The phase plane is a broad term, but we limit ourselves here to the cross-plot between the position and the velocity of a moving mass. Such a plot can be useful to get a grip on some non-linear system behaviour.
Some basic properties are :
| (1) |
| (2) |
Here x is the position, v is the velocity, and a is the acceleration of the moving mass. The dot is Newton's symbol for the derivative with respect to time. Figure 1 shows what will happen next.
The point will move to the right in the plot with the velocity x• = v. It will move faster in direct proportion to its ver­tical coordinate, because that represents the velocity v. At the same time, the point will also move upward at a rate of v • = a. The figure shows that the resulting motion has a slope of a / v.
A simple corollary is that the slope is "infinite" for v = 0. This is obvious anyway : since v = 0 means x • = 0, a point on the horizontal axis can only move vertically away from it. In other words, the trajectories can only cross the horizontal axis orthogonally.
Figure 1 : Phase plane acceleration.
From high school math we remember that when starting from standstill, the movement for a constant accel­eration is described by :
| (3) |
| (4) |
Suppose we can accelerate a mass with a maximum acceleration amax, and maximum deceleration −amax. Substituting t from (3) into (4) we have :
| (5) |
This is the equation of a parabola, but since it expresses x in terms of v, the parabola lies its side in the phase plane plot. Figure 2 shows the result. If we start from rest in the origin, then accelerate for a certain time T, and then decelerate to zero again, we will have covered a distance of x = ½ amax T 2, in a time 2 .T.
Halfway, we reached a maximum velocity of v = amax . T. For the maximum acceleration that was available, this distance could not have been covered faster. This is why this is called a "minimum time manoeuver".
The "control law", if you like, that underlies this manoeuver is : maximum to halfway, and negative maximum over the second half, starting the deceleration "just in time". This strategy is aptly called "bang-bang control". It is highly nonlinear. The phase plane method lends itself very well to the analysis of nonlinear control laws.
Figure 2 : Minimum time manoeuvre.
Another quite common constraint is that of a maximum velocity. Taken to the extreme, we have instantaneous v = vmax, with a distance covered of x = vmax . T. This trajectory shows up in the phase plane plot as a block.
If both a maximum acceleration and a maximum velocity apply, we get Figure 3. This combines the parabolic sections of Figure 2 with a straight intermediate stretch of constant maximum velocity and zero acceleration.
This constant speed part is often called the "coasting phase". The equations are more or less obvious, if T is the coasting period.
Figure 3 : Minimum time with coasting phase.
We briefly discuss the case of a pendulum, or a mass-spring-damper system.
This is a linear system, and the phase plane plot is not very useful in this case. We discuss it only because the plot bears a superficial resemblance to the far more useful eigenvector plot, and we wish to prevent any confus­ion between the two.
The equations of motion for a mass-spring-damper system centered on the origin are :
| (6) |
Here m is the mass, k is the stiffness, and b is the damping.
From this we see that for x = 0 :
| (7) |
This shows that the vertical axis is crossed
at a slope of
v• / x•
= a / v =
−b / m.
From (2) we concluded that the horizontal axis
This allows us to sketch the trajectory as in Figure 4. From the signs in (2), the point will always move clock­wise. The trajectory is a kind of slanted spiral. We will see elsewhere that the eigenvector plot is more appropri­ate to this problem, and that it produces a true spiral which by convention rotates anti-clockwise.
Figure 3 : Mass-spring-damper system.