707550000054
Figure GDA0003327707550000055
in the formula, x1And x2State variables representing the system;
Figure GDA0003327707550000056
representing a state variable differential of the system;
Figure GDA0003327707550000057
represents the differential of the system output;
Figure GDA0003327707550000058
represents the second derivative of the system output; f, F1(x1) Representing a first order system variable matrix; g1(x1) Representing a first order system state matrix; u represents a control variable of the system;
Figure GDA0003327707550000059
an output matrix representing the second order system output; b (x) ═ G1(x1)G2(x) A control matrix representing the second order system output; c (x) ═ G1(x1)F2(x) A parameter matrix representing the second order system output; f2(x) Representing a second-order system variable matrix; g2(x) Representing a second order system control matrix;
22) it is assumed that the system is already in steady state motion, at which point
Figure GDA00033277075500000510
Then the steady-state-like control law of the system is:
Figure GDA00033277075500000511
in the formula usRepresenting a steady-state-like control law of the system; g2(x) Representing a second order system control matrix; f2(x) Representing a second-order system variable matrix; f. of2,1(x)、g2,1(x) Representing a system local basis function; f. of2(x)、g2(x) Representing the system overall basis function; p1And P2Is a system parameter matrix;
23) adding a feedforward control law into a calibrated control law is used for improving the response performance of the system, namely:
u=us+uf (22)
wherein u represents a system control law; u. ofsSteady state-like control law, u, representing the systemfRepresenting the dynamic reference feedforward control law of the system.
Let y be yd
Figure GDA00033277075500000512
Substituting the control law (22) into the system (20) to obtain a feed forward control law as follows:
Figure GDA0003327707550000061
in the formula ufRepresenting a dynamic reference feedforward control law of the system; g2(x) Representing a second order system control matrix;
Figure GDA00033277075500000615
a differential representing a desired output of the system;
Figure GDA00033277075500000616
a second derivative representing the desired output of the system; a (x) represents an output matrix of the second order system output; a (x) represents an output matrix of the second order system output; p2Is a system parameter matrix; g2,1(x) Representing a system local basis function; g2(x) Representing the system overall basis function;
24) the introduced error feedback control law is as follows:
u=us+uf+ue (24)
wherein u represents a system control law; u. ofsRepresenting a steady-state-like control law of the system; u. offRepresenting a dynamic reference feedforward control law of the system; u. ofeRepresenting the error feedback control law of the system;
defining a system tracking error as e1=yd-y, substituting the control law (24) into the system (20) can determine:
Figure GDA0003327707550000062
in the formula,
Figure GDA0003327707550000063
represents the system tracking error differential;
Figure GDA0003327707550000064
a second derivative representing a system tracking error; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; u. ofeRepresenting the error feedback control law of the system;
order to
Figure GDA0003327707550000065
The closed loop error system is then expressed as:
Figure GDA0003327707550000066
Figure GDA0003327707550000067
in the formula,
Figure GDA0003327707550000068
represents the system tracking error differential; e.g. of the type2Representing a virtual control input;
Figure GDA0003327707550000069
representing a virtual control input differential; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix, ueRepresenting the error feedback control law of the system;
25) option e2Defining Lyapunov functions for virtual control inputs
Figure GDA00033277075500000610
Then the corresponding derivative is:
Figure GDA00033277075500000611
in the formula,
Figure GDA00033277075500000612
representing a defined first lyapunov function differential; e.g. of the type1Representing a system tracking error;
Figure GDA00033277075500000613
represents the system tracking error differential; e.g. of the type2Representing a virtual control input;
26) to ensure stability of the closed-loop control system, i.e.
Figure GDA00033277075500000614
The selected virtual control inputs are:
Figure GDA0003327707550000071
in the formula,
Figure GDA0003327707550000072
representing a desired virtual control input; e.g. of the type1Indicating the system tracking error, k1Representing a controller parameter;
for k1>0,
Figure GDA0003327707550000073
It is possible to obtain:
Figure GDA0003327707550000074
Figure GDA0003327707550000075
in the formula,
Figure GDA0003327707550000076
representing a defined first lyapunov function differential; k is a radical of1Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure GDA0003327707550000077
represents the system tracking error differential;
27) to e is making e2Approach to
Figure GDA0003327707550000078
To ensure the system e1→ 0, we define
Figure GDA0003327707550000079
Then we get:
Figure GDA00033277075500000710
Figure GDA00033277075500000711
in the formula,
Figure GDA00033277075500000712
representing the first defined lyapunov function differential, k1Representing the three-step controller parameters, e1And
Figure GDA00033277075500000713
respectively representing the systematic tracking error and the systematic tracking error differential, e3Representing a virtual control input error.
With e3→ 0, obtaining
Figure GDA00033277075500000714
Then system e1Gradual stabilization to error e3The derivation is carried out to obtain:
Figure GDA00033277075500000715
in the formula,
Figure GDA00033277075500000716
representing a virtual control input error differential; e.g. of the type2Representing an actual virtual control input;
Figure GDA00033277075500000717
representing a desired virtual control input differential;
Figure GDA00033277075500000718
representing a virtual control input differential; k is a radical of1Representing a controller parameter;
Figure GDA00033277075500000719
represents the system tracking error differential; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; u. ofeRepresenting the error feedback control law of the system;
28) definition includes error e3Lyapunov function of the interior
Figure GDA00033277075500000720
And (5) obtaining by derivation:
Figure GDA00033277075500000721
in the formula,
Figure GDA00033277075500000722
represents a defined second lyapunov function differential;
Figure GDA00033277075500000723
representing a defined first lyapunov function differential; e.g. of the type3Representing a virtual control input error;
Figure GDA00033277075500000724
representing a virtual control input error differential; k is a radical of1Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure GDA00033277075500000725
represents the system tracking error differential; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; u. ofeRepresenting the error feedback control law of the system.
According to the Lyapunov direct method, the error feedback control law is selected as follows:
Figure GDA0003327707550000081
in the formula ueRepresenting the error feedback control law of the system; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; k is a radical of1And k2Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure GDA0003327707550000082
represents the system tracking error differential; e.g. of the type3Representing a virtual control input error;
selection of k2>0, then
Figure GDA0003327707550000083
In the formula,
Figure GDA0003327707550000084
represents a defined second lyapunov function differential; k is a radical of1And k2Representing a controller parameter; e.g. of the type1Representing a system tracking error; e.g. of the type3Representing a virtual control input error;
29) the error closed loop system is gradually stabilized, and (26), (29) and
Figure GDA0003327707550000085
and (36) obtaining the error feedback control law of practical application as follows:
Figure GDA0003327707550000086
in the formula ueRepresenting the error feedback control law of the system; a (x) an output matrix representing the output of the second order system, G2(x) Representing a second order system control matrix; k is a radical of1And k2Representing a three-step controller parameter; e.g. of the type1Representing a system tracking error;
Figure GDA0003327707550000087
represents the system tracking error differential; g2,1(x) Representing a system local basis function; g2(x) Representing the system overall basis function; p2Is a system parameter matrix;
the obtained complete system control law:
Figure GDA0003327707550000088
wherein u represents a system control law; u. ofsIs a system-like steady-state control law; u. offThe system dynamically refers to a feedforward control law; u. ofeRepresenting a system error feedback control law; f. ofP(x)=[G2(x)]-1(1+k1k2) Representing a scale term parameter; f. ofD(x)=[G2(x)]-1[k1+k2+A(x)]Representing a differential term parameter; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; k is a radical of1And k2Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure GDA0003327707550000089
representing the system tracking error differential.
