Matlab simulink problem

The following is a linearized state space model of the helicopter shown below. Simulate the system from 0 to 10 sec usingthe Simulink for the unit step input of rotor tilt angle ?. 2. -0.4 0-0.011 ?6.31 Fuselage reference -1.4 9.8-0021 L9.8 axi Ve 0//Rotor thrust where q = pitch rate pitch angle of fuselage u-horizontal velocity (assume measured feedback) 6 rotor tilt angle (control input) Rotor Output (ltems to be submitted) Simulink diagram using SS model block Plot the horizontal velocity from 0-10 sec. Don't forget to include axes labels and title of each plots The following is a linearized state space model of the helicopter shown below. Simulate the system from 0 to 10 sec usingthe Simulink for the unit step input of rotor tilt angle ?. 2. -0.4 0-0.011 ?6.31 Fuselage reference -1.4 9.8-0021 L9.8 axi Ve 0//Rotor thrust where q = pitch rate pitch angle of fuselage u-horizontal velocity (assume measured feedback) 6 rotor tilt angle (control input) Rotor Output (ltems to be submitted) Simulink diagram using SS model block Plot the horizontal velocity from 0-10 sec. Don't forget to include axes labels and title of each plots