The block diagram given below represents a satellite attitude control system (employing both angle and angular...

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The block diagram given below represents a satellite attitude control system (employing both angle and angular velocity measurements). er(s) K W(s) K2 115 115 S e(s) a. With W(S) = 0, find the transfer function between 0,(s) and 0(s). Do this by manipulating the block diagram (4 pts). b. With 0,(s) = 0, find the transfer function between W(s) and 0(s). Do this analytically (with equations), without manipulating the block diagram (4 pts). The block diagram given below represents a satellite attitude control system (employing both angle and angular velocity measurements). er(s) K W(s) K2 115 115 S e(s) a. With W(S) = 0, find the transfer function between 0,(s) and 0(s). Do this by manipulating the block diagram (4 pts). b. With 0,(s) = 0, find the transfer function between W(s) and 0(s). Do this analytically (with equations), without manipulating the block diagram (4 pts).