SOLVING A STABILITY PROBLEM BY POLYA S FOUR STEPS
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1 INTERNATIONAL JOURNAL OF ELECTRONICS MECHANICAL AND MECHATRONICS ENGINEERING Volume. Number. pp.(9-8) SOLVING A STABILITY PROBLEM BY POLYA S FOUR STEPS Cengiz Alacacı Murat Doğruel Bilent University Graduate School of Education 347G69 Bilent 68 AnaraTurey [email protected] Marmara University Faculty of Engineering Goztepe Istanbul Abstract: In this paper we consider the proof of stability of a nonlinear system. We found it useful to employ Polya s general four step problem solving process to organize and present the solution and our thining. Polya's ideas can help us become aware of how we thin when we solve problems. Reflecting on how we solve a problem allows us mae conceptual connections between a problem at hand and the problems we may need to solve in the future. Key Words: Saturation Nonlinearity Lyapunov stability Teaching problem solving and heuristic strategies I. INTRODUCTION Stability problems are important in engineering especially in designing control systems. Solving stability problems may require extensive use of mathematical analysis. Methods of solution are sometimes more than straightforward applications of familiar algorithms. The problems and their solutions require intuition experimentation trial and error and active monitoring of one s thining. In presenting mathematical solutions of many engineering problems most scholarly papers and textboos treat the solution as a finished product giving little insight into the processes of solution. There is often little exposition of the choices made why they were made and little reflection on the solution once it is reached. As George Polya said in his well-nown boo How to solve it Teachers and authors of textboos should not forget that the intelligent student and the intelligent reader are not satisfied by verifying that the steps of reasoning are correct but also want to now the motive and the purpose of the various steps. [7 p. 5]. We believe that there is value in consideration of these aspects of thining about thining in solving problems. Most experienced problem solvers agree that relating the problem at hand to similar problems understanding it choosing a method of approach nowing when to bac off and reconsider the method when it seemed unproductive and looing bac and reflecting on the solution are critical parts of the solution process. Readers of a problem solution would benefit from discussion of these issues as much as the products of the solution because it helps to give a deeper understanding of the solution. For novices it maes attainment of these self-regulatory sills less of a solitary experience. In this article we present a solution of a stability problem. We found it useful to employ George Polya s ( ) general four step problem solving process to organize and present the solution and our thining. The steps of solving a problem are outlined in his well-nown boo How to Solve It [7]:. Understanding the problem. Devising a plan 3. Carrying out the plan 4. Looing bac.
2 Cengiz Alacacı Murat Doğruel The first step involves understanding the given conditions and constraints of the problem III. UNDERSTANDING THE PROBLEM elaborating the goal and the unnown maing the necessary assumptions. The second step requires consideration of similar problems solved before if the problem can be worded differently to mae it more familiar and eventually developing a plan of attac. The third step involves applying the procedures of the chosen method and maing sure that it is used correctly. In the last step findings are tested against the conditions of the problem and connections with similar problems of more general type are made based on the findings. The steps may not be used in a fixed order..for example if problems are encountered while carrying out the plan individual may need to go bac and revise the plan or even return to the first step to mae additional assumptions in order to use a particular method [9]. It is important to note that we use Polya s steps of problem solving as a tool of illustrating organizing and presenting our thining rather than a specific method of solution by itself. II. THE PROBLEM Solving problems is a fundamental human activity. In fact the greater part of our conscious thining is concerned with problems. [7 p. ] As an example consider the following specific system provided in [3]: x& x + x + u () x& x x + u with a saturated linear control function u sat(.65x.475x ) where α sat ( α) α α > α<. The problem is to find out if the above system is globally asymptotically stable. The intelligent problem-solver tries first of all to understand the problem as fully and as clearly as he can. The open secret of real success is to throw your whole personality into your problem. [7 p. 73] Our first duty is to understand the problem [7 p73]. If there was no saturation the system would be completely linear and we could have checed the global asymptotic stability by just seeing if the eigenvalues of the feedbac system have negative real parts. Anyhow let us chec them and have an idea about the system. When there is no feedbac (u) the open loop system eigenvalues are both located at and they are coupled. This is a little bit alarming because this ind of system is potentially unstable. Assuming there is no saturation with the linear feedbac the system eigenvalues are moved to -.5 and -.6 which would produce a stable system. This linear feedbac is only valid in the unsaturated region where.65x.475x. This region on the other hand includes the origin where the state variable will eventually reach. This suggests that the system () with the feedbac is asymptotically stable. To show that it is globally asymptotically stable we further need to show that all trajectories starting at any initial position in the state space will actually reach the origin. Let us elaborate on the problem further. We should simulate the system to understand its behavior. Figure shows trajectories for various initial conditions. As expected the system shows a stable behavior at least locally. To see the behavior in the large we simulate the system for an initial value of (5 5) as shown in Figure. The corresponding saturated control is depicted in Figure 3.
