Monte Carlo Simulation of Dynamic Systems in VS .NET

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Monte Carlo Simulation of Dynamic Systems
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(b) Sequential Monte Carlo Studies
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Instead of computing Monte Carlo statistics after n repeated simulation runs, we can accumulate sample averages after every simulation run The following experiment-protocol script first initializes the sample averages xAvg and xxAvg and then again loops to make n simulation runs with new parameter and initial-condition values At the end of the ith run, the program reads x = x(t0 + TMAX) = x(i) and updates the statistics values:
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xAvg = 0 | xxAvg = 0 | -initialize statistics computation for i = 1 to n | -Monte Carlo loop b = b0 + B * f1(ran()) | -set a new random parameter value q = q0 + C * f2(ran()) | -set a new random initial value -drunr | -make a simulation run and reset state variables x[i] = X | -read successive sample values of x =X(t0 + TMAX) -----------------------------------------------now accumulate statistics! xAvg = xAvg + (x - xAvg)/n xxAvg = xxAvg + (x^2 - xxAvg)/n xVar = xxAvg - xAvg^2 next | -and loop back
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This technique can save time, for it permits us to terminate the study when the sample variance has become sufficiently small (sequential Monte Carlo simulation)
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(c) Example: Effects of Gun-elevation Errors on the 1776 Cannon
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We will study a continuous random process generated by a differentialequation system with a random parameter, specifically a random initial value Similar programs apply directly to many Monte Carlo studies of manufacturing-tolerance effects Simulation of the 1776 cannon5 in Figure 4-2 has been used as a textbook problem for over 50 years [6,7] Assuming that the wind force W(t) is zero, the only forces acting on the spherical cannonball are its weight mg and aerodynamic drag opposing the velocity vector Airspeed is relatively low, so that the drag is roughly proportional to the square of the velocity Referring to Figure 4-2, the equations of motion in the horizontal and vertical directions are
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(d/dt) x = xdot (d/dt) y = ydot (d/dt) xdot = R v2 cos = R v xdot (d/dt) ydot = R v2 sin g = R v ydot g
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1776 gun elevations were not really affected by manufacturing errors Elevations of land-based guns were usually set with wedges under the rear part of the barrel, and naval-gun elevation also required judgment of the ship s roll angle Either way, there were lots of random errors
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Parameter-influence Studies, Model Replication, and Monte Carlo Simulation
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FIGURE 4-2 Cannon geometry (based on Reference [6]) We assume that the wind force W(t) is zero
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v = sqrt(xdot2 + ydot2)
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The acceleration due to gravity g = 322 ft/s2 and R = 75E-05 ft 1 is the drag coefficient divided by the projectile mass The trajectory of each shot is then determined by the initial muzzle position x(0) = y(0) = 0 and the initial velocity components
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xdot(0) = v0 * cos(theta0) ydot(0) = v0 * sin(theta0)
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theta0 is the gun elevation angle, and v0 = 900 ft/s is the given muzzle velocity Assuming level ground, the impact abscissa xI is the value of x where y = 0 at the end of a trajectory A good way to read xI is with the track-hold differ-
ence equation
xI = xI + swtch(y) * (x - xI)
(Section 2-16b), which causes xI to track x while and then holds the x value The initial value of the difference-equation state variable xI defaults to 0 To aim the cannon, we set the elevation angle theta0 to obtain a desired impact abscissa xI, say theta0 = 70 * PI/180 Our Monte Carlo study then adds random perturbations to this nominal gun elevation and determines their effect on the sample average and sample variance of the impact coordinate xI To get approximately Gaussian-distributed elevation errors, we set
theta0 = 70 * PI/180 + a * (ran()+ran()+ran()+ran())
Monte Carlo Simulation of Dynamic Systems
Since ran() is uniformly distributed between 1 and 1 with expected value 0 and theoretical variance 1/3, we have
E{theta0} = 70 PI/180 Var{theta0} = 4 * a2/3
Figure 4-3 shows time histories of x(t) and the track-hold output xI(t) for a few simulation runs together with the complete program for the repeated-run Monte Carlo study The program also displays the resulting sample average xavg and the sample statistical dispersion s = sqrt(abs(xxavg xavg^2)) of the impact abscissa xI after n runs