CN106094842B - A kind of UUV diving plane H based on T-S model and PDC∞Control method - Google Patents

A kind of UUV diving plane H based on T-S model and PDC∞Control method Download PDF

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CN106094842B
CN106094842B CN201610487739.9A CN201610487739A CN106094842B CN 106094842 B CN106094842 B CN 106094842B CN 201610487739 A CN201610487739 A CN 201610487739A CN 106094842 B CN106094842 B CN 106094842B
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张勋
李昀澄
凌飞
周佳加
陈涛
张宏瀚
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Harbin Engineering University
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    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04Control of altitude or depth
    • G05D1/06Rate of change of altitude or depth
    • G05D1/0692Rate of change of altitude or depth specially adapted for under-water vehicles

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Abstract

The invention belongs to underwater moving body control technology fields, and in particular to a kind of UUV diving plane H based on T-S model and PDCControl method.The present invention includes establishing UUV diving plane model, including the deep-controlled model of UUV and UUV trim Controlling model;It is modeled using depth and trim system of the T-S model to UUV;H is designed based on parallel distributed compensation PDC methodController;With the dive for the method control UUV that depth-trim coordinated control deepens, to guarantee that Angle of Trim meets design requirement.Diving plane H is designed by establishing the depth and trim model of the UUV based on T-S model, and based on parallel distributed compensation (PDC) methodController, using the dive for the method control UUV that depth-trim coordinated control deepens, Angle of Trim is excessive during solving the problems, such as UUV dive, to guarantee the safety of UUV operation.

Description

A kind of UUV diving plane H based on T-S model and PDC∞Control method
Technical field
The invention belongs to underwater moving body control technology fields, and in particular to a kind of UUV based on T-S model and PDC is vertical Face movement H directlyControl method.
Background technique
UAV navigation (UnmannedUnderwaterVehicle, UUV) is a kind of based on the small-sized of new and high technology Underwater self-propelled carrier can complete specific underwater operation task by way of remote control or autonomous operation.It can be with using UUV Carry out deep-sea exploration, marine resources development, the tasks such as raising of a wreck and the investigation of military harbour tactics.Though diving plane It is so a special case of UUV spatial movement, but its key for completing mission task, UUV diving plane is controlled The research of problem suffers from important meaning in terms of theoretical Research And Engineering practice.The movement of UUV have it is serious non-linear, And the speed of a ship or plane is frequently necessary to change.It is required with UUV intelligence and control accuracy requirement and to extraneous interference rejection capability Improve, UUV movement control technology is also faced with huge challenge, the control algolithms of some classics due to itself limitation It is not able to satisfy the high-precision control to UUV.
Document " the H based on LMIApplication of the filter in the control of UUV trim " (Shipbuilding of China, 2013, volume 54 the 4 phases) based on LMI method be UUV pitching control system devise an optimal robustness HFilter, then, using special Bilinear transformation method solves in the imaginary axis of UUV pitching control system equation that there are poles to be unsatisfactory for filter design condition Problem.Finally by the robust H of designFilter is applied to UUV pitching control system, however document is specific there is no establishing The T-S model of UUV vertical plane, but trim control problem is solved by the robustness of filter, the control that the present invention takes Method is essentially different with it.
Document " Research on Comprehensive Control Technology of latent device diving plane " (Harbin Engineering University's master thesis, 2008.) the excessive problem of Angle of Trim during UUV dive is had studied, and using Sliding Mode Controller in UUV dive process Middle addition Angle of Trim judgment module, to realize the limitation to Angle of Trim during dive, but the not control to depth and trim Coordination switching is carried out, the present invention uses HDepth controller controls the depth of UUV, while Angle of Trim is added and judges mould Block realizes the switching of deep-controlled and trim control, can depth-trim to UUV dive process carry out coordinated control.
Summary of the invention
It can be in UUV the object of the present invention is to provide one kind and become the speed of a ship or plane and in the case where by ocean current interference, The UUV diving plane H based on T-S model and PDC that the movement of UUV vertical plane is controlledControl method.
