File Name: Analytics – Projectile Motion
Location: Modeling Toolkit | Analytics | Projectile Motion
Brief Description: Uses simulation to compute the probabilistic distance a missile will travel given the angle of attack, initial velocity, and probability of midflight failure
Requirements: Modeling Toolkit, Risk Simulator
This example illustrates how a physics model can be built in Excel and simulated, to account for the uncertainty in inputs. This model shows the motion of a projectile (e.g., a missile) launched from the ground with a particular initial velocity, at a specific angle. The model computes the height and distance of the missile at various points in time and maps the motion in a graph. Further, we model the missile’s probability of failure (i.e., we assume that the missile can fail midflight and is a crude projectile, rather than a smart bomb, where there is no capability for any midcourse corrections and no onboard navigational and propulsion controls).
We know from physics that the location of the projectile can be mapped on an x-axis and y-axis chart, representing the distance and height of the projectile at various points in time, and those x-axis and y-axis values are determined by:
In addition, we can compute the following assuming that there is no midflight failure:
The inputs are initial velocity, angle, time step, and failure rate (Figure 5.1). Time step (delta t) is any positive value representing how granular you wish the distance and height computations to be, in terms of time. For instance, if you enter 0.10 for time steps, the time period will step 0.1 hours each period.
Figure 5.1: Assumptions in the missile trajectory model
Velocity, angle, and the failure rate can be uncertain and hence subject to simulation. The results are shown as a table and graphical representation. The failure rate is simulated using a Bernoulli distribution (yes-no or 0-1 distribution, with 1 representing failure, and 0 representing no failure), as seen in Figure 5.2. Figure 5.3 illustrates the sample flight path or trajectory of the missile.
Figure 5.2: Missile coordinates midflight and probability of missile failure
Figure 5.3 Graphical representation of the missile flight path
This model has preset assumptions and forecasts, and is ready to be run by following these steps:
Figure 5.4: Probabilistic forecast of a projectile’s range
Alternatively, you can recreate the model assumptions and forecast by following these steps:
Figure 5.5: Simulating midflight failures