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An Optimal Control Model of Arms Races*

Published online by Cambridge University Press:  01 August 2014

John V. Gillespie
Affiliation:
Indiana University
Dina A. Zinnes
Affiliation:
Indiana University
G.S. Tahim
Affiliation:
Indiana University
Philip A. Schrodt
Affiliation:
Northwestern University
R. Michael Rubison
Affiliation:
Kansas State University

Abstract

Lewis Frye Richardson's simple differential equations model of armaments races has been long criticized for its lack of incorporation of the goals of nations. Using the mathematics of optimal control theory, the authors formulate a model which incorporates national goals into an “arms balance” objective function. The goals used are based on the traditional concerns in the balance-of-power literature. From an objective function together with the Richardson model an optimal armaments policy is derived. The United States-Soviet, NATO-WTO, and Arab-Israeli arms races are used as empirical examples, and the parameters in the model are estimated by means of functional minimization techniques. The optimal control model is further examined for its equilibrium and stability properties. The equilibrium and stability conditions are assessed with respect to the empirical examples. The findings are that while the United States and the Soviet Union in direct confrontation pursue strategies that lead to a lack of equilibrium and stability, when taken as part of NATO and WTO, the major powers and their alliance partners do pursue stable and equilibrium strategies. The Israeli policy is found to lead to equilibrium and stability while the Arab policy does not.

Type
Research Article
Copyright
Copyright © American Political Science Association 1977

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Footnotes

*

Support for this research was supplied by the National Science Foundation, Research Grant GS-36806. The authors wish to express appreciation to Professors Jose B. Cruz, Jr. (University of Illinois), Dagobert Brito (Ohio State University), Michael Intriligator (University of California, Los Angeles), and I. W. Sandberg (Bell Laboratories) for their helpful suggestions and valuable assistance. A previous draft of this paper was presented at the 1974 meetings of the Midwest Political Science Association, Chicago, Illinois.