The object of the present invention is achieved like this:
(1) UUV diving plane model, including the deep-controlled model of UUV and UUV trim Controlling model are established;
UUV diving plane model is
Vertical equation:
Trim equation:
Posture equation:
Movement relation formula:
In formula, m is UUV mass;L is the length of UUV;ρ is density of sea water;B is buoyancy suffered by UUV;U, v, w UUV Longitudinally, laterally with vertical component velocity;Q, p, r are UUV trim, heel and vertical angular speed;X, y, z be UUV surging, swaying and Heaving displacement;xG、yG、zGLongitudinally, laterally and vertical center gravity for UUV;φ is UUV roll angle, θ is UUV Angle of Trim, ψ is UUV bow Cradle angle;δsFor hydroplane rudder angle;X, Y, Z be UUV longitudinally, laterally with vertical active force;K, M, N be UUV longitudinally, laterally with it is vertical Opplied moment;Z′(·)、M′(·)For zero dimension hydrodynamic force coefficient, I(·)For under hull coordinate system to the rotary inertia of axis;Center of gravity with Centre of buoyancy coordinate is respectively (0,0,0), (0,0, zB);J be UUV to origin not in the inertia matrix of barycentric coordinate system,
(2) it is modeled using depth and trim system of the T-S model to UUV;
UUV depth and pitching control system contain the state space description of the nonlinear system of disturbance are as follows:
In formula, x (t) ∈ RnFor state variable;u(t)∈RmTo control input variable;w(t)∈Rq,w(t)∈L2(R) it is External disturbance;F (t) is nonlinear function;
The vertical face system of above-mentioned UUV is approached with following T-S fuzzy system, rule is as follows:
Ri:if ξ1(t) is Mi1 and ξ2(t) is Mi2...andξp(t) is Mip
then
Z (t)=Cx (t)+Du (t)
In formula, ξi(t), i=1,2 ..., the former piece variable of r fuzzy rule;Mij(j=1,2 ..., p) it is fuzzy set;r For rule number;(Ai,Bi, H) be the corresponding dimension of i-th of subsystem matrix;RiFor the i-th rule of fuzzy system;C, D are Controlled output phase answers the matrix of dimension, obtains the Global fuzzy model of the vertical face system of UUV:
Z (t)=Cx (t)+Du (t)
Wherein,
βi(ξ (t)) indicates that ξ (t) belongs to fuzzy set MijMembership function, while also illustrating that the relevance grade of the i-th rule; hi(ξ (t)) indicates standardization subordinating degree function;
(3) H is designed based on parallel distributed compensation PDC methodController;
Fuzzy system are as follows:
Obtain fuzzy domination structure:
Ri:if ξ1(t) is Mi1 and...ξp(t) is Mip
Then u (t)=KiX (t), i=1,2 ..., r;
Global system fuzzy controller are as follows:
Closed-loop system are as follows:
Wherein,
(4) dive of the method control UUV deepened with depth-trim coordinated control, to guarantee that Angle of Trim meets design It is required that.
The beneficial effects of the present invention are: depth and trim model by establishing the UUV based on T-S model, and base Diving plane H is designed in parallel distributed compensation (PDC) methodController, the method deepened using depth-trim coordinated control The dive of UUV is controlled, Angle of Trim is excessive during solving the problems, such as UUV dive, to guarantee the safety of UUV operation.
Detailed description of the invention
Fig. 1 UUV diving plane controls hardware structure diagram;
Fig. 2 UUV depth control system schematic diagram;
Fig. 3 UUV pitching control system schematic diagram;
Fig. 4 PDC schematic diagram;
Fig. 5 UUV depth-trim coordinated control flow chart.
Specific embodiment
The present invention is described in more detail with reference to the accompanying drawing.
The invention discloses a kind of based on T-S model and PDC (Parallel Distributed Compensation) UUV (Unmanned Underwater Vehicle) diving plane HControl method, its object is to be in become for UUV Speed of a ship or plane work characteristics and in the case of by ocean current interference, controls the movement of UUV vertical plane.Firstly, utilizing T-S model pair The depth and pitching control system of UUV is approached;Then, LMI (Linear Matrix is utilized based on PDC method Inequality H) is designedController;Finally, the problem excessive for UUV dive process Angle of Trim, utilizes the H of designIt is deep It spends controller and trim controller and carries out the coordinated control of depth trim, the present invention is for can be preferable in the speed of a ship or plane section of setting It realizes depth and trim control, there is preferable dynamic property, and utilize the H of designDepth controller and trim controller into Trim coordinated control deepens method to row depth-can effectively reduce the Angle of Trim of UUV dive process, guarantees the safety of aircraft.
