Journal of Engineering and Technology

ARTICLE
Year
: 2012  |  Volume : 2  |  Issue : 1  |  Page : 13--18

A High-Order Sliding Mode Observer: Torpedo Guidance Application


Ahmed Rhif, Zohra Kardous, Naceur BenHadj Braiek 
 Advanced System Laboratory, Polytechnic School of Tunisia (Laboratoire des Systèmes Avancés (L.S.A), Ecole Polytechnique de Tunisie, BP 743, 2078 La Marsa, Tunisie)

Correspondence Address:
Ahmed Rhif
Advanced System Laboratory, Polytechnic School of Tunisia (Laboratoire des Systèmes Avancés (L.S.A), Ecole Polytechnique de Tunisie, BP 743, 2078 La Marsa, Tunisie)

Abstract

The guidance of a torpedo represents a hard task because of the smooth nonlinear aspect of this system and because of the extreme external disturbances. The torpedo guidance reposes on the speed and the position control. In fact, the control approach which is very solicited for the electromechanical systems is the sliding mode control (SMC) which proved its effectiveness through the different studies. The SMC is robust versus disturbances and model uncertainties; however, a sharp discontinuous control is needed which induces the chattering phenomenon. The angular velocity measurement is a hard task because of the high level of disturbances. In this way, the sliding mode observer could be a solution for the velocity estimation instead of a sensor. This article deals with torpedo guidance by SMC to reach the desired path in a short time and with high precision quality. Simulation results show that this control strategy and observer can attain excellent control performances with no chattering problem.



How to cite this article:
Rhif A, Kardous Z, Braiek NB. A High-Order Sliding Mode Observer: Torpedo Guidance Application.J Eng Technol 2012;2:13-18


How to cite this URL:
Rhif A, Kardous Z, Braiek NB. A High-Order Sliding Mode Observer: Torpedo Guidance Application. J Eng Technol [serial online] 2012 [cited 2019 Aug 23 ];2:13-18
Available from: http://www.onlinejet.net/text.asp?2012/2/1/13/94231


Full Text

 1. Introduction



Most modern torpedoes are completely autonomous. They have active sonar which gives them abilities to direct themselves to the target which have been designated before launch. Other types of torpedoes, for example, self-possessed, have an acoustic sensor (passive sonar) that allowed them to track the noise emitted by the engines of the target. Modern torpedoes are powered by steam or electricity, they have speeds ranging from 25 to 45 knots, and their scope ranges are from 4 to 27 km. They consist of four elements: the warhead, the air section, rear section, and tail section. The warhead is filled with explosive (181 to 363 kg). In a torpedo, steam-air section is about one third of the torpedo and contains compressed air and fuel tanks and water for the propulsion system. In fact, the torpedo guidance reposes on the speed and the position control. In this way, the sliding mode control (SMC) has largely proved its effectiveness through the reported theoretical studies; its principal scopes of application are robotics, mobile vehicle, and the electrical engines [1],[2],[3],[4] . The advantage of such a control is its robustness and its effectiveness through the disturbances and the uncertainties of the model.

Indeed, to make certain the convergence of the system to the wished state, a high level control in addition to a discontinuous control is often requested. This fact generates the chattering phenomenon which can be harmful for the actuators. In fact, there are many solutions suggested to this problem. In literature, (SMC) with limiting band has been considered. This solution consists in replacing the discontinuous part of the control by a saturation function. Also, fuzzy control was proposed as a solution, thanks to its robustness. In another hand, the high-order sliding mode consists in the sliding variable system derivation. This method allows the rejection of the chattering phenomenon while maintaining the robustness of the approach. The high-order SMC can be represented by two algorithms:



The twisting algorithm: the system control is increased by a nominal control u e ; the system error, on the phase plane, rotates around the origin until been cancelled. If we derive the sliding surface (S) n times we notice that the convergence of the state to the sliding surface S is even more accurate when n is higher.The super twisting algorithm: the system control is composed of two parts u 1 and u 2 with u 1 equivalent control and u 2 the discontinuous control used to reject disturbances. In this case, to obtain a sliding mode of order n, we have to derive the error of the system n times [5].

In the literature, different approaches have been proposed for the synthesis of nonlinear surfaces. In Ref. [6] , the proposed area consists of two terms, a linear term that is defined by the Herwitz stability criteria and another nonlinear term used to improve transient performance. In Ref. [7] , to measure the armature current of a DC motor, Zhang Li used the high-order sliding mode because it is faster than traditional approaches such as vector control.... To eliminate the static error that appears when measuring parameters, one uses a PI controller [8],[9],[10],[11],[12],[13],[14] . Thus, the authors have chosen to write the sliding surface in a transfer function of a proportional integral form while respecting the convergence properties of the system to this surface. The same problem of the static error was treated by adding an integrator block just after the SMC [15] .

 2. Process Modeling



Torpedoes [Figure 1] are systems with strong non linearity and always subject to disturbances and model parameter uncertainties which makes their measurement and their control a hard task. Equation (1) represents the torpedo's motion's dynamic equation in 6 degrees of freedom. M is the matrix of inertia and added inertia, C is the matrix of Coriolis and centrifugal terms, D is the matrix of hydrodynamic damping terms, G is the vector of gravity and buoyant forces, and τ is the control input vector describing the efforts acting on the torpedo in the body-fixed frame. B is a nonlinear function depending of the actuators characteristics, and u is the control input vector [16] .