References

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3 Numerous scholars have attempted to examine the degree of empirical fit between the Richardson model or modified Richardson models and armaments races or have suggested reformulations of Richardson's basic model. See, for example: Alcock, N. Z. and Lowe, Keith, ‘The Vietnam War as a Richardson Process,” Joumal of Peace Research, 6 (April, 1969), 105112 CrossRefGoogle Scholar; Blumberg, Avron A., “Model for a Two-Adversary Arms Race,” Nature, 234 (November 19, 1971),158 CrossRefGoogle Scholar; Caspary, William R., “Richardson's Model of Arms Races: Description, Critique, and an Alternative Model,” International Studies Quarterly, 11 (March, 1967), 6388 CrossRefGoogle Scholar; Chase, P. E., ‘The Relevance of Arms Race Theory to Arms Control,” General Systems Yearbook, 13 (1968), 9198 Google Scholar, and Feedback Control Theory and Arms Races,” General Systems Yearbook, 14 (1969), 137149 Google Scholar; Chatterji, Manas, “A Model of Resolution of Conflict between India and Pakistan,” Peace Research Society Papers, 12 (1969), 87102 Google Scholar; Ferejohn, John, “On the Effects of Aid to Nations in Arms Races” (Paper delivered at the Annual Meeting of the American Statistical Association, December, 1970)Google Scholar; Friberg, Mats and Jonsson, Dan, “A Simple War and Armament Game,” Journal of Peace Research, 5 (July, 1968), 233247 CrossRefGoogle Scholar; Intriligator, Michael D., “Some Simple Models of Arms Races,” General Systems Yearbook, 9 (1964),143147 Google Scholar; Ivanilov, Yu. P., “A Model of Competition between Two Countries,” Engineering Cybernetics, 1 (Jan.-Feb., 1969),1930 Google Scholar; Kupperman, Robert H. and Smith, Harvey A., “Strategies of Mutual Deterrence,” Science, 176 (April 7, 1972), 1823 CrossRefGoogle ScholarPubMed; Lambelet, John C, “A Dynamic Model of the Arms Race in the Middle East, 1953–1965,” General Systems Yearbook, 16 (1971), 145167 Google Scholar, and Towards a Dynamic Theater Model of the East-West Arms Race,” Journal of Peace Science, 1 (Autumn, 1973), 138 CrossRefGoogle Scholar; Midgaard, Knut, “Arms Races, Arms Control, and Disarmament,” Cooperation and Conflict, 5 (February, 1970), 2051 CrossRefGoogle Scholar; Moll, Kendall D., The Influence of History Upon Seapower, 1865–1914 (Menlo Park, Cal.: Stanford Research Institute, September, 1968)Google Scholar; O'Neill, Barry, ‘The Pattern of Insta-bihty among Nations: A Test of Richardson's Theory,” General Systems Yearbook, 15 (1970), 175181 Google Scholar; Rathjens, George W., ‘The Dynamics of the Arms Race,” Scientific American, 220, no. 4 (April, 1969), 1525 CrossRefGoogle Scholar; Smoker, Paul, “A Mathematical Study of the Present Arms Race,” General Systems Yearbook, 8 (1963), 6176 Google Scholar, Fear in the Arms Race: A Mathematical Study,” Joumal of Peace Research, 1 (February, 1964), 5564 CrossRefGoogle Scholar, Trade, Defense and the Richardson Theory of Arms Races: A Seven Nation Study,” Journal of Peace Research, 2 (April, 1965), 161176 CrossRefGoogle Scholar, Nation State Escabtion and international Integration,” Journal of Peace Research, 4 (February, 1967), 6175 CrossRefGoogle Scholar. The Arms Race As an Open and Closed System,” Peace Research Society Papers, 7 (1967), 4142 Google Scholar; Wagner, D. L., Perkins, R. T. and Taagepera, R., “Fitting the Soviet-U.S. Arms Race Data to the Complete Solution of Richardson's Equations” (paper presented at the 1974 Meetings of the Western Regional Peace Science Society)Google Scholar; Zinnes, Dina A. and Gillespie, John V., “Analysis of Arms Race Models: USA vs. USSR and NATO vs. WTO,” Modeling and Simulation, vol. 4, ed. Vogt, William G. and Mickle, Marlin H. (Pittsburgh: Instrument Society of America, 1973), pp. 145148 Google Scholar; Wotfson, Murray, “A Mathematical Model of the Cold War,” Peace Research Society Papers, 9 (1968), 107124 Google Scholar. Some schokrs have suggested goals for nations involved in various specific aspects of armaments races. See McGuire, Martin C, Secrecy and the Arms Race (Cambridge, Mass.: Harvard University Press, 1965)Google Scholar, and Saaty, Thomas L., Mathematical Models of Arms Control and Disarmament New York: John Wilay and Sons, 1968)Google Scholar.

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7 Other objections have been raised about the Richardson model. See Alker, “Structure of Social Action”; Rapoport, “Richardson's Mathematical Theory”; and Caspary, “Richardson's Model.”

8 The most useful explanations of optimal control theory are Athans, Michael and Falb, Peter L., Optimal Control (New York: McGraw-Hill, 1966)Google Scholar; Bryson, Arthur E. Jr. and Ho, Yu-Chi, Applied Optimal Control (Valtham, Mass.: Ginn and Co., 1969)Google Scholar; Citron, Stephen J., Elements of Optimal Control (New York: Holt, Rinehart and Winston, 1969)Google Scholar; Cruz, Jose B. Jr., ed., Feedback Systems (New York: McGraw-Hill, 1972)Google Scholar; Dyer, Peter and McReynolds, Stephen R., The Computation and Theory of Optimal Control (New York: Academic Press, 1970)Google Scholar; Hsu, Jay C and Meyer, Andrew U., Modern Control Principles and Applications New York: McGraw-Hill, 1968)Google Scholar; Ogata, Katsuhiko, Modern Control Engineering (Englewood Cliffs, N.J.: Prentice-Hall, 1970)Google Scholar; Perkins, William R. and Cruz, Jose B. Jr., Engineering of Dynamic Systems (New York: John Wiley and Sons, 1969)Google Scholar; Varaiya, Pravin P., Notes on Optimization (New York: Van Nostrand Reinhold, 1972)Google Scholar. See also: Arrow, Kenneth, Applications of Control Theory to Economic Growth (Stanford, Cal.: fastitute for Mathematical Studies in Social Science, Technical Report #2, Stanford University, July, 1968)Google Scholar; Dorfman, Robert, “An Economic Interpretation of Optimal Control Theory,” American Economic Review, 10 (December, 1969), 817831 Google Scholar; Intriligator, Michael D., Mathematical Optimization and Economic Theory (Englewood Cliffs, N.J.: Prentice-Hall, 1971)Google Scholar; Gillespie, John. V., “Optimal Control Theory and Comparative Foreign Policy: A Promising Approach to Future Research,” in In Search of Global Patterns, ed. Rosenau, James N. (New York: Free Press, forthcoming)Google Scholar and Some Observations on Dynamic Modeling,” in Measurement and Research Design in Political Science, ed. Leege, David (Chicago: Aldine, forthcoming)Google Scholar.