A kind of UUV diving plane H based on T-S model and PDC of the present inventionThe working principle of control method: Motion control computer calculates the pitch angle of UUV, speed of a ship or plane original state input T-S model after receiving control instruction State feedback factor inputs the H designed based on PDCController utilizes HDepth controller controls the depth of UUV, together When be added Angle of Trim judgment module: when Angle of Trim be greater than design requirement when, from HIt is deep-controlled to switch to HTrim control, when vertical When inclination angle is not more than design requirement, then H is switched back intoIt is deep-controlled.It specifically includes:
1 establishes UUV diving plane model, including the deep-controlled model of UUV and UUV trim Controlling model;
2 are modeled using depth and trim system of the T-S model to UUV;
3 design H based on parallel distributed compensation (PDC) methodController;
The dive of the 4 method control UUV deepened with depth-trim coordinated control, is wanted with guaranteeing that Angle of Trim meets design It asks.
1, a kind of to be described based on the UUV vertical plane of T-S fuzzy model and PDC control specific implementation step in conjunction with Fig. 5 Are as follows:
1) user inputs the desired depth of UUV;
2) deep-controlled, motion control computer reception desired depth instruction, in conjunction with the initial shape of sensor feedback is carried out State information input T-S fuzzy model solves controller state feedback factor.
3) real time status information that controller is fed back by resolving current sensor, output rudder angle control instruction;
4) when steering engine executes control instruction, if Angle of Trim is not above limitation, UUV is continued to run until reaching desired depth And controlling depth is exported, need to carry out trim control if Angle of Trim is more than limitation and goes to step 2.It is thusly-formed closed-loop control System realizes the deep-controlled and trim control of UUV vertical plane.
2, the deep-controlled and trim control of UUV vertical plane contains the building, based on T-S model foundation of hardware configuration UUV depth and trim model, diving plane HThe resolving of controller, in conjunction with attached drawing to the detailed description of the present invention:
In conjunction with Fig. 1, the UUV diving plane built controls hardware structure diagram.Doppler log, programmable movements control Device, depth transducer, attitude transducer form the sensing system of UUV vertical plane;ARM and motion control computer form UUV The controller system of vertical plane;The executing agency of Programmable Multi-Axis Controller and hydroplane composition UUV vertical plane.Sensing system Pitch angle, the speed of a ship or plane, depth information are provided, these information are sent to motion control computer by serial ports.Motion control computer Carry out corresponding analog-to-digital conversion after receiving the data and clear out rudder angle instruction, while by Ethernet output rudder angle instruct to The depth and Angle of Trim of actuating mechanism controls UUV are controlled after ARM.
3, in conjunction with Fig. 2 and Fig. 3, UUV diving plane model, including the deep-controlled model of UUV and the control of UUV trim are established Model.
Due to the symmetry of UUV structure, it is assumed that the origin of hull coordinate system is located at the center of gravity of UUV, with reference to six degree of freedom mould Type can obtain shown in UUV diving plane model such as formula (1)~formula (4).
Vertical equation:
Trim equation:
Posture equation:
Movement relation formula:
In formula, m is UUV mass;L is the length of UUV;ρ is density of sea water;B is buoyancy suffered by UUV;U, v, w UUV Longitudinally, laterally with vertical component velocity;Q, p, r are UUV trim, heel and vertical angular speed;X, y, z be UUV surging, swaying and Heaving displacement;xG、yG、zGLongitudinally, laterally and vertical center gravity for UUV;φ is UUV roll angle, θ is UUV Angle of Trim, ψ is UUV bow Cradle angle;δsFor hydroplane rudder angle;X, Y, Z be UUV longitudinally, laterally with vertical active force;K, M, N be UUV longitudinally, laterally with it is vertical Opplied moment;Z′(·)、M′(·)For zero dimension hydrodynamic force coefficient, I(·)For under hull coordinate system to the rotary inertia of axis;Center of gravity with Centre of buoyancy coordinate is respectively (0,0,0), (0,0, zB);J be UUV to origin not in the inertia matrix of barycentric coordinate system,
For the ease of the design of controller, simplification appropriate is carried out to the depth of UUV and trim model below.