The concrete method of the third step is as follows:
31) defining system parameter estimation values:
Figure GDA0003327707550000091
in the formula,
Figure GDA0003327707550000092
representing system parameter estimates;
Figure GDA0003327707550000093
an estimate representing a change in a system parameter with a vehicle motion state; rhooiStandard values representing system parameters;
32) the system control law is redefined as:
Figure GDA0003327707550000094
wherein u represents a system control input;
Figure GDA0003327707550000095
representing a second-order system variable matrix estimated value;
Figure GDA0003327707550000096
representing a second-order system control matrix estimated value;
Figure GDA0003327707550000097
P1and P2Is a system parameter matrix estimated value;
Figure GDA0003327707550000098
representing system parameter estimates;
Figure GDA0003327707550000099
a differential representing a desired output of the system;
Figure GDA00033277075500000910
a second derivative representing the desired output of the system;
Figure GDA00033277075500000911
an output matrix estimation value representing the output of the second-order system; e.g. of the type1Representing a system tracking error;
Figure GDA00033277075500000912
represents the system tracking error differential; k is a radical of1And k2Representing a controller parameter;
33) by substituting the obtained system control law (41) into the system (20), the following can be obtained:
Figure GDA00033277075500000913
in the formula,
Figure GDA00033277075500000914
represents the second derivative of the system output; k is a radical of1And k2Representing a controller parameter;
Figure GDA00033277075500000915
an output matrix estimation value representing the output of the second-order system; e.g. of the type1Representing a system tracking error;
Figure GDA00033277075500000916
represents the system tracking error differential; f2(x) The representation represents a second-order system variable matrix;
Figure GDA00033277075500000917
representing a second-order system variable matrix estimated value; g2(x) Representing a second order system control matrix;
Figure GDA00033277075500000918
representing a second-order system control matrix estimated value; u represents a system control input;
Figure GDA00033277075500000919
a second derivative representing the desired output of the system;
from the above equation, the closed-loop error system considering parameter uncertainty can be organized as:
Figure GDA00033277075500000920
wherein,
Figure GDA00033277075500000921
in the formula, k1And k2Representing a controller parameter;
Figure GDA00033277075500000922
an output matrix estimation value representing the output of the second-order system; e.g. of the type1Representing a system tracking error;
Figure GDA0003327707550000101
represents the system tracking error differential; Δ P represents the total error of the system parameter matrix; theta represents a system composition base; p1And P2Representing a system parameter matrix; delta P1And Δ P2Representing the system parameter matrix error;
Figure GDA0003327707550000102
an estimate representing a change in a system parameter with a vehicle motion state;
Figure GDA0003327707550000103
ideal values representing the variation of system parameters with the vehicle motion state; f. of2(x)、g2(x) Representing the system overall basis function; u represents a system control input;
34) selecting
Figure GDA0003327707550000104
Is the state variable of the error system, then:
Figure GDA0003327707550000105
in the formula, emA state variable representing an error system;
Figure GDA0003327707550000106
a state variable differential representing an error system;
Figure GDA0003327707550000107
Figure GDA0003327707550000108
a state variable parameter matrix representing an error system;
Figure GDA0003327707550000109
a parameter variable matrix representing an error system; theta represents a system composition base; Δ P represents the total error of the system parameter matrix; k is a radical of1And k2Representing a controller parameter;
35) defining a Lyapunov function including uncertainty of system parameters
Figure GDA00033277075500001010
Wherein Q>0 is a positive definite symmetric matrix, and the derivation is as follows:
Figure GDA00033277075500001011
in the formula,
Figure GDA00033277075500001012
represents a defined third lyapunov function differential; e.g. of the typemA state variable representing an error system; a. themA state variable parameter matrix representing an error system; q represents a positive definite symmetric matrix; b ismA parameter variable matrix representing an error system; theta represents a system composition base; Δ P represents the total error of the system parameter matrix;
Figure GDA00033277075500001013
representing the total error differential of the system parameter matrix; tau represents a parameter error variable parameter quantization parameter;
Figure GDA00033277075500001014
representing the system parameter adaptation law;
36) the system parameter self-adaptation law is taken as follows:
Figure GDA00033277075500001015
in the formula,
Figure GDA00033277075500001016
represents a system parameter ofAn adaptation law; tau represents a parameter error variable parameter quantization parameter; e.g. of the typemA state variable representing an error system; q represents a positive definite symmetric matrix; b ismA parameter variable matrix representing an error system, and theta represents a system combination base;
and substituting the adaptive law of the system parameters into (45) to obtain:
Figure GDA00033277075500001017
in the formula,
Figure GDA00033277075500001018
represents a defined third lyapunov function differential; e.g. of the typemA state variable representing an error system; q represents a positive definite symmetric matrix; a. themA state variable parameter matrix representing an error system.
The concrete method of the fourth step is as follows:
equivalent longitudinal force F applied to vehicle centroid and obtained based on solution of trajectory tracking controlleruxCan not be directly applied to vehicle control, and needs to be decomposed by a bottom-layer control distribution strategy to obtain a driving torque signal T which can be responded by the vehicletqAnd a brake pressure signal;
equivalent longitudinal force F when applied at the center of mass of the vehicleuxWhen the torque is greater than or equal to 0, the vehicle system is considered to be in the driving mode, and the corresponding driving torque is expressed as:
Figure GDA0003327707550000111
in the formula, TtqA signal indicative of a target drive torque of the vehicle; fuxRepresenting an equivalent longitudinal force applied at the vehicle center of mass; r represents a wheel rolling radius; i.e. i0Representing the whole equivalent transmission ratio of the whole vehicle; etaTThe whole equivalent transmission efficiency of the whole vehicle is represented;
equivalent longitudinal force F when applied at the center of mass of the vehicleuxLess than 0; consider a vehicle trainWhen the system is in the driving mode, the corresponding driving torque can be expressed as:
Figure GDA0003327707550000112
wherein P represents a vehicle target master cylinder brake pressure; fuxRepresenting an equivalent longitudinal force applied at the vehicle center of mass; r represents a wheel rolling radius; d represents the diameter of the brake master cylinder; rBRepresents the effective brake caliper radius; i istRepresenting the moment of inertia of the tire;
Figure GDA0003327707550000113
representing the differential of the tire speed.
The invention has the beneficial effects that:
1) the vehicle track tracking model built by the invention comprises the problems of longitudinal and lateral nonlinear coupling dynamic characteristics of the vehicle, uncertainty of system parameters and the like, and fully reflects the key behavior characteristics expressed in the track tracking control of the automatic driving vehicle;
2) the invention provides a vehicle longitudinal and lateral coupling track tracking controller based on a nonlinear three-step method control theory, and solves the nonlinear control problem brought to a system by the vehicle longitudinal and lateral nonlinear coupling dynamic characteristics;
3) the vehicle track tracking controller designed based on the nonlinear three-step method theory has a simple structure, has a structure similar to a PID algorithm applied to engineering, accords with the use habit calibrated by an algorithm engineer, and is convenient for practical application and popularization of engineering;
4) the invention provides a used parameter self-adaptive law which effectively compensates the uncertain disturbance of system parameters caused by the change of the vehicle motion state and improves the track tracking control precision and the system robustness;
5) based on the Lyapunov stability theory, the method deduces that the designed vehicle track tracking controller has good robustness to the problems of unmodeled disturbance, parameter uncertainty and the like of the system.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings needed to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained according to the drawings without inventive efforts.
FIG. 1 is an architectural diagram of the present invention;
FIG. 2 is a schematic diagram of a trajectory tracking dynamics model of an autonomous vehicle;
FIG. 3 is a schematic diagram of a trajectory tracking kinematics model of an autonomous vehicle;
FIG. 4 is a schematic diagram of a sorting architecture for adaptive control law compensation of system parameter uncertainty;
FIG. 5 is a graph of longitudinal speed control performance;
FIG. 6 is a graph of longitudinal speed error control performance;
FIG. 7 is a trace-tracking graph;
FIG. 8 is a graph of trajectory tracking lateral error;
fig. 9 is a graph of yaw angle control performance;
FIG. 10 is a graph of yaw angle error control performance;
FIG. 11 is a graph of front wheel steering control performance;
fig. 12 is a graph of yaw-rate control performance.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.
