Root Locus Sketching: Re-arrange & Sketch for Parameter "a

In summary, the task is to re-arrange the open-loop transfer function and sketch the root locus for the system as the parameter 'a' varies from 0 to infinity. This can be done by finding the points where G(s)H(s) = -1 and manipulating the equation to get it in the traditional root locus form. This allows for the graphical analysis of the system's behavior as 'a' changes. The key to the root locus method is to find points in the complex plane where the sum of the angles on the numerator differs by 180 degrees (+360n) from the sum of angles on the denominator.
  • #1
wh88
9
0

Homework Statement



Re-arrange the open-loop transfer function and sketch the root locus for the system for variation of the parameter 'a' from 0 to infinity.

Homework Equations



G(s)H(s) = 10(s+a) / [s(s+1)(s+8)]

The Attempt at a Solution



my problem is that i don't know how to re-arrange the transfer function into the familiar form of KF(s). any help would be appreciated. Thanks!
 
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  • #2
Hi wh88. Can you tell me what must be the angle (and magnitude) of G(s)H(s) for the point "s" to be a pole of the closed loop TF?
 
  • #3
sorry i made a mistake in the opening post. it should be 'variation of the parameter a'. i missed out the 'a'.

to uart, i believe its -180 degs and magnitude 1
 
  • #4
wh88 said:
sorry i made a mistake in the opening post. it should be 'variation of the parameter a'. i missed out the 'a'.
That's ok, I guessed that :smile:

i believe its -180 degs and magnitude 1
Yep that's correct (180 degrees + any multiple of 360). The key to the root locus method is to find points in the complex plane where the sum of the angles on the numerator differs by 180 degrees (+360n) from the sum of angles on the denominator.

Start by plotting all the poles and zeros (of GH) on the complex plane and recognize that the angle that each pole (or zero) contributes to GH is equal to the angle of the vector drawn from the pole (or zero) to the test point "s". It's definitely a process that requires some practice before you become proficient.
 
  • #5
uart said:
That's ok, I guessed that :smile:


Yep that's correct (180 degrees + any multiple of 360). The key to the root locus method is to find points in the complex plane where the sum of the angles on the numerator differs by 180 degrees (+360n) from the sum of angles on the denominator.

Start by plotting all the poles and zeros (of GH) on the complex plane and recognize that the angle that each pole (or zero) contributes to GH is equal to the angle of the vector drawn from the pole (or zero) to the test point "s". It's definitely a process that requires some practice before you become proficient.

Thanks for your help, uart. My understanding is that before plotting the poles and zeros on the complex plane, we have to get the open loop TF arranged in the form KF(s) if we want to find out how variation of K from 0 to infinity affects the system.
So in this case, won't we have to re-arrange the TF to the form aF(s)?
 
  • #6
Hi wh88,

while uart has very kindly answered your question if you are doing a course in linear control you MUST (along with anyone else interested in this topic) look at the series of lectures by prof Madan Gopal on utube. I think root locus starts around lec 33.

Likely you will find these vids of more use than any text or lecture you might otherwise sit in on. Definitely worth you time. extremely well presented!
 
  • #7
wh88 said:
Thanks for your help, uart. My understanding is that before plotting the poles and zeros on the complex plane, we have to get the open loop TF arranged in the form KF(s) if we want to find out how variation of K from 0 to infinity affects the system.
So in this case, won't we have to re-arrange the TF to the form aF(s)?

Ok you're right, this case is quite different to a traditional root locus question where the parameter under variation is the loop gain. It's been a long while since I've had to do root locus so I'm pretty rusty, but I think that in the traditional case that every point in the complex plane that satisfies the angle condition automatically satisfies magnitude condition for some value of of loop gain. In this case however, where the parameter under variation is the position of a zero, then it's definitely not true that magnitude condition is automatically satisfied, so this seems like a much harder problem (compared to the standard type root locus problem).
 
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  • #8
wh88, is there any further context to this problem. Do you know if you're meant to try and solve it numerically or are you pretty sure that you're meant to be solving it graphically using the angle and magnitude conditions of root locus?
 
