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Feedback Systems E6.8 Designers have developed small, fast, vertical-take- off fighter aircraft that are invisible to radar (stealth aircraft). This aircraft concept uses quickly turning jet nozzles to steer the airplane [16]. The control sys- tem for the heading or direction control is shown in Figure E6.8. Determine the maximum gain of the sys- tem for stable operation. Aircraft dynamics (s + 20) s(s + J0)? Controller Y(s) R(s) Heading FIGURE E6.8 Aircraft heading control.

Feedback Systems E6.8 Designers have developed small, fast, vertical-take- off fighter aircraft that are invisible to radar (stealth aircraft). This aircraft concept uses quickly turning jet nozzles to steer the airplane [16]. The control sys- tem for the heading or direction control is shown in Figure E6.8. Determine the maximum gain of the sys- tem for stable operation. Aircraft dynamics (s + 20) s(s + J0)? Controller Y(s) R(s) Heading FIGURE E6.8 Aircraft heading control.

Introductory Circuit Analysis (13th Edition)
Introductory Circuit Analysis (13th Edition)
13th Edition
ISBN:9780133923605
Author:Robert L. Boylestad
Publisher:Robert L. Boylestad
Chapter1: Introduction
Section: Chapter Questions
Problem 1P: Visit your local library (at school or home) and describe the extent to which it provides literature...
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Control system stability 

Feedback Systems E6.8 Designers have developed small, fast, vertical-take- off fighter aircraft that are invisible to radar (stealth aircraft). This aircraft concept uses quickly turning jet nozzles to steer the airplane [16]. The control sys- tem for the heading or direction control is shown in Figure E6.8. Determine the maximum gain of the sys- tem for stable operation.
Transcribed Image Text:Feedback Systems E6.8 Designers have developed small, fast, vertical-take- off fighter aircraft that are invisible to radar (stealth aircraft). This aircraft concept uses quickly turning jet nozzles to steer the airplane [16]. The control sys- tem for the heading or direction control is shown in Figure E6.8. Determine the maximum gain of the sys- tem for stable operation.
Aircraft dynamics (s + 20) s(s + J0)? Controller Y(s) R(s) Heading FIGURE E6.8 Aircraft heading control.
Transcribed Image Text:Aircraft dynamics (s + 20) s(s + J0)? Controller Y(s) R(s) Heading FIGURE E6.8 Aircraft heading control.
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