6.3  Siacci’s Method 6.3.1  The Change of Independent Variables 

6.3  Siacci’s Method 

Siacci’s appr simplified their solutions.

6.3.1  The Change of Independent Variables 

Siacci introduced the “pseudovelocity” shown in Figure 6-2 as a new independent variable replacing time in our previous equations. The pseudovelocity is a velocity in the direction of the extended bore centerline which would give the correct component resolved along the x-axis. Then and are related by the equation.





(6.3-3) (6.3-4)

 Using equations (6.3-1) through (6.3-4) in equations (6.2-15) and (6.2-16) we can derive the following differential equations of bullet motion in terms of the new independent variable u :

(6.3-5) (6.3-6) (6.3-7) (6.3-8)

The initial conditions for the solution of these equations are:

t o = 0
u o = v m
x o = 0
y o = 0
(tan q ) o = tan q o        (6.3-9)

The velocity components v x and v y at any point in the trajectory are given by [equations (6.3-1) and (6.3-3)]:

v x = u cos q o
V y = v tan = u cos q tan q     (6.3-10)

and the total velocity is


We now have a set of first-order differential equations for the time of flight t , the range x , the vertical coordinate y , and the trajectory slope tan X. But these simplified equations of the bullet motion are still nonlinear coupled.