Kindly answer all. Please skip if you're not interested to answer them.Thank you! CommandedPitchelevator Elevator ElevatorVehiclecommandPitch gaindeflection actuator deflectiondynamicsPitch0,(8)28,(s)-0.125(s+0.435)-K,s+2(s+1.23)(s²+0.226s+0.0169)Pitch ratesensor-K,sFIGUREPitch control loop for the UFSS vehiclea. Using only the second-order poles shown in the transfer function, predictpercent overshoot, rise time, peak time, and settling time.b. Using Laplace transforms, find the analytical expression for the response of thepitch angle to a step input in elevator surface deflection.c. Evaluate the effect of the additional pole and zero on the validity of the second-order approximation.d. Plot the step response of the vehicle dynamics and verify your conclusions foundin (c).

Initial Step According to Given Data:-

Commanded elevator Elevator Elevator deflection actuator deflection Pitch Vehicle command Pitch gain dynamics Pitch 2 8,(s) -0.125(s+0.435) -K, s+2 (s+1.23)(s²+0.226s+0,0169) Pitch rate sensor -K,8 FIGURE Pitch control loop for the UFSS vehicle a. Using only the second-order poles shown in the transfer function, predict

Commanded elevator Elevator Elevator deflection actuator deflection Pitch Vehicle command Pitch gain dynamics Pitch 2 8,(s) -0.125(s+0.435) -K, s+2 (s+1.23)(s²+0.226s+0,0169) Pitch rate sensor -K,8 FIGURE Pitch control loop for the UFSS vehicle a. Using only the second-order poles shown in the transfer function, predict

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Question

Kindly answer all.

Please skip if you're not interested to answer them.

Thank you!

Commanded
Pitch
elevator Elevator Elevator
Vehicle
command
Pitch gain
deflection actuator deflection
dynamics
Pitch
0,(8)
2
8,(s)
-0.125(s+0.435)
-K,
s+2
(s+1.23)(s²+0.226s+0.0169)
Pitch rate
sensor
-K,s
FIGURE
Pitch control loop for the UFSS vehicle
a. Using only the second-order poles shown in the transfer function, predict
percent overshoot, rise time, peak time, and settling time.
b. Using Laplace transforms, find the analytical expression for the response of the
pitch angle to a step input in elevator surface deflection.
c. Evaluate the effect of the additional pole and zero on the validity of the second-
order approximation.
d. Plot the step response of the vehicle dynamics and verify your conclusions found
in (c).

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