6- The altitude dynamics of a quad-rotor is given by the following equation: = 0.00925 8 where z is the altitude and 8 is control input parameter (a) Put the system in state space form. (b) Design a compensator to satisfy 5 = 0.95 and @n=6. (c) Design an estimator to have roots at s =-18, s = -16. (d) Draw the block diagram showing the controller and estimator. (e) Put the final system with compensator and estimator in state space form. 6- The altitude dynamics of a quad-rotor is given by the following equation: = 0.00925 8 where z is the altitude and 8 is control input parameter (a) Put the system in state space form. (b) Design a compensator to satisfy 5 = 0.95 and @n=6. (c) Design an estimator to have roots at s =-18, s = -16. (d) Draw the block diagram showing the controller and estimator. (e) Put the final system with compensator and estimator in state space form