Question

For the following control System: • Conduct test (without the controller) using open loop configuration or close loop configuration. • Give example if we input something what will be the output. • Find the %overshoot and Settling time and peak time and the steady state error. • Then improve the value of the %overshoot and Settling time and peak time and the steady state error to get better value than what we got above. • Design a controller using one of the following technic state feedback and state observer or using LQR or using modern control system or using integral control (using hand calculation) • then test the design if its working fine or not. Pitch Control System Pitch command Commanded Pitch gain elevator deflection Elevator Elevator Vehicle actuator deflection dynamics Pitch $\theta_c(s)$ + $-K_1$ + $\delta_c(s)$ $\frac{2}{s+2}$ $\delta_c(s)$ $\frac{-0.125(s+0.435)}{(s+1.23)(s^2+0.226s+0.0169)}$ $\theta(s)$ Pitch rate sensor $-K_2s$

          For the following control System:
• Conduct test (without the controller) using open loop configuration or close loop configuration.
• Give example if we input something what will be the output.
• Find the %overshoot and Settling time and peak time and the steady state error.
• Then improve the value of the %overshoot and Settling time and peak time and the steady state
error to get better value than what we got above.
• Design a controller using one of the following technic state feedback and state observer or using
LQR or using modern control system or using integral control (using hand calculation)
• then test the design if its working fine or not.
Pitch Control System
Pitch
command
Commanded
Pitch gain
elevator
deflection
Elevator Elevator
Vehicle
actuator deflection
dynamics
Pitch
$\theta_c(s)$ + $-K_1$ + $\delta_c(s)$ $\frac{2}{s+2}$ $\delta_c(s)$ $\frac{-0.125(s+0.435)}{(s+1.23)(s^2+0.226s+0.0169)}$ $\theta(s)$
Pitch rate
sensor
$-K_2s$

For the following control System:
• Conduct test (without the controller) using open loop configuration or close loop configuration.
• Give example if we input something what will be the output.
• Find the %overshoot and Settling time and peak time and the steady state error.
• Then improve the value of the %overshoot and Settling time and peak time and the steady state
error to get better value than what we got above.
• Design a controller using one of the following technic state feedback and state observer or using
LQR or using modern control system or using integral control (using hand calculation)
• then test the design if its working fine or not.
Pitch Control System
Pitch
command
Commanded
Pitch gain
elevator
deflection
Elevator Elevator
Vehicle
actuator deflection
dynamics
Pitch
(s) + -K1 + (s) (2)/(s+2) (s) (-0.125(s+0.435))/((s+1.23)(s^2+0.226s+0.0169)) θ(s)
Pitch rate
sensor
-K2s

Added by Katherine D.

Question

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