Video

i have a doubt, can we connect AC load instead of grid in your testcase or that LCL filter can cause inductive effect on load?

Thank You. Great video.

Really good explanation.. Thank you so much

So sad😢😢please help me

Great video, I am designing a grid following inverter. for that i want to design the PLL considering 5% of 3rd harmonics at 150Hz and 5% of negative sequence. But i don't know how i can play with my PLL to make it such. I have used SRF PLL which controls the current.

Tricky part of PWM output filter design is the dampening required when loads are switched off/on and when load has high crest factor with pulsing high current peaks. Sets PWM filter ringing.

Hello sir , it is possible if you share me your email to ask you few questions regarding your slides ?

wow, it is a really appreciable gesture of your kindness.wonderful work ,thanks a lot

@ 21:38, the transfer function Iinv/Vinv={1/(L1+L2)}* 1/S. = Kp/S. But next you design PI controller where transfer changed entirely because ouput is now Vinv = C*(Iref-I). It seems confusing to me. Kindly comment.. same is true for @ 6:11

SUPERB!!!!!!! Even reading an entire book did not give such a crystal-clear idea....

sir, can you provide Simulink files @frankydebruyne9842

sir, can you provide Simulink files

your thoughts is very clear！ I like that~

Hi Sir, In case of Output Disturbance, How can we change the matrix [A, BC_di; 0, A_di] at 8:06

hi sir this is wonderfull please how i can mail you sir please

How come this channel has only 2.2k subscribers?! This is amazing material. Thank you sr.

I wonder could we get access to the slides?

Wow, method 3 actually worked wonders for me. thanks.

I think equation for ippmaxL2 (37:43) is wrong the modulus is : 1/|1 - L*C*Wsw^2| 😁😁

Hello Dr. Franky De Bruyne. Thank you very much for the good tutorials you put on your channel I enjoy watching these educational videos. Is it possible to model and control a tilt-rotor grazer (QTR UAV or TTR UAV)?

Hello Dr. Franky De Bruyne. Thank you very much for the good tutorials you put on your channel I enjoy watching these educational videos. Is it possible to model and control a tilt-rotor grazer (QTR UAV or TTR UAV)?

Absolute master piece , if you can do a similar video for quadcopter but with Lagrangian Mechanics would be great.

❤

Nice explanation enjoing this and hoping to become a PLC tech by the end of 2025, Iam preparing myself

What bibliography do you use?

very well explained.

Sir, I have a question, in the simulink simulation from video 1:07:00 onwards, during the simulation using the "Discrete Filter" module, the expression of the filter is supposed to be in terms of z^-1 as the discretization factor, but we use z as the factor throughout the whole derivation, and the coefficients derived in the video are directly filled into the "Discrete" module, why doesn't it generate an error? Why doesn't it generate an error?

Thanks for sharing, I have a question, at 47:40, why delat_b = 0; isn't it 1?

I enjoyed this.

une super bonne idée, les quizz

Very powerful explanation. Please i which to model the grid tie inverter in state space. Can you help me with a video link for that. Thank you

Thanks so much. It really helps a lot.

What a class!

Can you give link to the notebook please?

Hello, what a great series.. thank you professor for sharing this with us. I have a question, how can I avoid the initial transient that can be observed at the start of each graph at 7:00 ? If I'm not mistaken that transient arises only because of the big difference between the reference Vdc and the real Vdc, am I correct? Is this a limitation of the IMC tuning method? Are real PV systems affected by this kind of problem or is there a solution to this? Thank you again Francesco

it is necessary to know the real matrices A B and C ?

amazing explanation much better than paid courses thank you

Thank you sir De Bruyne, Always talking to you about "observer polynomial " and that it must be changed to have the robustness, but it is not very clear, is the purpose of this polynom is to recalibrate the model with the real process to eliminate errors of modeling, or does it have to be adjusted to change the disturbance rejection dynamics ?, can you put a video to explain the interest of this plynome? please Thanks in advance

Many thanks. one question: if we want to connect the inverter to a 4 wire grid side, is it necessary to have a star/delta transformer with star grounded to get neutral point? can we use DC bus midpoint as neutral instead of transformer?

Why is the Harris index not exactly equal to 1 for the MV controller? Looking at the final frame of the video, it seems it is estimating some nonzero impulse response coefficients even after the delay. Is this due to the ARMA estimate of the MV closed-loop being based on a finite dataset?

Incredibly useful and informative. The only question I have is the direction of rotation of the yaw. What forces are acting on the rotors to cause it to rotate clockwise with w1 and w3 rotating clockwise? Is it not the pushing force at the outer tip of each of the propellors, acting opposite to the rotation direction- IE, wouldn’t the system rotate counter clockwise if the propeller pair was rotating at a higher speed clockwise?

Very informative and well explained. Hats off to you!!!

The best explanation I could find. Thank you.

Could you please make video for h infinity state observer?

Sir, your lectures are very interesting. Where I can get access for further information about your lectures

Very well explained Franky, thanks a lot!

thank you for this Clarification

Thank you for posting these video lectures. It has been really helpful for me to review the contents of this course. I would love to get access to the slides. Can you help with that sir?

I used this tuning parameters and it worked very well for my PLL. Can you please provide the sources for this IMC tuning method?? That would be great. Thank you very much

thank you