Referring to fig. 1, a method for designing a vehicle longitudinal-lateral coupling trajectory tracking controller includes the following steps:
step one, establishing a track tracking model containing system parameter uncertainty and vehicle longitudinal and lateral nonlinear coupling dynamics characteristic relation according to the kinematics and dynamics relation between a vehicle and an expected track;
referring to fig. 2, 11), a complete vehicle dynamics model is established, and although the designed controller can be closer to the practical application, the design burden of the controller is also greatly increased. The relationship between the longitudinal motion and the lateral motion of the vehicle is more concerned in track tracking control, so that the roll, pitch and vertical motion of the vehicle are ignored, the left wheel and the right wheel are assumed to be stressed symmetrically, and a simplified vehicle dynamic model is established as follows:
Figure GDA0003327707550000121
Figure GDA0003327707550000122
Figure GDA0003327707550000123
in the formula, m represents the mass of the whole vehicle; v. ofxRepresenting a vehicle longitudinal speed; v. ofyRepresenting a vehicle lateral speed;
Figure GDA0003327707550000131
a differential representing a longitudinal speed of the vehicle;
Figure GDA0003327707550000132
a differential representing the lateral velocity of the vehicle; ω represents the yaw angular velocity of the vehicle;
Figure GDA0003327707550000133
represents the derivative of the yaw rate of the vehicle; fuxRepresenting an equivalent longitudinal force applied at the vehicle center of mass; cwxRepresenting a longitudinal wind resistance coefficient of the vehicle; cwyRepresenting a lateral wind resistance coefficient of the vehicle; i iszRepresenting the moment of inertia of the vehicle; lfRepresenting the distance of the center of mass to the front axle of the vehicle; lrRepresenting the distance of the center of mass to the rear axle of the vehicle; fyfIndicating the lateral force to which the front wheel tyre is subjected; fyrIndicating the lateral force to which the rear wheel tire is subjected;
12) during the tracking process of the vehicle, the tire is in a linear area, and the lateral force of the tire is approximately represented as:
Figure GDA0003327707550000134
Figure GDA0003327707550000135
in the formula, CfRepresenting tire front wheel side sheet stiffness; crRepresenting tire rear wheel cornering stiffness; alpha is alphafRepresenting a tire front wheel side slip angle; alpha is alpharIndicating a tire rear wheel side slip angle; fyfIndicating the lateral force to which the front wheel tyre is subjected; fyrIndicating the lateral force to which the rear wheel tire is subjected; beta represents the vehicle centroid slip angle; deltafIndicating a vehicle front wheel steering angle; lfRespectively representing the distances of the center of mass to the front axle of the vehicle; lrRepresenting the distance of the center of mass to the rear axis; v. ofxRepresenting vehicle longitudinal speed, ω representing vehicle yaw angular velocity;
13) in addition, vehicle system parameters can create uncertainties as certain changes occur in the motion state of the vehicle. Assuming that the actual values of the vehicle system parameters during trajectory tracking are known, the complete vehicle dynamics model is represented as:
Figure GDA0003327707550000136
Figure GDA0003327707550000137
Figure GDA0003327707550000138
in the formula, m represents the mass of the whole vehicle; v. ofxRepresenting a vehicle longitudinal speed; v. ofyRepresenting a vehicle lateral speed;
Figure GDA0003327707550000139
a differential representing a longitudinal speed of the vehicle;
Figure GDA00033277075500001310
a differential representing the lateral velocity of the vehicle; ω represents the yaw angular velocity of the vehicle;
Figure GDA00033277075500001311
represents the derivative of the yaw rate of the vehicle; fuxRepresenting an equivalent longitudinal force applied at the vehicle center of mass; beta represents the vehicle centroid slip angle; deltafIndicating a vehicle front wheel steering angle;
Figure GDA00033277075500001312
ρiactual values representing system parameters;
Figure GDA00033277075500001313
ideal values representing the variation of system parameters with the vehicle motion state; rhooiStandard values for system parameters are expressed and are expressed as:
Figure GDA0003327707550000141
in the formula, CwxRepresenting a longitudinal wind resistance coefficient of the vehicle; cwyRepresenting a lateral wind resistance coefficient of the vehicle; i iszRepresenting the moment of inertia of the vehicle; m represents the mass of the whole vehicle; lfRepresenting the distance of the center of mass to the front axle of the vehicle; lrRepresenting the distance of the center of mass to the rear axle of the vehicle; cfRepresenting tire front wheel cornering stiffness; crRepresenting tire rear wheel cornering stiffness;
referring to fig. 3, in order to obtain a trajectory tracking model, a kinematic model of the vehicle needs to be derived. FIG. 3 is a schematic view of trajectory tracking kinematics for an autonomous vehicle, wherein f1Represents the position, r, of the vehicle at the present moment3Representing the desired movement position, r, of the vehicle on the target trajectory2To a desired movement positionThe intersection of the normal of the velocity and the current motion position velocity direction.
14) The vehicle kinematic model is:
Figure GDA0003327707550000142
Figure GDA0003327707550000143
Figure GDA0003327707550000144
in the formula, xeIndicating a vehicle longitudinal tracking error; y iseIndicating a vehicle lateral tracking error;
Figure GDA0003327707550000145
a differential representing a longitudinal tracking error of the vehicle;
Figure GDA0003327707550000146
a differential representing a vehicle lateral tracking error; v. ofxdRepresenting a desired vehicle longitudinal speed; v. ofxRepresenting an actual vehicle longitudinal speed;
Figure GDA0003327707550000147
a differential representing an actual vehicle yaw angle;
Figure GDA0003327707550000148
a derivative representing a desired vehicle yaw angle;
Figure GDA0003327707550000149
representing an error between the desired yaw angle and the actual yaw angle;
Figure GDA00033277075500001410
representing the differential error between the desired yaw angle and the actual yaw angle; v. ofyRepresenting a vehicle lateral speed; omegadRepresenting a desired vehicle yaw angular velocity; omega represents the true vehicle yaw angular velocity; rρA road curvature representing a target trajectory;
15) deriving a vehicle kinematic model to obtain:
Figure GDA00033277075500001411
Figure GDA00033277075500001412
Figure GDA00033277075500001413
in the formula, xeIndicating a vehicle longitudinal tracking error; y iseIndicating a vehicle lateral tracking error;
Figure GDA0003327707550000151
a differential representing a longitudinal tracking error of the vehicle;
Figure GDA0003327707550000152
a differential representing a vehicle lateral tracking error;
Figure GDA0003327707550000153
a second derivative representing a longitudinal tracking error of the vehicle;
Figure GDA0003327707550000154
a second derivative representing a vehicle lateral tracking error; v. ofxdRepresenting a desired vehicle longitudinal speed;
Figure GDA0003327707550000155
a differential representing a desired vehicle longitudinal speed; v. ofxRepresenting a vehicle longitudinal speed;
Figure GDA0003327707550000156
a differential representing a longitudinal speed of the vehicle; v. ofyRepresenting a vehicle lateral speed;
Figure GDA0003327707550000157
a differential representing the lateral velocity of the vehicle;
Figure GDA0003327707550000158
a derivative representing a yaw angular velocity of the desired vehicle;
Figure GDA0003327707550000159
represents the derivative of true vehicle yaw angular velocity; ω represents the yaw angular velocity of the vehicle;
Figure GDA00033277075500001510
representing an error between the desired yaw angle and the actual yaw angle;
Figure GDA00033277075500001511
representing the differential error between the desired yaw angle and the actual yaw angle;
Figure GDA00033277075500001512
representing the error second derivative between the desired yaw angle and the actual yaw angle;
Figure GDA00033277075500001513
a second derivative representing an actual vehicle yaw angle;
Figure GDA00033277075500001514
a second derivative representing a desired vehicle yaw angle;
16) using longitudinal and lateral tracking errors as state variables of the system, i.e. x1=[xe ye]T
Figure GDA00033277075500001515
Figure GDA00033277075500001516
The equivalent longitudinal force applied at the vehicle's center of mass and the front wheel steering angle as control variables of the system, i.e.u=[Fuxδf]TSubstituting the vehicle dynamics model into the vehicle kinematics model to obtain a vehicle longitudinal and lateral coupling nonlinear trajectory tracking model containing system parameter uncertainty:
Figure GDA00033277075500001517
Figure GDA00033277075500001518
y=x1 (18)
in the formula, x1And x2State variables representing the system; u represents a control variable of the system; y represents the system output, F1(x1)=02×1Representing a first order system variable matrix; g1(x1)=I2×2Representing a first order system state matrix;
Figure GDA00033277075500001519
Figure GDA00033277075500001520
representing a second-order system variable matrix;
Figure GDA00033277075500001521
representing a second order system control matrix; p1And P2Is a system parameter matrix, f2,1(x)、g2,1(x) Representing the local basis function of the system, f2(x)、g2(x) And represents the system overall basis function:
P1=[ρ1 ρ2 ρ3 ρ4 ρ6 ρ7]T,P2=[ρ5 ρ8]T,g2(x)=[g2,2(x) g2,3(x)]T,
f2(x)=[f2,2(x) f2,3(x) f2,4(x) f2,5(x) f2,6(x) f2,7(x)]T,
Figure GDA0003327707550000161
Figure GDA0003327707550000162
Figure GDA0003327707550000163
Figure GDA0003327707550000164
in the formula, P1And P2Is a system parameter matrix, pi(i ═ 1,2, … 8) represents the true values of the system parameters; f. of2,j(x)(j=1,2,…7)、g2,k(x) (k ═ 1,2,3) represents the system local basis function; f. of2(x)、g2(x) Representing the system overall basis function; v. ofxRepresenting a vehicle longitudinal speed; v. ofyRepresenting a vehicle lateral speed; v. ofxdRepresenting a desired vehicle longitudinal speed;
Figure GDA0003327707550000165
a differential representing a desired vehicle longitudinal speed;
Figure GDA0003327707550000166
representing an error between the desired yaw angle and the actual yaw angle;
Figure GDA0003327707550000167
representing the differential error between the desired yaw angle and the actual yaw angle; ω represents the yaw angular velocity of the vehicle; x is the number ofeIndicating a vehicle longitudinal tracking error; y iseIndicating a vehicle lateral tracking error; beta represents the vehicle centroid slip angle; and m represents the mass of the whole vehicle.