3 Cengiz Alacacı Murat Doğruel x Initial points State trajectory Linear Region Saturation: u Saturation: u - In order to obtain a simpler system representation a linear transformation can be applied. From () it is easily seen that x& + x& u. Hence if one of the state variables is chosen as ( x )/ + x its derivative will be simply u. Also x & x& ( x+ x) or x x )/ ( x& & )/ 4 ( x x Fig.. State trajectories of the nonlinear system for various initial values. x Initial point State trajectory Therefore if the second state variable is chosen as ( x )/ 4 its derivative will be simply the first state variable. Using this idea let us try the following transformation: y ( x x ) / 4 x () y ( x + x ) /. Now the following equivalent system is obtained y (3) sat(.3y.y ). Since the transformation () is invertible the systems () and (3) are equivalent in the global asymptotic stability. The system (3) on the other hand loos a little simpler. We now that the system (3) must also be asymptotically stable locally but is it globally stable? We simulate the system (3) for an initial value of ( 75) as shown in Figure x Fig.. The state trajectory for an initial value of (5 5). u y Initial point State trajectory Switching Line t (sec.) Fig. 3. The control input versus time (in seconds) for an initial value of (5 5). As seen in Figure although the trajectory starts at (5 5) it first moves to around (6-6) then to (-3 3) and eventually stabilized at the origin. Of course one example would not be sufficient but our intuition says that although the trajectory moves and oscillates too much the system could be globally stable y Fig. 4. The state trajectory for the system (3) for an initial value of ( 75). The trajectory path now appears easier to follow. The linear region where.3y.y loos so thin for large y values that it is shown as a dotted line in Figure 4. Outside this linear region saturation occurs. When the trajectory hits the linear region it quicly changes its
4 Cengiz Alacacı Murat Doğruel direction and follows the other saturated dynamics as seen in Figure 4. IV. DEVISING A PLAN To devise a plan to conceive the idea of the solution is not easy. It taes so much to succeed; formerly acquired nowledge good mental habits concentration upon the purpose and one more thing: good luc. [7 p. ] How can then we show that the system is actually globally stable? There are some methods to try in our toolbox. The famous circle or Popov criteria (for example see [] or [4]) would be a suitable method for this problem; however the open loop system has coupled eigenvalues on the jw axis. Loop transformation (see [4]) will not wor either because the saturation nonlinearity belongs to the sector [ ]. In fact for this ind of systems there are some nonlinearities in sector [ ] that maes the system globally unstable (see Example 7. in [6]); therefore the system is actually not absolutely globally stable therefore these methods are not applicable. There is actually a result to show the global stability of this specific system in the literature (for example see [][][8]) however let us continue on our path since our main goal is to show a solution strategy of the problem. A very well-nown method to show global stability is Lyapunov s direct method ([] [4]). Let us try to use this classical and powerful method. The level surfaces of the Lyapunov function (for a fixed function value) must be in such a way that when the trajectory enters in the surface it must never leave that surface. To be able to guess a proper Lyapunov function for this example we need to understand how exactly the trajectory moves when it is in the saturated regions. On the right side of the linear region (for.3y.y < )the corresponding system dynamics is y (4). And on the left side (for.3y.y ) we have > y (5). The solutions of these systems can be easily found as follows. For the system y( t) t + y () t+ y() (4): (6) y ( t) t+ y (). For the system y( t) t + y () t+ y() (5): (7) y ( t) t+ y (). Therefore we conclude that outside the linear region the trajectories follow a parabolic path. Another observation from Figure 4 is that although the intersections of the trajectory with the y axis grow linearly as y is increased the intersections grow approximately in square fashion for the y axis. Through these observations we can conclude that V(x) x Px type quadratic Lyapunov function candidates are not suitable for this nonlinear system. The reason is that a quadratic function produces elliptic level surfaces which have a fixed width/height ratio. In this case however the level surfaces should be in such a way that the width/height ratio should grow for a higher Lyapunov function value. Devising the plan of the solution we should not be too afraid of merely plausible heuristic reasoning. Anything is right that leads to the right idea. [7 p. 68] Then how can we find a proper Lyapunov function for this example? From the simulations and from (6) and (7) we observe that in either one of the saturation regions and for a certain portion of the y + remains constant. trajectory the quantity This may be a good start for a Lyapunov function candidate. Let y + y (8) y and chec how it behaves for the system (3). Using the same initial value as in Figure 4 the function (8) is shown in Figure 5. It almost wors; there is no increase in the function and it stays constant on the parabolic paths as expected. However the function must be strictly decreasing to show the global stability.
