The attitude control system of a space shuttle rocket is shown in Figure DP6.4 [17]. (a)
Chapter 0, Problem DP6.4(choose chapter or problem)
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).
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