Designing a vehicle longitudinal and lateral coupling track tracking controller based on a nonlinear three-step method theory to obtain a complete system control law; the three-step method track tracking controller consists of three parts of steady-state-like control, reference dynamic feedforward control and state-dependent error feedback control;
21) the system output y is derived until the occurrence of the control input u:
Figure GDA0003327707550000168
Figure GDA0003327707550000169
in the formula, x1And x2State variables representing the system;
Figure GDA00033277075500001610
representing a state variable differential of the system;
Figure GDA00033277075500001611
represents the differential of the system output;
Figure GDA00033277075500001612
represents the second derivative of the system output; f, F1(x1) Representing a first order system variable matrix; g1(x1) Representing a first order system state matrix; u represents a control variable of the system;
Figure GDA00033277075500001613
an output matrix representing the second order system output; b (x) ═ G1(x1)G2(x) A control matrix representing the second order system output; c (x) ═ G1(x1)F2(x) A parameter matrix representing the second order system output; f2(x) Representing a second-order system variable matrix; g2(x) Representing a second order system control matrix;
22) it is assumed that the system is already in steady state motion, at which point
Figure GDA0003327707550000171
Then the steady-state-like control law of the system is:
Figure GDA0003327707550000172
in the formula usRepresenting a steady-state-like control law of the system; g2(x) Representing a second order system control matrix; f2(x) Representing a second-order system variable matrix; f. of2,1(x)、g2,1(x) Representing a system local basis function; f. of2(x)、g2(x) Representing the system overall basis function; p1And P2Is a system parameter matrix;
23) adding a feedforward control law into a calibrated control law is used for improving the response performance of the system, namely:
u=us+uf (22)
wherein u represents a system control law; u. ofsSteady state-like control law, u, representing the systemfRepresenting the dynamic reference feedforward control law of the system.
Let y be yd
Figure GDA0003327707550000173
Substituting the control law (22) into the system (20) to obtain a feed forward control law as follows:
Figure GDA0003327707550000174
in the formula ufRepresenting a dynamic reference feedforward control law of the system; g2(x) Representing a second order system control matrix;
Figure GDA0003327707550000175
a differential representing a desired output of the system;
Figure GDA0003327707550000176
a second derivative representing the desired output of the system; a (x) represents the output moment of the second order system outputArraying; a (x) represents an output matrix of the second order system output; p2Is a system parameter matrix; g2,1(x) Representing a system local basis function; g2(x) Representing the system overall basis function;
24) considering modeling errors, external disturbance and other factors, the quasi-steady-state control law and the dynamic reference feedforward control law cannot completely eliminate the track tracking errors. Therefore, the error feedback control law continues to be introduced as:
u=us+uf+ue (24)
wherein u represents a system control law; u. ofsRepresenting a steady-state-like control law of the system; u. offRepresenting a dynamic reference feedforward control law of the system; u. ofeRepresenting the error feedback control law of the system;
defining a system tracking error as e1=yd-y, substituting the control law (24) into the system (20) can determine:
Figure GDA0003327707550000177
in the formula,
Figure GDA0003327707550000181
represents the system tracking error differential;
Figure GDA0003327707550000182
a second derivative representing a system tracking error; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; u. ofeRepresenting the error feedback control law of the system;
order to
Figure GDA0003327707550000183
The closed loop error system is then expressed as:
Figure GDA0003327707550000184
Figure GDA0003327707550000185
in the formula,
Figure GDA0003327707550000186
represents the system tracking error differential; e.g. of the type2Representing a virtual control input;
Figure GDA0003327707550000187
representing a virtual control input differential; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix, ueRepresenting the error feedback control law of the system;
25) due to the introduction of the quasi-steady-state control law and the reference dynamic feedforward control law, the closed-loop error system is simpler in structure. In order to obtain an error feedback control law, the method adopts a classic backstepping method to deduce the error feedback control law, and the closed loop stability of a track tracking system is ensured. Option e2Defining Lyapunov functions for virtual control inputs
Figure GDA0003327707550000188
Then the corresponding derivative is:
Figure GDA0003327707550000189
in the formula,
Figure GDA00033277075500001810
representing a defined first lyapunov function differential; e.g. of the type1Representing a system tracking error;
Figure GDA00033277075500001811
represents the system tracking error differential; e.g. of the type2Representing a virtual control input;
26) to ensure stability of the closed-loop control system, i.e.
Figure GDA00033277075500001812
The selected virtual control inputs are:
Figure GDA00033277075500001813
in the formula,
Figure GDA00033277075500001814
representing a desired virtual control input; e.g. of the type1Indicating the system tracking error, k1Representing a controller parameter;
for k1>0,
Figure GDA00033277075500001815
It is possible to obtain:
Figure GDA00033277075500001816
Figure GDA00033277075500001817
in the formula,
Figure GDA00033277075500001818
representing a defined first lyapunov function differential; k is a radical of1Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure GDA00033277075500001819
represents the system tracking error differential;
27) however, in the tracking process, it is difficult to fully implement
Figure GDA00033277075500001820
To e is making e2Approach to
Figure GDA00033277075500001821
To ensure the system e1→ 0, we define
Figure GDA00033277075500001822
Then we get:
Figure GDA0003327707550000191
Figure GDA0003327707550000192
in the formula,
Figure GDA0003327707550000193
representing the first defined lyapunov function differential, k1Representing the three-step controller parameters, e1And
Figure GDA0003327707550000194
respectively representing the systematic tracking error and the systematic tracking error differential, e3Representing a virtual control input error.
With e3→ 0, obtaining
Figure GDA0003327707550000195
Then system e1Gradual stabilization to error e3The derivation is carried out to obtain:
Figure GDA0003327707550000196
in the formula,
Figure GDA0003327707550000197
representing a virtual control input error differential; e.g. of the type2Representing an actual virtual control input;
Figure GDA0003327707550000198
representing a desired virtual control input differential;
Figure GDA0003327707550000199
representing a virtual control input differential; k is a radical of1Representing a controller parameter;
Figure GDA00033277075500001910
represents the system tracking error differential; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; u. ofeRepresenting the error feedback control law of the system;
28) definition includes error e3Lyapunov function of the interior
Figure GDA00033277075500001911
And (5) obtaining by derivation:
Figure GDA00033277075500001912
in the formula,
Figure GDA00033277075500001913
represents a defined second lyapunov function differential;
Figure GDA00033277075500001914
representing a defined first lyapunov function differential; e.g. of the type3Representing a virtual control input error;
Figure GDA00033277075500001915
representing a virtual control input error differential; k is a radical of1Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure GDA00033277075500001916
represents the system tracking error differential; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; u. ofeRepresenting the error feedback control law of the system.