5 Cengiz Alacacı Murat Doğruel V t (sec.) Fig. 5. The Lyapunov function candidate (8) for an initial state value of ( 75). How can we mae the function decrease when the trajectory moves on the parabolic path? We observe that y increases for the left region and decreases for the right region when the time moves forward. Using this hint we suggest this new Lyapunov function candidate y + y + y. (9) After some simulations we see that this candidate seems to wor for positive values less than 6.4. For the resulting function is shown in Figure 6. Now we have a strictly decreasing Lyapunov function candidate for the system (3). V t (sec.) Fig. 6. The Lyapunov function candidate (9) for an initial state value of ( 75). y + y y + sat( ) dα α () which behaves approximately the same as shown in Figure 6. Simulations fortunately shows that for small y values around the origin in the linear region () still wors as a proper Lyapunov function. Finally using the transformation () and the candidate () the corresponding Lyapunov function candidate for the system () can be found as V ( x) x 4 ( x + x ) + sat( ) dα α. () We expect that the global asymptotical stability of the system () should be shown using this function. IV. CARRYING OUT THE PLAN To carry out the plan is much easier; what we need is mainly patience. The plan gives a general outline; we have to convince ourselves that the details fit into the outline and so we have to examine the details one after the other patiently till everything is perfectly clear and no obscure corner remains in which an error could be hidden. [7 p. -3] Now we need to prove that the candidate () is really a proper Lyapunov function for global asymptotic stability (for example see Theorem 3.3 in [4]). It is easy to see that V (x) is positive definite and radially unbounded and has continuous first order derivatives. Using the system equations we have One problem with (9) is that it does not have continuous first order derivatives due to the absolute value operator. To fix this problem we may substitute the following smoother function in place of the absolute value function z z z z sat( α ) dα z z > which has continuous first order derivatives and for larger values ( z > ) approximately does the same job as an absolute value function. Therefore choosing we suggest a Lure-type Lyapunov function candidate
6 Cengiz Alacacı Murat Doğruel V& ( x) ( x + x )( x& + x& ) + sat( x ) x& ( x * sat(.65x sat( x ) * * * ( x + x + sat(.65x.475x )) ( x + x ) * ) *.475x ( sat( x ) + sat(.65x.475x )) sat( x ) sat(.65x + x ) +.475x Let us first formally define the regions shown in Figure 7 A { x cx and x } B { x cx< and x > } C { x cx< and x } D { x cx< and x < } E { x cx and x < } F { x cx> and x < } G { x cx> and x } H { x cx> and x > } I { x cx and x > }. where cx.65x. 475x. ). + V & ( x) ( x + x ).5x ( x.65x.475x ) + x (.65x.475x ).575x x.475x (.5x +.575x ).444x And V & ( ). In region B: < for x. ( ) + ( ). V & ( x) ( x + x ) < In region C: V& ( x) ( x+ x )( x ) + x( ) ( x+ x ) ( x ) < In region D: ( x + x > V& ( x) ( x + x ) ( ) ( ) ) + ( x+ x ) < 443 > In region E: V& ( x) ( x + x ).65x.475x.65x ( ).x x.475x.375x.55x. (.65x.475x ) In regions F to I: Since V ( x) V ( x) and & & V & ( x) < in the opposite regions V & (x) must also be negative in these regions. Hence V & (x) is a negative definite function. Therefore we conclude that the system () with the saturated linear feedbac is actually globally asymptotically stable. VI. LOOKING BACK Looing bac at the completed solution is an important and instructive phase of the wor. He thins not well that thins not again. Second thoughts are best. [7 p.4] Looing bac the problem according to Polya we need to as these questions [7]: Can you derive the solution differently? Can you use the result or the method for some other problem? Fig. 7. The regions for the Lyapunov function (). In region A:
7 Cengiz Alacacı Murat Doğruel Here we have considered a specific problem however we may use the solution strategy and the insights we gained from it in a general statement of the problem. Let us reconsider (3) with general parameters y () sat( y+ y). Here and are assumed to be positive constants otherwise the system will not be asymptotically stable because locally the corresponding linear system will not have both eigenvalues in the left half plane. For any positive and on the other hand the system will be guaranteed to be asymptotically stable locally. To understand the global behavior in general let us consider Figure 8 as done for the specific case in Figure 4. y y -( / )y -p l () (3) () p r For the system (5) (the left side): y y p l (4) where p r and -p l are the points that the trajectory crosses y axis on the right and left sides. Actually the values p r and p l can be good measures for the energy or size of