9 Not all models in which manipulable variables appear are controllable. m general, if the desired state is specified for all time, the requirements for the existence of a control input that will generate the desired x(t) are very stringent. A less ambitious but more realistic goal is to require only a partial specification of the state variables. One such partial specification is forcing the state of the system to attain a specified value at some finite time in the future. That is, given an initial time, t 0, an initial state x(t0)=x0 , and a final state xf, t0 tt + T, for some finite T, such that s(t0 + T) = xt, there may or may not be any control, u(t), which can force the system to attain the state xf . By a suitable choice of error coordinates such as state variables, the problem of reaching and maintaining a specified state is the problem of matching a desired dynamic response. A system is said to be completely state-controllable if, for any initial x0 , for any initial time t0 , it is possible to generate an unconstrained control vector, u(t), that will take any given initial state x(t0) to any final state x(tf) in a finite time interval t0 ttf For a linear system, the final state may be taken to the origin without any loss of generality. The model we have developed here is completely state-controllable.

10 Bellman, Richard E., Dynamic Programming (Princeton, N.J.: Princeton University Press, 1957)Google ScholarPubMed; Pontryagin, L. S., Boltyanskii, V. G., Gamkrelidge, R. V. and Mishchenko, E. F., The Mathematical Theory of Optimal Processes, trans. Trirogoff, K. M. (New York: Wiley Interscience, 1962)Google Scholar.

11 By obtaining an optimal trajectory in this way we are incorporating feedback into the model. Feedback in our case will allow countries to respond to the foreign policy decisions of other countries. A solution which incorporates feedback is a closed-loop solution. It is closed-loop in the sense that the output from the model is an input at a later time in the dynamic process.

12 Richardson, p. 16.

13 See, for example: Zinnes, Dina A., “An Analytical Study of the Balance of Power Theories,” Journal of Peace Research, 4 (July, 1967),270288 CrossRefGoogle Scholar, and Coalition Theories and the Balance of Power,” in The Study of Coalition Behavior, ed. Groennmgs, Sven, Kelley, E. W. and Leiserson, Michael (New York: Holt, Rinehart and Winston, 1970),351–36Google Scholar & See also: Qaude, Inis L. Jr., Power and International Rektions (New York: Random House, 1962),1193 Google Scholar; Pollard, A. F., ‘The Balance of Power,” Journal of the British Institute of International Affairs, 2 (March, 1923), 5364 CrossRefGoogle Scholar; Haas, Ernst B., ‘The Balance of Power: Prescription, Concept, or Propaganda?World Politics, 5 (July, 1953), 442477 CrossRefGoogle Scholar.

14 Although the variable u(t) is manipulable by the decision maker, if and only if the model is completely state-controllable is it the case that a manipulable variable becomes a control variable. For our model the condition of controllability is satisfied. We are assuming that the variable u(t) is completely manipulable, i.e., in principle, any values of u(t) can be chosen.

15 For block diagramming and network methods, see Perkins and Cruz, pp. 11–94.

16 Our analysis makes use of the Ricatti equations whereby the equations allow decomposition because certain terms must equal zero. The general form of our model is the “regulator problem with a Unear system and quadratic cost.” See Varaiya, pp. 176–184.

18 Since we have not specified any “scrap value,” i.e., value that must be shown by x(t) when t = T, the adjoint variables at time p(T) must be equal to zero. The adjoint variables are composed only of the state equation and contain no additional constraints. This property holds for all models of the general form of the linear-quadratic reguktor problem.

19 Because in equation (26), k1 is dependent on x(T) and in equation (24) k1(t) contains no k2 terms, it is the case that k1(t) is a zero function. In equation (25) k2(t) is dependent on k1(t), butinequation (26) it must be the case that k2(T) is equal to 0.

