a)is the aircraft stable about the equilibrium represented by the transfer function?b) Using proportional feedback,what is the range of acceptable gains for the closed loop systen to be stable?c) Design a feedback control system that allows the pilot to command a pitch angle with overshoot less than or equal to 4.15% and a natural frequency of greater than or equal to 0.99 rad/sd) Design a feedback control system that allows the pilot to command a pitch angle with the same overshoot and a natural frequency of one half the system in part c. 2) An aircraft2/8/2e(s)₂ (5)designNc) DesignisS-4s²-0.65 +9• pitch angle (radians)Se elevator deflection (radians)open loop transfer functionstablaa) Is the aircraft "about the equilibrium represent by (3)theofb) using proportional feedback, what isgaindacceptablerangethe closed loop system to be stable?a feedback control system that allows the pilot topitchanglewith overshoot less than oregud!!to10.98 reda4.15% and a noturd frequency of greater than ord) Design a feedback control system that allows the pilot tocommand a pitch angle with the same overshoot and aof the half of system in part c)naturalEvegueray

Answered: a)is the aircraft stable about the…

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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a)is the aircraft stable about the equilibrium represented by the transfer function?

b) Using proportional feedback,what is the range of acceptable gains for the closed loop systen to be stable?

c) Design a feedback control system that allows the pilot to command a pitch angle with overshoot less than or equal to 4.15% and a natural frequency of greater than or equal to 0.99 rad/s

d) Design a feedback control system that allows the pilot to command a pitch angle with the same overshoot and a natural frequency of one half the system in part c.

2) An aircraft
2/8/2
e(s)
₂ (5)
design
N
c) Design
is
S-4
s²-0.65 +9
• pitch angle (radians)
Se elevator deflection (radians)
open loop transfer function
stabla
a) Is the aircraft "about the equilibrium represent by (3)
the
of
b) using proportional feedback, what is
gaind
acceptable
range
the closed loop system to be stable?
a feedback control system that allows the pilot to
pitch
angle
with overshoot less than or
egud!!
to
10.98 red
a
4.15% and a noturd frequency of greater than or
d) Design a feedback control system that allows the pilot to
command a pitch angle with the same overshoot and a
of the half of system in part c)
natural
Evegueray

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