the parabolic trajectory. Perhaps we can use these values to construct the Lyapunov function. Therefore using (3) and (4) let us suggest a Lyapunov function candidate as y + y y+ y > (5) y + <. + y y y Actually this function may not even be positive definite (especially when / is small) however let us not stop and get discouraged but go on and try to improve the function step by step if possible. The two cases in the above formula can be combined as shown below V y) y + y sat( y + y ) (6) ( where the sat() function automatically handles the sign of y in (5). Therefore when the trajectory is on the parabolic path V(y) will be constant; and when the trajectory reaches the other side it will be reduced almost instantly as observed in Figure 5. Again y can be used to obtain a decreasing V(y) as V y) y + ( y + σ y ) sat( y + y ) (7) ( Fig.8. The general state trajectory in the large. As before the linear region loos so thin in the large view that it is shown as a dotted line in Figure 8. Assuming the initial state is sufficiently large we see that trajectory starting at point () follows a parabolic path and reaches point (). Then it follows another parabolic path and reaches point (3). The formulas (6) and (7) will also apply here for the general case. Then the trajectory continues in a similar way until it reaches the origin. This suggests that for any positive and the system () should be globally asymptotically stable. However how can we prove this result? In the earlier specific problem we spent too much effort to find and prove a proper Lyapunov function. y where σ is a positive constant so that on the right side V should decrease since y decreases. On the left side y increases but because of the negative sign of the sat() function V should again decrease. To ensure that the function in (7) is a positive definite function for any (positive) and the parameter σ can be chosen as / therefore one obtains y+ ( y + y) sat( y y+ ). (8) Note that z sat(z) is always positive for z. Now the problem as before is that V must have continuous first order derivatives. Using (6) and (7) the parabolic trajectory paths can be obtained as For the system (4) (the right side): y y + pr (3)
8 Cengiz Alacacı Murat Doğruel To overcome this problem the following approximation can be used z sat( z) sat( α ) dα z and finally the following Lyapunov function candidate can be suggested y+ y y + sat( α ) dα. (9) Examining the various parts one after the other and trying various ways of considering them we may be led finally to see the whole result in a different light and our new conception of the result may suggest a new proof. [7 p. 64] It is clear that V(y) is positive definite and radially unbounded also it has continuous first order derivatives. Let us chec its derivative V & ( y) y sat( y + y ) + y sat( y + y sat ( y sat ( y It is easily seen that (y) ) + + y ) y ). () V & is negative semidefinite; y + y (the and for the points satisfying linear line in Figure 8) V & (y) is zero. Since V & (y) is only negative semidefinite the invariant set theorem can be applied (see Theorem 3.5 in []). In fact according to () for any initial state starting on the invariant set (the points on the linear line) the corresponding trajectory immediately leaves the invariant set except for the origin. Hence we conclude that the origin of the system () is globally asymptotically stable for any positive and. Therefore using the Lyapunov function (9) instead of () the stability is proven in a much easier way and for a general system. Let us generalize the system representation even further as y () f ( y+ y ). Here a general nonlinear function is used instead of the saturation. Adapting (9) for this case we can suggest y+ y y + f ( α ) dα () and therefore V &( y) f ( y+ y). (3) If the following conditions are satisfied ) f (x) is continuous ) xf ( x) > for x (and f ( ) ) x ( α dα as 3) f ) 4) > and >. x then the Lyapunov function () will be positive definite (conditions and 4) radially unbounded (condition 3) having continuous first order derivatives (condition ); and the derivative (3) will be negative semidefinite (condition 4) and zero only on the line y+ y (condition ). Again according invariant set theorem we can conclude the following result: The system () satisfying the conditions (4) is globally asymptotically stable. Actually many systems in practice can be reduced to the system description in (). Many electromechanical systems can be described as a double integrator type dynamics with linear negative feedbac through a nonlinear and/or saturating actuator. One example for such f(x) is shown in Figure 9. It should be noted that although this ind of systems are globally asymptotically stable the trajectories may easily pass over the practical limits in the state space as observed in Figure.