According to the Lyapunov direct method, the error feedback control law is selected as follows:
Figure GDA00033277075500001917
in the formula ueRepresenting the error feedback control law of the system; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; k is a radical of1And k2Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure GDA00033277075500001918
represents the system tracking error differential; e.g. of the type3Representing a virtual control input error;
selection of k2>0, then
Figure GDA00033277075500001919
In the formula,
Figure GDA0003327707550000201
represents a defined second lyapunov function differential; k is a radical of1And k2Representing a controller parameter; e.g. of the type1Representing a system tracking error; e.g. of the type3Representing a virtual control input error;
29) this means that the error closed loop system is progressively stabilized, will (26), (29) and
Figure GDA0003327707550000202
and (36) obtaining the error feedback control law of practical application as follows:
Figure GDA0003327707550000203
in the formula ueRepresenting the error feedback control law of the system; a (x) an output matrix representing the output of the second order system, G2(x) Representing a second order system control matrix; k is a radical of1And k2Representing a three-step controller parameter; e.g. of the type1Presentation systemTracking errors;
Figure GDA0003327707550000204
represents the system tracking error differential; g2,1(x) Representing a system local basis function; g2(x) Representing the system overall basis function; p2Is a system parameter matrix;
thus far, the complete system control law obtained:
Figure GDA0003327707550000205
wherein u represents a system control law; u. ofsIs a system-like steady-state control law; u. offThe system dynamically refers to a feedforward control law; u. ofeRepresenting a system error feedback control law; f. ofP(x)=[G2(x)]-1(1+k1k2) Representing a scale term parameter; f. ofD(x)=[G2(x)]-1[k1+k2+A(x)]Representing a differential term parameter; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; k is a radical of1And k2Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure GDA0003327707550000206
representing the system tracking error differential.
Compensating system uncertainty disturbance caused by vehicle motion state change by combining with an adaptive law;
besides the need of processing the nonlinear coupling problem of the transverse and longitudinal dynamics, the vehicle track tracking controller has the system parameter true value rhoiUncertainty associated with ( i 1,2, …,8) changes in vehicle motion also interferes with trajectory tracking performance. Therefore, the adaptive control law is used for compensating the uncertainty problem of the system parameters, and the overall architecture is shown in FIG. 4.
31) Defining system parameter estimation values:
Figure GDA0003327707550000207
in the formula,
Figure GDA0003327707550000208
representing system parameter estimates;
Figure GDA0003327707550000209
an estimate representing a change in a system parameter with a vehicle motion state; rhooiStandard values representing system parameters;
32) the system control law is redefined as:
Figure GDA0003327707550000211
wherein u represents a system control input;
Figure GDA0003327707550000212
representing a second-order system variable matrix estimated value;
Figure GDA0003327707550000213
representing a second-order system control matrix estimated value;
Figure GDA0003327707550000214
P1and P2Is a system parameter matrix estimated value;
Figure GDA0003327707550000215
representing system parameter estimates;
Figure GDA0003327707550000216
a differential representing a desired output of the system;
Figure GDA0003327707550000217
a second derivative representing the desired output of the system;
Figure GDA0003327707550000218
an output matrix estimation value representing the output of the second-order system; e.g. of the type1Representing a system tracking error;
Figure GDA0003327707550000219
represents the system tracking error differential; k is a radical of1And k2Representing a controller parameter;
33) substituting the obtained system control law (41) into the system (20) to obtain:
Figure GDA00033277075500002110
in the formula,
Figure GDA00033277075500002126
represents the second derivative of the system output; k is a radical of1And k2Representing a controller parameter;
Figure GDA00033277075500002111
an output matrix estimation value representing the output of the second-order system; e.g. of the type1Representing a system tracking error;
Figure GDA00033277075500002112
represents the system tracking error differential; f2(x) The representation represents a second-order system variable matrix;
Figure GDA00033277075500002113
representing a second-order system variable matrix estimated value; g2(x) Representing a second order system control matrix;
Figure GDA00033277075500002114
representing a second-order system control matrix estimated value; u represents a system control input;
Figure GDA00033277075500002115
a second derivative representing the desired output of the system;
from the above equation, the closed-loop error system considering parameter uncertainty can be organized as:
Figure GDA00033277075500002116
wherein,
Figure GDA00033277075500002117
in the formula, k1And k2Representing a controller parameter;
Figure GDA00033277075500002118
an output matrix estimation value representing the output of the second-order system; e.g. of the type1Representing a system tracking error;
Figure GDA00033277075500002119
represents the system tracking error differential; Δ P represents the total error of the system parameter matrix; theta represents a system composition base; p1And P2Representing a system parameter matrix; delta P1And Δ P2Representing the system parameter matrix error;
Figure GDA00033277075500002120
an estimate representing a change in a system parameter with a vehicle motion state;
Figure GDA00033277075500002121
ideal values representing the variation of system parameters with the vehicle motion state; f. of2(x)、g2(x) Representing the system overall basis function; u represents a system control input;
34) selecting
Figure GDA00033277075500002122
Is the state variable of the error system, then:
Figure GDA00033277075500002123
in the formula, emIndicating the error systemA state variable of the system;
Figure GDA00033277075500002124
a state variable differential representing an error system;
Figure GDA00033277075500002125
Figure GDA0003327707550000221
a state variable parameter matrix representing an error system;
Figure GDA0003327707550000222
a parameter variable matrix representing an error system; theta represents a system composition base; Δ P represents the total error of the system parameter matrix; k is a radical of1And k2Representing a controller parameter;
35) defining a Lyapunov function including uncertainty of system parameters
Figure GDA0003327707550000223
Wherein Q>0 is a positive definite symmetric matrix, and the derivation is as follows:
Figure GDA0003327707550000224
in the formula,
Figure GDA0003327707550000225
represents a defined third lyapunov function differential; e.g. of the typemA state variable representing an error system; a. themA state variable parameter matrix representing an error system; q represents a positive definite symmetric matrix; b ismA parameter variable matrix representing an error system; theta represents a system composition base; Δ P represents the total error of the system parameter matrix;
Figure GDA0003327707550000226
representing the total error differential of the system parameter matrix; tau represents a parameter error variable parameter quantization parameter;
Figure GDA0003327707550000227
representing the system parameter adaptation law;
36) the system parameter self-adaptation law is taken as follows:
Figure GDA0003327707550000228
in the formula,
Figure GDA0003327707550000229
representing the system parameter adaptation law; tau represents a parameter error variable parameter quantization parameter; e.g. of the typemA state variable representing an error system; q represents a positive definite symmetric matrix; b ismA parameter variable matrix representing an error system, and theta represents a system combination base;
substituting the system parameter adaptation law into (45) to obtain:
Figure GDA00033277075500002210
in the formula,
Figure GDA00033277075500002211
represents a defined third lyapunov function differential; e.g. of the typemA state variable representing an error system; q represents a positive definite symmetric matrix; a. themA state variable parameter matrix representing an error system;
thus, only a suitable a needs to be selectedmAnd Q guarantee
Figure GDA00033277075500002212
Can make
Figure GDA00033277075500002213
Thus proving that the closed loop system is consistently bounded, i.e., limt→∞e1→0。
37) The following performs a system robustness analysis. In order to simplify problem analysis, factors such as parameter uncertainty, unmodeled disturbance and the like faced by the system are uniformly defined as xi, so that the original system control law is changed into:
u=uim+ξ (1)
in the formula, xi represents parameter uncertainty and unmodeled disturbance factors faced by the system; u. ofimRepresenting the original system control input; u represents a system control input;
substitution of (48) into (20) in combination with e1=yd-y is reduced to yield:
Figure GDA0003327707550000231
in the formula, e1Representing a system tracking error;
Figure GDA0003327707550000232
represents the system tracking error differential;
Figure GDA0003327707550000233
representing a system tracking error second derivative; k is a radical of1And k2Representing a controller parameter;
Figure GDA0003327707550000234
an output matrix estimation value representing the output of the second-order system; Δ P represents the total error of the system parameter matrix; delta P2Representing the system parameter matrix error; theta represents a system composition base; ξ represents the parameter uncertainty, unmodeled perturbation factor faced by the system.