1) the deep-controlled model of UUV
When carrying out deep-controlled to UUV, ignore the effect of some non-principal factors in horizontal plane motion and equation, and And vertical equation (1) is disregarded to deep-controlled influence, it is u in the UUV speed of a ship or plane0Operating condition under carry out linearization process (w ≈ 0, v ≈0,p≈0,r≈0,Cos θ ≈ 1, sin θ ≈ θ), obtain equation group:
In formula, dq,dθ,dζIncluding error, uncertainty and external disturbance that model linearization generates, for system Bounded input, they are bounded.Enabling the depth of UUV instruct is constant ζr, meetIntroduce new variable ζer-ζ :
It is u that UUV, which can be obtained, in the speed of a ship or plane by (5) formula and (6) formula0When linear nominal depth control system state equation:
In formula:
2) UUV trim Controlling model
Assuming that the center of gravity G of UUV is located at the origin O of kinetic coordinate system, while ignoring horizontal plane motion and rolling motion ginseng Several influences (thinking that v, p, r are a small amount of), and disregard the higher order term of kinematic parameter, equation group can be obtained:
In formula, dq,dw,dθIncluding error, uncertainty and external disturbance that model linearization generates, for system Bounded input, they are bounded.Enabling the Angle of Trim of UUV platform instruct is constant θr, meet conditionIt introduces newly Variable θer- θ is obtained:
It is u that UUV, which can be obtained, in the speed of a ship or plane by (8) formula and (9) formula0When linear nominal pitching control system state equation:
Wherein, A=H-1P, B=H-1Q
4, the H based on T-S modelController design
1) the T-S model description of the vertical face system of UUV
Assuming that the state space of nonlinear system of the vertical face system of UUV (depth and pitching control system) containing disturbance Description are as follows:
In formula, x (t) ∈ RnFor state variable;u(t)∈RmTo control input variable;w(t)∈Rq,w(t)∈L2(R) it is External disturbance (ocean current, ocean current and measurement noise etc.);F (t) is nonlinear function.
The vertical face system of above-mentioned UUV is approached with following T-S fuzzy system, rule is as follows:
Ri:if ξ1(t) is Mi1 and ξ2(t) is Mi2...and ξp(t) is Mip
then
Z (t)=Cx (t)+Du (t)
In formula, ξi(t), i=1,2 ..., the former piece variable of r fuzzy rule;Mij(j=1,2 ..., p) it is fuzzy set;r For rule number;(Ai,Bi, H) be the corresponding dimension of i-th of subsystem matrix;RiFor the i-th rule of fuzzy system;C, D are Controlled output phase answers the matrix of dimension, then can obtain the Global fuzzy model of the vertical face system of UUV:
Wherein,
βi(ξ (t)) indicates that ξ (t) belongs to fuzzy set MijMembership function, while also illustrating that the relevance grade of the i-th rule; hi(ξ (t)) indicates standardization subordinating degree function.
2) based on the H of PDCController design
By the principle of Fig. 4 PDC it is found that the former piece of fuzzy model is enjoyed in the design of the fuzzy controller based on PDC.Assuming that mould Paste system can then obtain the fuzzy domination structure of (15) formula as shown in (14) formula:
Global system fuzzy controller are as follows:
Closed-loop system can be obtained by (13) formula and (16) formula:
Wherein,
For T-S fuzzy system (13), design point feedback controller (16), so that closed-loop system (17) asymptotically stability is simultaneously And for given γ > 0, to all w (t) ∈ L2[0 ,+∞), meet | | z (t) | |2< γ | | w (t) | |2, that is, there is H Norm circle.
