Abstract
In the method of analysis presented, phase plane techniques have been successfully modified to cater to a class of third order non-linear systems. This method is applicable to control systems having non-linearities in the feedback loops.
The technique involves plotting an (x1, x3) master plane having all possible trajectories for any non-zero value of x2. The variation and initial conditions of variable x2 are incorporated by adding a set of x3-scales, and an origin shift scale, for various values of x2, to the (x1, x3) master plane. Using this master plane, the required (x1, x2 and (x1, x3) trajectories can be obtained for any set of initial conditions, by following the procedure illustrated by typical examples.