Let d be Δ P2ξ, then the closed-loop error system is represented as:
Figure GDA0003327707550000235
in the formula, emA state variable representing an error system;
Figure GDA0003327707550000236
a state variable differential representing an error system; a. themState variable parameter moment representing error systemArraying; b ismA parameter variable matrix representing an error system; theta represents a system composition base; Δ P represents the total error of the system parameter matrix; d represents the overall disturbance faced by the system;
38) definition of
Figure GDA0003327707550000237
And gamma is>0, then Lyapunov function
Figure GDA0003327707550000238
The derivative of (c) is reduced to:
Figure GDA0003327707550000239
in the formula,
Figure GDA00033277075500002310
represents a defined third lyapunov function differential; e.g. of the typemA state variable representing an error system; a. themA state variable parameter matrix representing an error system; b ismA parameter variable matrix representing an error system; theta represents a system composition base; Δ P represents the total error of the system parameter matrix; d represents the overall disturbance faced by the system;
Figure GDA00033277075500002311
representing the system parameter adaptation law; tau represents a parameter error variable parameter quantization parameter; q represents a positive definite symmetric matrix; l represents a defined comparison matrix; γ represents a defined comparison matrix parameter quantization parameter.
In view of
Figure GDA00033277075500002312
Is a continuous positive function, and the error system (48) is input state stable for the comprehensive disturbance d faced by the system. Therefore, the system is robust to the uncertainty of the system parameters considered, unmodeled disturbances, etc.
And step four, realizing the track tracking control of the whole vehicle through a bottom layer control distribution strategy.
Equivalent longitudinal force F applied to vehicle centroid and obtained based on solution of trajectory tracking controlleruxCan not be directly applied to vehicle control, and needs to be decomposed by a bottom-layer control distribution strategy to obtain a driving torque signal T which can be responded by the vehicletqAnd a brake pressure signal.
Equivalent longitudinal force F when applied at the center of mass of the vehicleuxWhen the torque is greater than or equal to 0, the vehicle system is considered to be in the driving mode, and the corresponding driving torque is expressed as:
Figure GDA0003327707550000241
in the formula, TtqA signal indicative of a target drive torque of the vehicle; fuxRepresenting an equivalent longitudinal force applied at the vehicle center of mass; r represents a wheel rolling radius; i.e. i0Representing the whole equivalent transmission ratio of the whole vehicle; etaTThe whole equivalent transmission efficiency of the whole vehicle is represented;
equivalent longitudinal force F when applied at the center of mass of the vehicleuxLess than 0; considering the vehicle system in the drive mode, the corresponding drive torque can be expressed as:
Figure GDA0003327707550000242
wherein P represents a vehicle target master cylinder brake pressure; fuxRepresenting an equivalent longitudinal force applied at the vehicle center of mass; r represents a wheel rolling radius; d represents the diameter of the brake master cylinder; rBRepresents the effective brake caliper radius; i istRepresenting the moment of inertia of the tire;
Figure GDA0003327707550000243
representing the differential of the tire speed.
Examples
A joint simulation platform is built based on MATLAB/Simulink and vehicle dynamics software CarSim and used for testing the trajectory tracking controller designed by the application. The target vehicle was subjected to a double lane test at a varying longitudinal movement speed on a road surface having a road surface adhesion coefficient of 0.5. The target vehicle speed is between 45km/h and 85km/h, and is continuously transformed in a sine form. Fig. 5, 6, 7, 8, 9, 10, 11, and 12 are a longitudinal speed control performance curve, a longitudinal speed error control performance curve, a trajectory tracking coordinate axis control performance curve, a trajectory tracking lateral error control performance curve, a yaw angle error control performance curve, a front wheel corner control performance curve, and a yaw angle control performance curve, respectively. It can be seen from the experimental curve that the longitudinal and lateral coupling track tracking controller based on the adaptive three-step method can ensure that the longitudinal speed of the vehicle can follow well, and the error of the longitudinal speed is within 0.66 km/h. In the aspect of lateral track tracking, the lateral track tracking error is controlled within 0.05m, and the cross shoving error is controlled within 0.72 deg. The front wheel angle control in the whole track tracking process is stable, and the smoothness of the transverse swing angular speed of the whole vehicle is good. Therefore, the designed track tracking controller can realize stable, accurate and smooth control of the longitudinal and lateral track tracking motion of the vehicle.

Claims (4)

1. A design method for a vehicle longitudinal and lateral coupling trajectory tracking controller is characterized by comprising the following steps:
step one, establishing a track tracking model containing system parameter uncertainty and vehicle longitudinal and lateral nonlinear coupling dynamics characteristic relation according to the kinematics and dynamics relation between a vehicle and an expected track;
designing a track tracking controller coupled in the longitudinal direction and the lateral direction of the vehicle to obtain a complete system control law; the trajectory tracking controller consists of three parts of steady-state-like control, reference dynamic feedforward control and state-dependent error feedback control;
compensating system uncertainty disturbance caused by vehicle motion state change by combining with an adaptive law;
fourthly, track tracking control of the whole vehicle is realized through a bottom layer control distribution strategy;
the specific method of the first step is as follows:
11) assuming that the left wheel and the right wheel are stressed symmetrically, a simplified vehicle dynamic model is established as follows:
Figure FDA0003327707540000011
Figure FDA0003327707540000012
Figure FDA0003327707540000013
in the formula, m represents the mass of the whole vehicle; v. ofxRepresenting a vehicle longitudinal speed; v. ofyRepresenting a vehicle lateral speed;
Figure FDA0003327707540000014
a differential representing a longitudinal speed of the vehicle;
Figure FDA0003327707540000015
a differential representing the lateral velocity of the vehicle; ω represents the vehicle yaw rate;
Figure FDA0003327707540000016
a differential representing a yaw rate of the vehicle; fuxRepresenting an equivalent longitudinal force applied at the vehicle center of mass; cwxRepresenting a longitudinal wind resistance coefficient of the vehicle; cwyRepresenting a lateral wind resistance coefficient of the vehicle; i iszRepresenting the moment of inertia of the vehicle; lfRepresenting the distance of the center of mass to the front axle of the vehicle; lrRepresenting the distance of the center of mass to the rear axle of the vehicle; fyfIndicating the lateral force to which the front wheel tyre is subjected; fyrIndicating the lateral force to which the rear wheel tire is subjected;
12) during the tracking process of the vehicle, the tire is in a linear area, and the lateral force of the tire is approximately represented as:
Figure FDA0003327707540000017
Figure FDA0003327707540000021
in the formula, CfRepresenting tire front wheel side sheet stiffness; crRepresenting tire rear wheel cornering stiffness; alpha is alphafRepresenting a tire front wheel side slip angle; alpha is alpharIndicating a tire rear wheel side slip angle; beta represents the vehicle centroid slip angle; deltafIndicating a vehicle front wheel steering angle;
13) assuming that the actual values of the vehicle system parameters during trajectory tracking are known, the complete vehicle dynamics model is represented as:
Figure FDA0003327707540000022
Figure FDA0003327707540000023
Figure FDA0003327707540000024
in the formula,
Figure FDA0003327707540000025
ρiactual values representing system parameters;
Figure FDA0003327707540000026
ideal values representing the variation of system parameters with the vehicle motion state; rhooiStandard values for system parameters are expressed and are expressed as:
Figure FDA0003327707540000027
in the formula, CwyRepresenting a lateral wind resistance coefficient of the vehicle;
14) the vehicle kinematic model is:
Figure FDA0003327707540000028
Figure FDA0003327707540000029
Figure FDA00033277075400000210
in the formula, xeIndicating a vehicle longitudinal tracking error; y iseIndicating a vehicle lateral tracking error;
Figure FDA00033277075400000211
a differential representing a longitudinal tracking error of the vehicle;
Figure FDA00033277075400000212
a differential representing a vehicle lateral tracking error; v. ofxdRepresenting a desired vehicle longitudinal speed;
Figure FDA00033277075400000213
a differential representing an actual vehicle yaw angle;
Figure FDA00033277075400000214
a derivative representing a desired vehicle yaw angle;
Figure FDA00033277075400000215
representing an error between the desired yaw angle and the actual yaw angle;
Figure FDA0003327707540000031
representing the differential error between the desired yaw angle and the actual yaw angle; omegadRepresenting a desired vehicle yaw rate; rρA road curvature representing a target trajectory;
15) deriving a vehicle kinematic model to obtain:
Figure FDA0003327707540000032
Figure FDA0003327707540000033
Figure FDA0003327707540000034
in the formula,
Figure FDA0003327707540000035
a second derivative representing a longitudinal tracking error of the vehicle;
Figure FDA0003327707540000036
a second derivative representing a vehicle lateral tracking error;
Figure FDA0003327707540000037
a differential representing a desired vehicle longitudinal speed;
Figure FDA0003327707540000038
a derivative representing a desired vehicle yaw rate;
Figure FDA0003327707540000039
representing the second derivative of the error between the desired yaw angle and the actual yaw angle;
Figure FDA00033277075400000310
a second derivative representing an actual vehicle yaw angle;
Figure FDA00033277075400000311
a second derivative representing a desired vehicle yaw angle;
16) using longitudinal and lateral tracking errors as state variables of the system, i.e. x1=[xe ye]T
Figure FDA00033277075400000312
The equivalent longitudinal force applied at the vehicle center of mass and the front wheel steering angle serve as control variables of the system, i.e. u ═ Fux δf]TSubstituting the vehicle dynamics model into the vehicle kinematics model to obtain a vehicle longitudinal and lateral coupling nonlinear trajectory tracking model containing system parameter uncertainty:
Figure FDA00033277075400000313
Figure FDA00033277075400000314
y=x1 (18)
in the formula, x1And x2State variables representing the system; u represents a control variable of the system; y represents the system output, F1(x1)=02 ×1Representing a first order system variable matrix; g1(x1)=I2×2Representing a first order system state matrix;
Figure FDA00033277075400000315
representing a second-order system variable matrix;
Figure FDA00033277075400000316
Figure FDA00033277075400000317
representing a second order system control matrix; p1And P2Is a system parameter matrix, f2,1(x)、g2,1(x) Representing the local basis function of the system, f2(x)、g2(x) And represents the system overall basis function:
P1=[ρ1 ρ2 ρ3 ρ4 ρ6 ρ7]T,P2=[ρ5 ρ8]T,g2(x)=[g2,2(x) g2,3(x)]T
f2(x)=[f2,2(x) f2,3(x) f2,4(x) f2,5(x) f2,6(x) f2,7(x)]T
Figure FDA0003327707540000041
Figure FDA0003327707540000042
Figure FDA0003327707540000043
Figure FDA0003327707540000044
in the formula, P1And P2Is a system parameter matrix, pi1,2, … 8, representing the true value of the system parameter; f. of2,j(x),j=1,2,…7,、g2,k(x) K is 1,2,3, representing the system local basis function; f. of2(x)、g2(x) Representing the overall basis function of the system;
Figure FDA0003327707540000045
Representing the derivative of the desired vehicle longitudinal speed.