Theorem 1: for giving constant γ > 0, existence feedback controller u (t)=K (h) x (t), so that closed-loop system (17) asymptotically stability and satisfaction | | z (t) | |2< γ | | w (t) | |2Necessary and sufficient condition be there are positive definite matrix Q and matrix R (h), So that:
It sets up, then designed state feedback controller are as follows:
Wherein,
The solvability of lower surface analysis inequality (18):
Due toThe item that inequality (18) formula is set up Part is inequality:
It sets up.Wherein, Q=P-1,Rj=KjQ。
Robust H has been carried out to T-S Fuzzy Descriptor SystemsThe research of control problem combines above-mentioned analysis based on this, has Theorem is set up below:
Theorem 2: system (13) is HCan be stable, if there is common nonsingular positive definite symmetric matrices Q, meet:
Wherein: Ri=KiQ.State feedback controller are as follows:
(21) formula and (22) formula are one about Q, RiLMIs.
5, UUV depth-trim coordinated control based on T-S model
The problem excessive for Angle of Trim during UUV dive, using Sliding Mode Controller during UUV dive Angle of Trim judgment module is added, to realize the limitation to Angle of Trim during dive, the present invention utilizes the H designedController Realize depth-trim coordinated control of UUV dive process.Depth-trim coordinated control basic ideas are as follows: first with H Depth controller controls the depth of UUV, while Angle of Trim judgment module is added: when Angle of Trim is greater than design requirement, From HIt is deep-controlled to switch to HTrim control then switches back into H when Angle of Trim is not more than design requirementIt is deep-controlled.
It is an advantage of the invention that being played strictly during UUV is deepened to Angle of Trim with depth-trim coordinated control Restriction effect, it is also higher to the safety of UUV operation.

Claims (1)

1. a kind of UUV diving plane H based on T-S model and PDCControl method, which comprises the steps of:
(1) UUV diving plane model, including the deep-controlled model of UUV and UUV trim Controlling model are established;
UUV diving plane model is
Vertical equation:
Trim equation:
Posture equation:
Movement relation formula:
In formula, m is UUV mass;L is the length of UUV;ρ is density of sea water;B is buoyancy suffered by UUV;U, v, w be UUV it is longitudinal, Lateral and vertical component velocity;Q, p, r are UUV trim, heel and vertical angular speed;X, y, z is UUV surging, swaying and heaving position It moves;xG、yG、zGLongitudinally, laterally and vertical center gravity for UUV;φ is UUV roll angle, θ is UUV Angle of Trim, ψ is UUV yaw angle;δs For hydroplane rudder angle;X, Y, Z be UUV longitudinally, laterally with vertical active force;K, M, N be UUV longitudinally, laterally with vertical active force Square;Z′(·)、M′(·)For zero dimension hydrodynamic force coefficient, I(·)For under hull coordinate system to the rotary inertia of axis;Center of gravity and centre of buoyancy are sat Mark is respectively (0,0,0), (0,0, zB);J be UUV to origin not in the inertia matrix of barycentric coordinate system,
(2) it is modeled using depth and trim system of the T-S model to UUV;
UUV depth and pitching control system contain the state space description of the nonlinear system of disturbance are as follows:
In formula, x (t) ∈ RnFor state variable;u(t)∈RmTo control input variable;w(t)∈Rq,w(t)∈L2(R) it is disturbed for the external world It is dynamic;F (t) is nonlinear function;
The vertical face system of above-mentioned UUV is approached with following T-S fuzzy system, rule is as follows:
Ri:if ξ1(t) is Mi1 and ξ2(t) is Mi2...and ξp(t) is Mip
Z (t)=Cx (t)+Du (t)
In formula, ξi(t), i=1,2 ..., the former piece variable of r fuzzy rule;Mij(j=1,2 ..., p) it is fuzzy set;R is rule Then number;(Ai,Bi, H) be the corresponding dimension of i-th of subsystem matrix;RiFor the i-th rule of fuzzy system;C, D are controlled Output phase answers the matrix of dimension, obtains the Global fuzzy model of the vertical face system of UUV:
Wherein,
βi(ξ (t)) indicates that ξ (t) belongs to fuzzy set MijMembership function, while also illustrating that the relevance grade of the i-th rule;hi(ξ (t)) standardization subordinating degree function is indicated;
(3) H is designed based on parallel distributed compensation PDC methodController;
Fuzzy system are as follows:
Obtain fuzzy domination structure:
Global system fuzzy controller are as follows:
Closed-loop system are as follows:
Wherein,
(4) dive of the method control UUV deepened with depth-trim coordinated control, to guarantee that Angle of Trim meets design requirement.
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