CONTROL SYSTEMS ENGINEERING7th EditionNISE Publisher: WILEYISBN: 9781119185666
CONTROL SYSTEMS ENGINEERING
Solutions for CONTROL SYSTEMS ENGINEERING
Problem 4RQ:
Why are marginally stable systems considered unstable under the BIBO definition of stability?Problem 13RQ:
13. Does the presence of an entire row of zeros always mean that the system has poles?
Problem 1P:
Tell how many roots of the following polynomial are in the right half-plane. In the left half-plane,...Problem 2P:
Tell how many roots of the following polynomial are in the right half-plane, in the left half-plane....Problem 3P:
Using the Routh table, tell how many poles of the following function are in the right half-plane. in...Problem 5P:
Determine how many closed-loop poles lie in the right half-plane. In the left half-plane, and on the...Problem 6P:
Determine how many closed-loop poles lie in the right half-plane. In the left half-plane, and on the...Problem 8P:
Symbolic Math SM 8. Use MATLAB and the Symbolic Math Toolbox to generate a Routh table to solve...Problem 9P:
Determine whether the unity feedback system of Figure P6.3 is stable if [Section: 6.2]...Problem 11P:
Consider the unity feedback system of Figure P6.3 with Gs=14s2s2+2 Using the Routh-Hurwitz...Problem 12P:
In the system of Figure P6.3, let Gs=Ks+1ss2s+3 Find the range of K for closed-loop stability....Problem 13P:
Given the unity feedback system of Figure P6.3 with Gs=84ss7+5s6+12s5+25s4+45s3+50s2+82s+60 tell how...Problem 15P:
Given the unity feedback system of Figure P6.3 with Gs=8ss62s5s4+2s3+4s28s4 tell how many...Problem 16P:
Repeat Problem 15 using MATLAB.Problem 18P:
For the system of Figure P6.4, tell how many closed-loop poles are located in the right half-plane....Problem 19P:
Using the Routh-Hurwitz criterion, tell how many closed-loop poles of the system shown in Figure...Problem 20P:
Determine if the unity feedback system of Figure P6.3 with Gs=Ks2+1s+1s+2 can be unstable. [Section:...Problem 21P:
For the unity feedback system of Figure P6.3 with Gs=Ks+6ss+1s+4 determine the range of K to ensure...Problem 22P:
In the system of Figure P6.3, let Gs=Ksassb Find the range of K for closed-loop stability when:...Problem 23P:
For the unity feedback system of Figure P63 with Gs=Ks+3s+5s2s4 determine the range of K for...Problem 26P:
Find the range of K for stability for the unity feedback system of Figure P6.3 with [Section: 6.4]...Problem 28P:
find the range of K for stability. [Section: 6.41] 28. Find the range of gain. K, to ensure...Problem 29P:
Find the range of gain, K, to ensure stability in the unity feedback system of Figure P6.3 with...Problem 30P:
Using the Routh-Hurwitz criterion, find the value of K that will yield oscillations for the unity...Problem 31P:
Use the Routh-Hurwitz criterion to find the range of K for which the system of Figure P6.6 is...Problem 33P:
Given the unity feedback system of Figure P63 with Gs=Ks+4ss+1.2s+2 find the following: [Section:...Problem 35P:
For the system shown in Figure P6.8, find the value of gain, K, that will make the system oscillate....Problem 36P:
Given the unity feedback system of Figure P6.3 with [Section: 6.4] Gs=Kss+2s24s+8s+3 a. Find the...Problem 38P:
For the unity feedback system of Figure P6.3 with Gs=Ks+2s2+1s+4s1 find the range of K for which...Problem 39P:
For the unity feedback system of Figure P6.3 with [Section: 6.4] Gs=Ks+13s+4 a. Find the range of K...Problem 40P:
Given the unity feedback system of Figure P6.3 with [Section: 6.4] Gs=Ks+49s2+4s+5 a. Find the range...Problem 41P:
Using the Routh-Hurwitz criterion and the unity feedback system of Figure P6.3 with [Section: 6.4]...Problem 44P:
The closed-loop transfer function of a system is Ts=s2+K1s+K2s4+K1s3+K2s2+5s+1 Determine the range...Problem 47P:
An interval polynomial is of the form Ps=a0+a1s+a2s2+a3s3+a4s4+a5s5+... with its coefficients...Problem 48P:
A linearized model of a torque-controlled crane hoisting a load with a fixed rope length is...Problem 49P:
The read/write head assembly arm of a computer hard disk drive (HDD) can be modeled as a rigid...Problem 50P:
A system is represented in state space as x=013224143x+010uy=110x Determine how many eigenvalues are...Problem 52P:
State Space SS 52. The following system in state space represents the forward path of a unity...Problem 56P:
A model for an airplane’s pitch loop is shown in Figure P6.12. Find the range of gain, K, that will...Problem 62P:
Look-ahead information can be used to automatically steer a bicycle in a closed-loop configuration....Problem 64P:
It has been shown (Pounds, 2011) that an unloaded UAV helicopter is closed-loop stable and will have...Problem 66P:
The system shown in Figure P6.16 has G1s=1/ss+2s+4 . Find the following: a. The value of K2for which...Browse All Chapters of This Textbook
Chapter 1 - IntroductionChapter 2 - Modeling In The Frequency DomainChapter 3 - Modeling In The Time DomainChapter 4 - Time ResponseChapter 5 - Reduction Of Multiple SubsystemsChapter 6 - StabilityChapter 7 - Steady-state ErrorsChapter 8 - Root Locus TechniquesChapter 9 - Design Via Root LocusChapter 10 - Frequency Response Techniques
Sample Solutions for this Textbook
We offer sample solutions for CONTROL SYSTEMS ENGINEERING homework problems. See examples below:
Feedback plays an important in control system. Feedback is defined as some part of the output or the...Introduction: A mathematical model is defined as a model which describes the system with the help of...To analyse the system, a mathematical model is needed. A mathematical model is defined as a model...Introduction: First order system are those systems whose input-output equation is a first order...Introduction: Linear time invariant system (LTI system) represents a class of systems which are...The complete response of a system consists of mainly two parts: Natural response Forced response...Steady state error: It is defined as the difference between the input and the output of a system....Root locus is a plot of system’s closed loop poles which is defined in terms of gain. From the root...In the gain adjustment technique, we adjust the value of gain to get the improved transient...
Root locus represents the path of closed loop poles of given transfer function in s-plane as the...For a system, the total response of the system is the sum of the steady state response and transient...The major drawback in frequency domain designing method using root locus technique is that even...Control system has changed the way various industries were operating. It gives a precise controlling...
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