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Consider the attitude dynamics of an aircraft with a transfer function 2s+0.1 G(s) s(s´+0.1s+4) Determine the transient response specifications, including Peak Time, Settling Time, Damping Ratio and Overshoot (%).

Consider the attitude dynamics of an aircraft with a transfer function 2s+0.1 G(s) s(s´+0.1s+4) Determine the transient response specifications, including Peak Time, Settling Time, Damping Ratio and Overshoot (%).

Elements Of Electromagnetics
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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Consider the attitude dynamics of an aircraft with a transfer function 2s+0.1 G(s) s(s'+0.1s+4) Determine the transient response specifications, including Peak Time, Settling Time, Damping Ratio and Overshoot (%).
Transcribed Image Text:Consider the attitude dynamics of an aircraft with a transfer function 2s+0.1 G(s) s(s'+0.1s+4) Determine the transient response specifications, including Peak Time, Settling Time, Damping Ratio and Overshoot (%).
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