Control Systems Final - Problem 4
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4.      A lunar lander must land at the correct angle.  Using variable thrust, it is possible to produce a torque on the lander to change the vertical angle.  That torque turns the lander.  To control the angle, the system in the figure needs to be designed.

The transfer function for the lander (the "plant") is:

Gp(s) = 1/[100s2]

This system is particularly obnoxious to control, and it has been suggested to try a compensator of the form:

Gc(s) = Kc(s - z)/(s - p)

Answer the following questions.


Solution

        If you add a pole and a zero in a compensator, then the center of gravity will shift

We can't afford to shift the CG to the right, so we need to have the pole to the left of the zero.

        If we place the zero at s = -1, then, any pole to the left of that will make the system stable for all gains.  Here is the root locus for a pole at s = -1.1.  Careful examination of the pole locations (in Matlab, for example) shows that the closed loop poles are just barely into the LHP.  Clearly, to get the locus further into the LHP will require a pole much further to the left.

        Now, lets's consider trying to get a closed loop pole at -1 +1.5j.  Here is the root locus (actually, for the solution) that shows a pole at some point on the negative real axis.