i need the answer quickly Consider the lateral position control system for a landing on aircraft carrier.K(s+0.3)1R(s)Y(s)(s-2)(s2+10s+45)The range of K for stability isa) K <260.68b) 50.06 0

The system in a control system is described by the transfer function of the system. Any system…

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Consider the lateral position control system for a landing on aircraft carrier. R(s) K(s+0.3) Y(s) (s-2(s²+10s+45) The range of K for stability is a) K <260.68 b) 50.06 0

Power System Analysis and Design (MindTap Course List)

6th Edition

ISBN:9781305632134

Author:J. Duncan Glover, Thomas Overbye, Mulukutla S. Sarma

Publisher:J. Duncan Glover, Thomas Overbye, Mulukutla S. Sarma

Chapter6: Power Flows

Section: Chapter Questions

Problem 6.6MCQ

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i need the answer quickly

Consider the lateral position control system for a landing on aircraft carrier.
K(s+0.3)
1
R(s)
Y(s)
(s-2)(s2+10s+45)
The range of K for stability is
a) K <260.68
b) 50.06 <K <123.98
c) 100.12 <K <260.68
d) The system is unstable for all K >0

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