20 The assumption that all parameters are positive is a very strong assumption. It can be shown that Richardson could have obtained his results with a less strict assumption. The quantity (b – la) is a very important quantity for this model as will be demonstrated below.

21 The assumption that a nation has a given objective function should not be thought to be unnecessarily strict because the objective function used here is sufficiently general to incorporate many differing instances. It is important to note that our derivation is both necessary and sufficient.

22 The method of analysis here can be described as: Find a G(λ) such that F[α, β, γ, G(*#x03BB;)] meets some criterion.

23 The associated measures of significance in ordinary least-squares analysis do not apply in our case. This is because we do not have, strictly speaking, a Unear estimation equation. We have “Unearized” equation (36) by using pseudoparameters, one of which is not chosen strictly by least-squares analysis.

24 In any minimization one may encounter local minima (shallow valleys in a hypersurface separated by hills from deeper valleys) which may mask themselves as global minima (the deepest valley in the hypersurface). To assure that we have obtained a global minimum we have begun our analysis from several randomly selected initial values and have required convergence of final estimates from these initial values.

25 See Brent, Richard P., Aleorithms for Minimization with Derivatives (Englewood Cliffs, N.J.: Prentice-Hall, 1973).Google Scholar

26 Powell, M. J. D.An Efficient Method for Finding the Minimum of a Function of Several Variables without Calculating Derivatives,” Computer Journal, 7 (July, 1964), 155162.Google Scholar

27 Davidon, William C., Variable Metric Method of Minimization, rev. ed. (Washington, D.C.: Atomic Energy Commission Research and Development Report, ANL-5990,1959)Google Scholar.

28 Our criterion was convergence. If for severalruns the analysis produced the same minimization, we assumed that a global minimum was found. The Davidon-Powell method is not constrained by the range selected for initial values. Values outside of the range are eligible as minima.

29 International Institute for Peace and Conflict Research, SIPRI Yearbook of World Armaments and Disarmaments (Stockhohn: Stockholm International Peace Research mstitute, 1968 and forward)Google Scholar. Our data sets run from 1947-1972 for the United States and Soviet Union; 1950–1972 for NATO, WTO, Israeland Arab states.

30 See Becker, Abraham S., Soviet Military Outkys Since 1955 (Rand Corporation Memorandum RM-3886 PR) (Santa Monica: The Rand Corporation, 1964)Google Scholar. To adjust for the Soviet accounting change, the mean value of the four years after 1960 was compared to the mean value of the four years immediately prior to 1960. The prior-1960 mean value was subtracted from the post-1960 mean value, and this mean difference was then subtracted from all post-1960 total defense expenditures. This adjusted Soviet expenditure was used in calcuhting the WTO aggregate defense expenditure.

31 The Arab nations were defined as Egypt (UAR), Syria, and Jordan. The data are expressed in terms of noninflationary dollars using mean yearly market exchange rates for determining conversion into American dollars. The rates of inflation were obtained from the Stockhomi International Peace Research Institute.

32 Autocorrelation is not the only statistical problem in time-series analysis. Multicollinearity is an additional problem. By the very nature of our model, one might expect multicollinearity. Our analyses show that there is some multicollinearity in our data but that it is not particukrly disturbing. There are no agreed-upon methods for treating multicollinearity in time-series analysis. Some may challenge the need for treating autocorrektion in a model with a lagged endogenous variable. Once again there is no agreement on whether adjustments for autocorrelation are meaningful in the kind of model we have posited. See Schrodt, Philip A., The Rektionship Between Arms Races and the Preservation of Peace (Boomington: Indiana University, Ph.D. dissertation, 1976), chapter 7Google Scholar; and Nerlove, Marc and Wallis, Kenneth F., “Use of the Durbin-Watson Statistic in blappropriate Situations,” Econometrica, 34 (March, 1966), 235238 CrossRefGoogle Scholar. The conclusions from our analyses are the same, whether or not corrections for autocorrelation are made. More conservative findings are obtained when the correction is made. However, by no means do we fully endorse use of the Durbin-Watson statistic or the Geary sign test for systems with togged endogenous variables. We have used these analyses because they do not alter the conclusions, and because they provide more conservative estimates of the parameters.