2. The design method of the vehicle longitudinal and lateral coupling track following controller according to claim 1, wherein the specific method of the second step is as follows:
21) the system output y is derived until the occurrence of the control input u:
Figure FDA0003327707540000046
Figure FDA0003327707540000047
in the formula, x1And x2State variables representing the system;
Figure FDA0003327707540000048
representing a state variable differential of the system;
Figure FDA0003327707540000049
represents the differential of the system output;
Figure FDA00033277075400000410
represents the second derivative of the system output; f, F1(x1) Representing a first order system variable matrix; g1(x1) Representing a first order system state matrix; u represents a control variable of the system;
Figure FDA00033277075400000411
Figure FDA00033277075400000412
representing outputs of a second order systemMatrix generation; b (x) ═ G1(x1)G2(x) A control matrix representing the second order system output; c (x) ═ G1(x1)F2(x) A parameter matrix representing the second order system output; f2(x) Representing a second-order system variable matrix; g2(x) Representing a second order system control matrix;
22) it is assumed that the system is already in steady state motion, at which point
Figure FDA00033277075400000413
Then the steady-state-like control law of the system is:
Figure FDA0003327707540000051
in the formula usRepresenting a steady-state-like control law of the system; g2(x) Representing a second order system control matrix; f2(x) Representing a second-order system variable matrix; f. of2,1(x)、g2,1(x) Representing a system local basis function; f. of2(x)、g2(x) Representing the system overall basis function; p1And P2Is a system parameter matrix;
23) adding a feedforward control law into a calibrated control law is used for improving the response performance of the system, namely:
u=us+uf (22)
wherein u represents a system control law; u. ofsSteady state-like control law, u, representing the systemfRepresenting a dynamic reference feedforward control law of the system;
let y be yd
Figure FDA0003327707540000052
Substituting the control law (22) into the system (20) to obtain a feed forward control law as follows:
Figure FDA0003327707540000053
in the formula ufRepresenting a dynamic reference feedforward control law of the system; g2(x) Representing a second order system control matrix;
Figure FDA0003327707540000054
a differential representing a desired output of the system;
Figure FDA0003327707540000055
a second derivative representing the desired output of the system; a (x) represents an output matrix of the second order system output; a (x) represents an output matrix of the second order system output; p2Is a system parameter matrix; g2,1(x) Representing a system local basis function; g2(x) Representing the system overall basis function;
24) the introduced error feedback control law is as follows:
u=us+uf+ue (24)
wherein u represents a system control law; u. ofsRepresenting a steady-state-like control law of the system; u. offRepresenting a dynamic reference feedforward control law of the system; u. ofeRepresenting the error feedback control law of the system;
defining a system tracking error as e1=yd-y, substituting the control law (24) into the system (20) can determine:
Figure FDA0003327707540000056
in the formula,
Figure FDA0003327707540000061
represents the system tracking error differential;
Figure FDA0003327707540000062
a second derivative representing a system tracking error; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; u. ofeRepresenting the error feedback control law of the system;
order to
Figure FDA0003327707540000063
The closed loop error system is then expressed as:
Figure FDA0003327707540000064
Figure FDA0003327707540000065
in the formula,
Figure FDA0003327707540000066
represents the system tracking error differential; e.g. of the type2Representing a virtual control input;
Figure FDA0003327707540000067
representing a virtual control input differential; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix, ueRepresenting the error feedback control law of the system;
25) option e2Defining Lyapunov functions for virtual control inputs
Figure FDA0003327707540000068
Then the corresponding derivative is:
Figure FDA0003327707540000069
in the formula,
Figure FDA00033277075400000610
representing a defined first lyapunov function differential; e.g. of the type1Representing a system tracking error;
Figure FDA00033277075400000611
represents the system tracking error differential; e.g. of the type2Representing a virtual control input;
26) to ensure stability of the closed-loop control system, i.e.
Figure FDA00033277075400000612
The selected virtual control inputs are:
Figure FDA00033277075400000613
in the formula,
Figure FDA00033277075400000614
representing a desired virtual control input; e.g. of the type1Indicating the system tracking error, k1Representing a controller parameter;
for k1>0,
Figure FDA00033277075400000615
It is possible to obtain:
Figure FDA00033277075400000616
Figure FDA00033277075400000617
in the formula,
Figure FDA00033277075400000618
representing a defined first lyapunov function differential; k is a radical of1Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure FDA00033277075400000619
represents the system tracking error differential;
27) to e is making e2Approach to
Figure FDA0003327707540000071
To ensure the system e1→ 0, we define
Figure FDA0003327707540000072
Then we get:
Figure FDA0003327707540000073
Figure FDA0003327707540000074
in the formula,
Figure FDA0003327707540000075
representing the first defined lyapunov function differential, k1Representing the three-step controller parameters, e1And
Figure FDA0003327707540000076
respectively representing the systematic tracking error and the systematic tracking error differential, e3Representing a virtual control input error;
with e3→ 0, obtaining
Figure FDA0003327707540000077
Then system e1Gradual stabilization to error e3The derivation is carried out to obtain:
Figure FDA0003327707540000078
in the formula,
Figure FDA0003327707540000079
representing virtual control input errorsDifferentiating; e.g. of the type2Representing an actual virtual control input;
Figure FDA00033277075400000710
representing a desired virtual control input differential;
Figure FDA00033277075400000711
representing a virtual control input differential; k is a radical of1Representing a controller parameter;
Figure FDA00033277075400000712
represents the system tracking error differential; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; u. ofeRepresenting the error feedback control law of the system;
28) definition includes error e3Lyapunov function of the interior
Figure FDA00033277075400000713
And (5) obtaining by derivation:
Figure FDA00033277075400000714
in the formula,
Figure FDA00033277075400000715
represents a defined second lyapunov function differential;
Figure FDA00033277075400000716
representing a defined first lyapunov function differential; e.g. of the type3Representing a virtual control input error;
Figure FDA00033277075400000717
representing a virtual control input error differential; k is a radical of1Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure FDA00033277075400000718
represents the system tracking error differential; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; u. ofeRepresenting the error feedback control law of the system;
according to the Lyapunov direct method, the error feedback control law is selected as follows:
Figure FDA00033277075400000719
in the formula ueRepresenting the error feedback control law of the system; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; k is a radical of1And k2Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure FDA0003327707540000081
represents the system tracking error differential; e.g. of the type3Representing a virtual control input error;
selection of k2> 0, then
Figure FDA0003327707540000082
In the formula,
Figure FDA0003327707540000083
represents a defined second lyapunov function differential; k is a radical of1And k2Representing a controller parameter; e.g. of the type1Representing a system tracking error; e.g. of the type3Representing a virtual control input error;
29) the error closed loop system is gradually stabilized, and (26), (29) and
Figure FDA0003327707540000084
and (36) obtaining the error feedback control law of practical application as follows:
Figure FDA0003327707540000085
in the formula ueRepresenting the error feedback control law of the system; a (x) an output matrix representing the output of the second order system, G2(x) Representing a second order system control matrix; k is a radical of1And k2Representing a three-step controller parameter; e.g. of the type1Representing a system tracking error;
Figure FDA0003327707540000086
represents the system tracking error differential; g2,1(x) Representing a system local basis function; g2(x) Representing the system overall basis function; p2Is a system parameter matrix;
the obtained complete system control law:
Figure FDA0003327707540000087
wherein u represents a system control law; u. ofsIs a system-like steady-state control law; u. offThe system dynamically refers to a feedforward control law; u. ofeRepresenting a system error feedback control law; f. ofP(x)=[G2(x)]-1(1+k1k2) Representing a scale term parameter; f. ofD(x)=[G2(x)]-1[k1+k2+A(x)]Representing a differential term parameter; a (x) represents an output matrix of the second order system output; g2(x) Representing a second order system control matrix; k is a radical of1And k2Representing a controller parameter; e.g. of the type1Representing a system tracking error;
Figure FDA0003327707540000088
representing the system tracking error differential.