  • #9
uart said:
wh88, is there any further context to this problem. Do you know if you're meant to try and solve it numerically or are you pretty sure that you're meant to be solving it graphically using the angle and magnitude conditions of root locus?

uart, the question asks us to re-arrange the open loop transfer function and sketch the root locus for the system as a varies from 0 to infinty. I doubt numerical methods are required. Its the re-arrangement that's troubling me.
 
  • #10
wh88 said:
uart, the question asks us to re-arrange the open loop transfer function and sketch the root locus for the system as a varies from 0 to infinty. I doubt numerical methods are required. Its the re-arrangement that's troubling me.

Ok I can see what they want you to do now.

You have to find where G(s) H(s) = -1. So split it across the numerator as :

[tex] \frac{10s +10a}{s (s+1) (s+8) } = \frac{10s}{s (s+1) (s+8) } + \frac{10a}{s (s+1) (s+8) } [/tex]

Using the above you can rearrange GH=-1 to :

[tex]\frac{10a}{s (s+1) (s+8) } =- \left(1 + \frac{10s}{s (s+1) (s+8) } \right) [/tex]

Now put the RHS to a common denominator and factorize the resulting numerator (it factorizes pretty easily). Finally mult/divide both sides in the obvious way so as to re-establish "-1" on the RHS.

You end up with an equation in the traditional root locus form, where the variable is proportional to the loop gain.
 
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  • #11
uart said:
Ok I can see what they want you to do now.

You have to find where G(s) H(s) = -1. So split it across the numerator as :

[tex] \frac{10s +10a}{s (s+1) (s+8) } = \frac{10s}{s (s+1) (s+8) } + \frac{10a}{s (s+1) (s+8) } [/tex]

Using the above you can rearrange GH=-1 to :

[tex]\frac{10a}{s (s+1) (s+8) } =- \left(1 + \frac{10s}{s (s+1) (s+8) } \right) [/tex]

Now put the RHS to a common denominator and factorize the resulting numerator (it factorizes pretty easily). Finally mult/divide both sides in the obvious way so as to re-establish "-1" on the RHS.

You end up with an equation in the traditional root locus form, where the variable is proportional to the loop gain.

i finally got it. Thank you very much uart!
 

Related to Root Locus Sketching: Re-arrange & Sketch for Parameter "a

1. What is root locus sketching?

Root locus sketching is a graphical method used in control systems engineering to analyze the behavior of a closed-loop system as a parameter, typically denoted as "a", is varied. It involves plotting the roots of the characteristic equation of the system on a complex plane to determine the stability and performance of the system for different values of the parameter.

2. How is the parameter "a" re-arranged in root locus sketching?

In root locus sketching, the parameter "a" is re-arranged as a function of the gain, K, and the complex variable, s. This allows the root locus plot to be simplified and the effects of changing the parameter on the system's stability and performance to be easily observed.

3. What are the steps involved in sketching the root locus for a given system?

The steps for sketching the root locus for a given system are as follows:

  • 1. Determine the open-loop transfer function of the system.
  • 2. Determine the poles and zeros of the transfer function.
  • 3. Construct the root locus plot by varying the parameter "a" and plotting the roots of the characteristic equation on the complex plane.
  • 4. Determine the location of the branches of the root locus and their behavior as the parameter "a" is varied.
  • 5. Analyze the stability and performance of the system for different values of the parameter "a".

4. How does the root locus plot indicate the stability of a closed-loop system?

The root locus plot provides information about the stability of a closed-loop system by showing the location of the closed-loop poles for different values of the parameter "a". The system is stable if all of the poles are located in the left half of the complex plane. If any poles are located in the right half of the complex plane, the system is unstable and will exhibit oscillatory behavior.

5. What are the advantages of using root locus sketching in control systems analysis?

Root locus sketching has several advantages, including:

  • 1. It provides a graphical representation of the behavior of a closed-loop system, making it easier to visualize and analyze.
  • 2. It allows for the effects of changing a single parameter to be easily observed, making it a useful tool for controller design and tuning.
  • 3. It can be used to determine the stability and performance of a system without the need for complex mathematical calculations.

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