Root Locus Technique | Solved Problem-2 | Control System
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- Опубликовано: 29 мар 2024
- Root Locus Technique | Solved Problem-2 | Control System
In control theory and stability theory, root locus analysis is a graphical method for examining how the roots of a system change with variation of a certain system parameter, commonly a gain within a feedback system. This is a technique used as a stability criterion in the field of classical control theory developed by Walter R. Evans which can determine stability of the system. The root locus plots the poles of the closed loop transfer function in the complex s-plane as a function of a gain parameter (see pole-zero plot).
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I mostly dont understand what you are saying but just looking at the solution I can understand what is going on with this root locus thing. Thats impressive actaully lol :)
Same here
Nice 💯❤
Saving me right now
You've explained in easy and clear way. If I watched this video just a week ago, I should've scored 100/100.✌ I lost 10 marks
Nice explanation of each and every point 👍
bhut badiya sir thanks
Brilliant explaination sir ...😊
Great lecture as always samll suggestion please stand on side before jumping to next page so we can take screenshots .
Noted!
Thank you for suggestion😊
Very thank you sir
Thanks sir❤
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Bhaiya transfer function nikalana Shikha dijiye please
💯
Thanks a lot sir. You made it so easy......and definitely deserve more subsribers....
Thank you Naman!
sir or bhi lecture video dal di jiye bahut badhiya tarika se aap samjhate hai
thank you...i will upload soon..stay connected
@@triple.e.sudhanshu sir 24 ko exam hai plz thoda jaldi upload kariyega plz
@@kumkum0902 thek hai...
angle of departure ϕd
is
ϕd=180−ϕ
15:56
The formula for the angle of arrival ϕa
is
ϕa=180+ϕ
👍
Hr kisi video m angle of departure (180 - fi) h or angle of arrival (180 +fi)... LekinApne dono ka formula( 180 - fi) likha h ...kyu😅???
If you write;
Angle of departure = 180 - @
then you have to calculate, Fi = (Summation of angles due to poles - Summation of angles due to zeros)
If you write;
Angle of departure = 180 + @
then you have to calculate, Fi = (Summation of angles due to zeros - Summation of angles due to poles).
It doesn't make any changes in the result.
Both are the same dear!
& In this question, I didn't calculate the angle of arrival.
Bode plot
wait...it will be uploaded soon...i am out of station