33 See Johnston, John, Econometric Methods, 2nd ed. (New York: McGraw-Hill, 1972), pp. 246–266 and 312313 Google Scholar; Goldberger, Arthur S., Econometric Theory (New York: John Wiley and Sons, 1964), pp. 153–155, 267–268 and 270272 Google Scholar.

34 Durbin, J. and Watson, G. S., ‘Testing for Serial Correkttion in Least Squares Regression, I,” Bio-metrika, 37 (June, 1950), 409428 Google Scholar, and Testing for Serial Correiation in Least Squares Regression, II,” Biometrika, 38 (June, 1951), 159178 CrossRefGoogle Scholar; Habibagahi, Hamid and Pratschke, John L., “A Comparison of the Power of the Von Neumann Ratio, Durbin-Watson and Geary Tests,” Review of Economics and Statistics, 54 (May, 1972), 179185 CrossRefGoogle Scholar; Durbin, J., “Estimation of Parameters in Time-Series Regression Modek,” Journal of the Royal Statistical Society, Series B, 22 (January, 1960), 139153 Google Scholar; Cochrane, D. and Orcutt, G. H., “Application of Least-Squares Regression to Rektion-ships Containing Autocorrekited Error Terms,” Journal of the American Statistical Assocktion, 44 (March, 1949), 3261 Google Scholar.

35 Kadiyala, Koteswara Rao, “A Transformation Used to Circumvent the Problem of Autocorrektion,” Econometrica, 36 (January, 1968), 9396 CrossRefGoogle Scholar.

36 In obtaining the parameter from this analysis, γ has been standardized by dividing by the autocorrektion parameter, The reader should note that, whereas GLS provides more conservative findings, the conclusions are the same whether the analysis is completed under GLS or OLS.

37 Care must be taken in interpreting these results, given the measures of fit in Tables 1 and 2.

38 Richardson and his followers have accepted the idea that all parameters must be positive. See Richardson and, for example, D. L. Wagner et al.

39 See for example Smoker's work, and Caspary.

40 It must be remembered that the parameter b is multiplied by a negative unity in the state equation.

41 For NATO all the signs ofthe coefficients are in the direction Richardson stiputated. See Richardson.

42 For readable summaries of equillbrium analysis, see Intrifigator, Mathematical Optimization, pp. 220257 Google Scholar; Perkins and Cruz, pp. 72–78.

43 Since our solution is for a steady-state equilibrium, one must be careful not to interpret equilibrium as total disarmament. Equilibrium for our analyses simply means that there the rate of change in armaments is zero, not that armaments expenditure becomes zero.

44 In equilibrium, if equals zero, it is not the case that u is equal to zero. The nation U is the controller in our model and may increase or decrease its armaments expenditure while nation X is in equilibrium.

45 This method has been shown to be entirely tegitimate. See, Weiss, Leonard and Inifante, E. F., “On the Stability of Systems Defined over a Finite Time Interval,” Proceedings of the National Academy of Sdences, 54 (July 15, 1965), 4448 CrossRefGoogle Scholar. Normally one assumes T to be infinity, but such an assumption is not appropriate for our analysis. The actual value of T is irrelevant.

46 For the optimal control reguktor problem of the form here, the assumption that equillbrium and stabllity exist in an infinite time horizon is incompatible with the boundary conditions used to solve for u*(t). Hence the weaker, but still legitimate, assumption of setting T equal to a krge number is employed.

47 For this analysis, estimates of the constant h needed to be derived. Consistent with our analysis is the use of the mean difference in expenditures. For our analysis h is equal to the following values for the six cases.

48 This numerical evaluation uses the values of h in footnote 47 and sets (T - t0 ) equal to numbers ranging from 50 to 1.

49 The actual values for the equliibrium are mean-ingless in that we have set the initial conditions for all nations equal to a small positive number. The numbers are interpretable in terms of whether or not the values yielded using series of (T - t0) numbers are about the same.

50 Liapunov, Aleksandr M., Stability of Motion (New York: Academic Press, 1966)Google Scholar; Liephote, Horst, Stability Theory (New York: Academic Press, 1970)Google Scholar.

51 For equation (56) from (55):

52 An examination of equation (55) will show that when (la - b) = -∞ then x(t) is equal only to the forcing function.

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