[INLINE:1]

{Figure 1}

For the modelling of this system, two references are defined [Figure 1]: one fix reference related to the torpedo which defined in an origin point: R 0 (X 0 , Y 0 , Z 0 ) and the second one related to the Earth R(x, y, z).

where

ω is linear velocity, q the angular velocity, θ the angle of inclination, and z the depth. The system control is provided by u which presents the immersion deflection.

The torpedo presents a strong nonlinear aspect that appears when we describe the system in three dimensions (3D), so the state function will present a new term of disturbances φ as shown in (2).

[INLINE:2]

As we consider only the linear movement in immersion phase, we need only four degrees of freedom, for that we describe the system only in two dimensions (2D). All development done, the resulting state space describing the system is given by (3).

[INLINE:3]

The system could be represented by two parts [17] : H 1 (p) the transfer function of inclination (4) and H 2 (p) the transfer function of immersion (5).

[INLINE:4]

 3. The Controller Design



3.1 The SMC

The SMC consists in bringing back the state trajectory toward the sliding surface and to make it move above this surface until reaching the equilibrium point. The sliding mode exists when commutations between two controls u max and u min remain until reaching the desired state. In another hand, the sliding mode exists when: [INSIDE:1]. This condition is based on Lyapunov quadratic function. In fact, control algorithms based on Lyapunov's method have proven effectiveness for controlling linear and nonlinear systems [18] .

To ensure the existence of the sliding mode, we must produce a high level commutation control. For that we will use a relay which commutates between two extreme values of control. Second, we have to define a first-order sliding surface. In this case we will choose the surface form written in (6).

[INLINE:5]

In the convergence phase to the sliding surface, we have to verify that:

[INLINE:6]

In this case, the control law of the sliding mode is given by (8).

[INLINE:7]

[INLINE:8]

sign(.) is the sign function and k a positive constant that represents the discontinuous control gain

Chattering phenomenon

The SMC has always been considered a very efficient approach. However, considered that it requires a high-level frequency of commutation between two different control values, it may be difficult to put it in practice.

In fact, for any control device which presents non linearity such as delay or hysteresis, limited frequency commutation is often imposed, other ways the state oscillation will be preserved even in vicinity of the sliding surface. This behavior is known by chattering phenomenon.

This highly undesirable behavior may excite the high-frequency unmodeled dynamics which could result in unforeseen instability and can cause damage to actuators or to the plant itself. In this case, the high-order sliding mode can be a solution.

3.2 High-order SMC synthesis

The aim of the high-order SMC is to force the system trajectories to reach in finite time the sliding ensemble of order r ≥ p defined by:

[INLINE:9]

p > 0, s(x,t) the sliding function: it is a differentiable function with its (r - 1) first-time derivatives depending only on the state x(t) (that means they contain no discontinuities) [19],[20],[21] . In the case of second-order SMC, the following relation must be verified:

[INLINE:10]

The derivative of the sliding function is

[INLINE:11]

Considering relation (12), the following equation can be written

[INLINE:12]

The second-order derivative of S(t,x) is:

[INLINE:13]

This last equation can be written as follows:

[INLINE:14]

We consider a new system whose state variables are the sliding function s(t,x) and its derivative [INSIDE:2].

[INLINE:15]

Eqs. (15) and (18) lead to (19)

[INLINE:16]

In this way, a new sliding function σ(t,x) is proposed:

[INLINE:17]

Eqs. (6) and (19) lead to (20)

[INLINE:18]

3.3 The sliding mode observer

The angular velocity measurements of the torpedo represent a hard task and could give unreliable results because of the very high disturbances that influence the tachymetry sensor. In this way, it may be adequate to estimate the angular velocity Ω using an observer instead of the sensor. This operation would give better results and will reduce the number of the sensors which are very costly and may have hard maintenance skills.

The observer can reconstruct the state of a system from the measurement of inputs and outputs. It is used when all or part of the state vector cannot be measured. It allows the estimation of unknown parameters or variables of a system. This observer can be used to reconstruct the speed of an electric motor, for example, from the electromagnetic torque. It also allows reconstructing the flow of the machine etc.…

The observed velocity error is noted in (22).

[INLINE:19]

with [INSIDE:3] the estimated angular velocity.

In this case, the system (3) could be represented as follow:

[INLINE:20]

 4. Simulation Results



The simulation results of systems (4) and (5) are given by the flowing figures [Figure 2], [Figure 3], [Figure 4] and [Figure 5]. {Figure 2}{Figure 3}{Figure 4}{Figure 5}

[Figure 2] and [Figure 3] show that using PID controller, the system does not reach the desired value and have a very sharp oscillations frequency. In the case of the first-order sliding mode control (SM1), we can reach the desired value in a short time, other ways we notice that the reaching phase presents some oscillations known as chattering effect. In another hand, the second-order sliding mode (SMC2) reduces considerably the chattering phenomenon and the convergence time to the desired state while preserving the robustness aspect of the control approach.

The inclination q of the torpedo is close to zero and its evolution is more stable in the case of the second-order SMC which gives more stability effect to the system [Figure 3].

Finally, we can conclude the excellent estimation quality of the sliding mode observer [Figure 4] and [Figure 5] which illustrates that the estimated velocity and current of the control are very close to the real measurements.

 5. Conclusion



In this work, torpedo controllers have been presented, detailed, and justified by simulation results. We approached the synthesis method of a control law by sliding mode using a nonlinear sliding surface. In the first time, we presented the class and the properties of this sliding surface adopted. Then, a SMC using the sliding surface developed together with stability studies were elaborated. Finally, second-order of SMC was developed with a sliding mode observer and then tested by simulation on a torpedo. Simulation results show the ability of the SMC for the tracking process of the needed path and the high estimation quality of the observer.

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