Figure Q2 shows the block diagram of a flight control system. a) Derive the system transfer function. b) Find out the system gain, natural frequency and damping ratio for this system based on the standard form of second order systems. c) If K1 = 2 and K2 = 10, use the standard response sheet to find out the system steady-state value, overshoot and 63% rise time, with a unit step input
Figure Q2 shows the block diagram of a flight control system. a) Derive the system transfer function. b) Find out the system gain, natural frequency and damping ratio for this system based on the standard form of second order systems. c) If K1 = 2 and K2 = 10, use the standard response sheet to find out the system steady-state value, overshoot and 63% rise time, with a unit step input
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Figure Q2 shows the block diagram of a flight control system.
a) Derive the system transfer function.
b) Find out the system gain, natural frequency and damping ratio for this system
based on the standard form of second order systems.
c) If K1 = 2 and K2 = 10, use the standard response sheet to find out the system
steady-state value, overshoot and 63% rise time, with a unit step input.
Transcribed Image Text:25
R(s) H
KI
C(s)
s(s+0.8)
K2s
Figure Q2. A flight control system
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