9 Cengiz Alacacı Murat Doğruel Fig.9. An example of a nonlinear function satisfying the conditions -3 in (4). It is also interesting to note that when there are three or more cascaded integrators no linear saturated feedbac will produce a globally asymptotically stable system []. According to the result found when there are two cascaded integrators (double integrators) all the stabilizing linear feedbacs will wor for the saturated case. The result presented here could not be found on many boos or papers on nonlinear systems. For example [] (Example 3.4) [4] (Example 4.9) and [6] (Example 6.5) only mentions that the systems in the following form are globally asymptotically stable: y f ( y) g( y ) where f satisfies the conditions -3 and g satisfies the conditions - in (4). As indicated in [8] Meyer studied the linear systems with two zero eigenvalues and saturated linear control and gave conditions on the global asymptotic stability (see pp in [5]). Although it is not shown explicitly when () is considered as a special case Meyer s conditions reduce to (4). Also in an exercise (p.65 in []) Aggarwal suggests a similar Lyapunov function as in () for the system (). Many different control methods and stability results for double integrators are presented in [8]. VII. CONCLUDING COMMENTS but how is it possible to invent such a solution? Yes this experiment seems to wor this appears to be a fact; but how can people discover such facts? And how could I invent or discover such things by myself? Trying to understand not only the solution of this or that problem but also the motives and procedures of the solution and trying to explain these motives and procedures to others he was finally led to write the present boo. [7 from introduction] In this article we attempted to present the plausible reasoning that Polya described. We tried to expose the thining that went into solving a saturation nonlinearity type stability problem with specified parameters. In order to solve it we needed to understand the effect of the nonlinearity on the linear system and explore its behavior. For example to understand the problem we simulated the system in various initial conditions. Then we looed into plausible methods and chose the one that seemed to satisfy the constraints of the problem. Popov criterion could not be applied even with a loop transformation but Lyapunov method seemed promising. After considerable experimentation we were able to find a function that helped demonstrate the global stability of the problem and we verified the findings. Looing bac based on the insights gained from solving the specific version of the problem we posed a new question: What if the parameters are considered in general as and? Using a similar solution strategy but finding a more convenient Lyapunov function this time we could prove the global stability for the general case. By simply adapting the Lyapunov function we were able to demonstrate the global stability of the more general case when the saturation is replaced by a special nonlinear function. We moved from specific to a general case in this problem. Technically the more general solution subsumes the specific solution but this should not tae away from the value of the findings to the specific case. Because reaching the general solution was based on the findings of the specific case. We are hoping that the inductive solution we present here can provide a glimpse of the thining that produced the results which are often given deductively as a finished product in most scholarly writings. The author remembers the time when he was a student himself a somewhat ambitious student eager to understand a little mathematics and physics. He listened to lectures read boos tried to tae in the solutions and facts presented but there was a question that disturbed him again and again: Yes the solution seems to wor it appears to be correct;
10 By its nature Polya's ideas can help us become aware of how we thin when we solve problems. By reflecting on how we solve a problem we are more liely to mae connections with the problem at hand and the problems we may need to solve in the future. Being well-versed in Polya's ideas and steps may not by itself guarantee success in understanding or solving a new problem because such success is a product of both nowledge of similar problems and how we regulate that nowledge and our mental resources. However Polya s ideas can help unpac the complex thining processes that go into the solution of a problem and hence can help the novices develop effective selfregulating sills in thining to re-produce the solution and produce new solutions to other problems. VIII. REFERENCES [] J.K. Aggarwal: Notes on Nonlinear Systems New Yor Van Nostrand Reinhold 97. [] J. Alvarez R. Suárez and J. Alvarez: Planar linear systems with single saturated feedbac Systems & Control Letters (993). [3] M. Doğruel: Input linearization of nonlinear systems via pulse width control IEEE Transactions on Automatic Control 48(4) (3). [4] H.K. Khalil: Nonlinear Control Systems Third Ed. Englewood Cliffs Prentice Hall. [5] S. Lefschetz: Stability of Nonlinear Control Systems New Yor Academic Press 965. [6] R.R. Moher: Nonlinear Systems Volume I Dynamics and Control Englewood Cliffs Prentice Hall 99. [7] G. Polya: How to Solve It A New Aspect of Mathematical Method Second Ed. Princeton Princeton University Press 985. [8] V. Rao and D. S. Bernstein: Naive Control of the Double Integrator IEEE Control Systems Magazine (). [9] A.H. Schoenfeld: Cognitive Science and Mathematics Education Hillsdale Lawrence Erlbaum 987. [] J.E. Slotine and W. Li: Applied Nonlinear Control Englewood Cliffs Prentice Hall 99. [] H.J. Sussmann and Y. Yang: On the stabilizability of multiple integrators by means of bounded feedbac controls Proc. 3th CDC pp. 7-7 Brighton U.K. (99).
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