The space satellite shown in Figure DP5.4(a) uses (b) a control system to readjust its
Chapter 0, Problem DP5.4(choose chapter or problem)
The space satellite shown in Figure DP5.4(a) uses (b) a control system to readjust its orientation, as shown in Figure DP5.4(b). (a) Determine a second-order model for the closed- (c ) loop system. Using the second-order model, select a gain K so that the percent overshoot is less than 15% and the steady-state error to a step is less than 12%. Verify your design by determining the actual performance of the third-order system.
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