3. The design method of the vehicle longitudinal and lateral coupling track following controller according to claim 1, wherein the specific method of the third step is as follows:
31) defining system parameter estimation values:
Figure FDA0003327707540000091
in the formula,
Figure FDA0003327707540000092
representing system parameter estimates;
Figure FDA0003327707540000093
an estimate representing a change in a system parameter with a vehicle motion state; rhooiStandard values representing system parameters;
32) the system control law is redefined as:
Figure FDA0003327707540000094
wherein u represents a system control input;
Figure FDA0003327707540000095
representing a second-order system variable matrix estimated value;
Figure FDA0003327707540000096
representing a second-order system control matrix estimated value;
Figure FDA0003327707540000097
Figure FDA0003327707540000098
P1and P2Is a system parameter matrix estimated value;
Figure FDA0003327707540000099
representing system parameter estimatesA value;
Figure FDA00033277075400000910
a differential representing a desired output of the system;
Figure FDA00033277075400000911
a second derivative representing the desired output of the system;
Figure FDA00033277075400000912
an output matrix estimation value representing the output of the second-order system; e.g. of the type1Representing a system tracking error;
Figure FDA00033277075400000913
represents the system tracking error differential; k is a radical of1And k2Representing a controller parameter;
33) by substituting the obtained system control law (41) into the system (20), the following can be obtained:
Figure FDA00033277075400000914
in the formula,
Figure FDA00033277075400000915
represents the second derivative of the system output; k is a radical of1And k2Representing a controller parameter;
Figure FDA00033277075400000916
an output matrix estimation value representing the output of the second-order system; e.g. of the type1Representing a system tracking error;
Figure FDA00033277075400000917
represents the system tracking error differential; f2(x) The representation represents a second-order system variable matrix;
Figure FDA00033277075400000918
representing a second-order system variable matrix estimated value; g2(x) Representing a second order system control matrix;
Figure FDA00033277075400000919
representing a second-order system control matrix estimated value; u represents a system control input;
Figure FDA00033277075400000920
a second derivative representing the desired output of the system;
from the above equation, the closed-loop error system considering parameter uncertainty can be organized as:
Figure FDA00033277075400000921
wherein,
Figure FDA0003327707540000101
in the formula, k1And k2Representing a controller parameter;
Figure FDA0003327707540000102
an output matrix estimation value representing the output of the second-order system; e.g. of the type1Representing a system tracking error;
Figure FDA0003327707540000103
represents the system tracking error differential; Δ P represents the total error of the system parameter matrix; theta represents a system composition base; p1And P2Representing a system parameter matrix; delta P1And Δ P2Representing the system parameter matrix error;
Figure FDA0003327707540000104
an estimate representing a change in a system parameter with a vehicle motion state;
Figure FDA0003327707540000105
ideal values representing the variation of system parameters with the vehicle motion state; f. of2(x)、g2(x) Representing the system overall basis function; u represents a system control input;
34) selecting
Figure FDA0003327707540000106
Is the state variable of the error system, then:
Figure FDA0003327707540000107
in the formula, emA state variable representing an error system;
Figure FDA0003327707540000108
a state variable differential representing an error system;
Figure FDA0003327707540000109
a state variable parameter matrix representing an error system;
Figure FDA00033277075400001010
a parameter variable matrix representing an error system; theta represents a system composition base; Δ P represents the total error of the system parameter matrix; k is a radical of1And k2Representing a controller parameter;
35) defining a Lyapunov function including uncertainty of system parameters
Figure FDA00033277075400001011
Wherein Q > 0 is a positive definite symmetric matrix, and the derivation is as follows:
Figure FDA00033277075400001012
in the formula,
Figure FDA00033277075400001013
represents a defined third lyapunov function differential; e.g. of the typemA state variable representing an error system; a. themA state variable parameter matrix representing an error system; q represents a positive definite symmetric matrix; b ismA parameter variable matrix representing an error system; theta represents a system composition base; Δ P represents the total error of the system parameter matrix;
Figure FDA00033277075400001014
representing the total error differential of the system parameter matrix; tau represents a parameter error variable parameter quantization parameter;
Figure FDA0003327707540000111
representing the system parameter adaptation law;
36) the system parameter self-adaptation law is taken as follows:
Figure FDA0003327707540000112
in the formula,
Figure FDA0003327707540000113
representing the system parameter adaptation law; tau represents a parameter error variable parameter quantization parameter; e.g. of the typemA state variable representing an error system; q represents a positive definite symmetric matrix; b ismA parameter variable matrix representing an error system, and theta represents a system combination base;
substituting the system parameter adaptation law into (45) to obtain:
Figure FDA0003327707540000114
in the formula,
Figure FDA0003327707540000115
represents a defined third lyapunov function differential; e.g. of the typemA state variable representing an error system; q represents a positive definite symmetric matrix; a. themA state variable parameter matrix representing an error system.
4. The design method of the vehicle longitudinal and lateral coupling track following controller according to claim 1, wherein the specific method of the fourth step is as follows:
equivalent longitudinal force F applied to vehicle centroid and obtained based on solution of trajectory tracking controlleruxCan not be directly applied to vehicle control, and needs to be decomposed by a bottom-layer control distribution strategy to obtain a driving torque signal T which can be responded by the vehicletqAnd a brake pressure signal;
equivalent longitudinal force F when applied at the center of mass of the vehicleuxWhen the torque is greater than or equal to 0, the vehicle system is considered to be in the driving mode, and the corresponding driving torque is expressed as:
Figure FDA0003327707540000116
in the formula, TtqA signal indicative of a target drive torque of the vehicle; fuxRepresenting an equivalent longitudinal force applied at the vehicle center of mass; r represents a wheel rolling radius; i.e. i0Representing the whole equivalent transmission ratio of the whole vehicle; etaTThe whole equivalent transmission efficiency of the whole vehicle is represented;
equivalent longitudinal force F when applied at the center of mass of the vehicleuxLess than 0; considering the vehicle system in the drive mode, the corresponding drive torque can be expressed as:
Figure FDA0003327707540000121
wherein P represents a vehicle target master cylinder brake pressure; fuxRepresenting an equivalent longitudinal force applied at the vehicle center of mass; r represents a wheel rolling radius; d represents the diameter of the brake master cylinder; rBRepresents the effective brake caliper radius; i istRepresenting the moment of inertia of the tire;
Figure FDA0003327707540000122
representing the differential of the tire speed.
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