Question

The figure below shows the block diagram of a space vehicle attitude control system. Determine the proportional gain constant Kp and Tsuch that the bandwidth of the closed-loop system is around 0.55 rad/sec and an overshoot of around 9%. Note that the closed-loop bandwidth is close to the gain crossover (cut-off) frequency. Check your design in both frequency and time domain and comment. Determine the maximum overshoot and the settling time. Determine as well -using the Bode diagram -the expression of the steady state closed loop output for a sinusoidal input with 0 deg phase, unity amplitude, and a frequency of Irad/sec.

Determine the proportioanl gain constant Kp and T such that the bandwidth of the closed-loop system is around 0.55 rad/sec and an overshoot of around 9%. Note that the closed-loop bandwidth is close to the gain crossover (cut-off) frequency. Check your design in both frequency and time domain and comment. Determine the maximum overshoot and settling time. Determine as well, using a Bode diagram, the expression of the stead state closed loop output for a sinusodial input with 0 deg phase, unity amplitude and a frequecny of 1 rad/sec.

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