The attitude control system of a space shuttle rocket is shown in Figure DP6.4 [17].
(a) Determine the range of gain K and parameter m so that the system is stable, and plot the region of stability.
(b) Select the gain and parameter values so that the steady-state error to a ramp input is less than or equal to 10% of the input magnitude.
(c) Determine the percent overshoot for a step input for the design selected in part (b).
Figure DP6.4
Shuttle attitude control.

Transcribed Image Text:

Space shuttle rocket Controller Ris) Attitude