Added: 10 months ago
From: TheScienceguy3000
Views: 11,724
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  • I am slightly confused about why you need u(t) * B here? what what is a(t) ? ( i.e. your value for u(t) ) - since you cannot apply a force the bird - shouldn't acceleration be part of the state?

  • you have a radical imagination :D

  • Hello internet! :) See channel bulletin for links to code!

  • At time 9:30

    how come Ex is a 2x2 matrix and you are adding this to 2x1 columns in top equation?

  • great tutorial, thanks! Now there is something I don't get. You say that cov(P,V)=std(P)*str(V). From looking at the definitions of cov and std, I don't understand how this can betrue. Are you assuming sometehing we don't know? thanks again, really nicely done

  • you make elec systems intracractive keep on

  • you say "matrices" when you mean to say "matrix" and it's sort of confusing at times

  • Thank you it was very informative

  • Hi Scienceguy :D

    Thanks a lot for the informatinve video. I was wondering since the ninja is using the kalman filter algorithm, how come he has access to the acceleraation of the quail?

    Also, pls email me the code @ zhang.feng16@yahoo.com

    I must say you did you great job man. You simply rock :D

    Zhang

  • very pedagogical lecture set, thanks alot i really like this way of teaching,

    you may will be a great proffesor in future, good luck.

    kindly send me the matlab code:

    quantum_track2001@yahoo.com

    thanx.

  • Great lecture, but isn't there a small error in the measurement position prediction matrix? At time 07:40 you add P at t-1 and V at t-1 into the Xbar at t matrix, shouldn't these be P at t and V at t instead?

  • @BluelightUAV  ack! yes..you are correct.. wish there was a way to send a cookie online :)... thx for noticing! it's the predicted measurement..so it's the prediction at time t...not a prediction about the past...lol..we already know the past :) thx again

  • @TheScienceguy3000

    Instead of a quail, I have a gyro on a plane. The gyro is measuring angular rate change about the fuselage - if a wing goes up the gyro will measure this, and my motor command, will move it back. Where you have 2 equations (quail position and vel) I propose to have only one describing the angular rate (AR) of my wing as: AR (at t) = AR (at t-1) - Acceleration (at t) * t. My acceleration is that of the angular rate (ie its change caused by my control signal). Reasonable?

  • @TheScienceguy3000 Can you please me the code at zhang.feng16@yahoo.com I love your explanantion and really want to understand this . please help! I will really appreciate it. Now that you have explained the concept so well, pleaese please help!

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  • thank u sooooo much , the way u explained is "AWESOME " totally out of the box .

    thank you for this wonderful contribution of yours for students like us.

  • @qasmii sure thing, just message me your email (probably don't wanna put it here, unless your love spam :)

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  • at the end the link to part 3 says "Video removed by user, sorry about that" but if you pick part 3from the list on the right side it works.

    I had trouble reading the 't' and 'z' subscript and what was 'C' ?

  • @iBradleyAllen

    thanks! i fixed it, and, yea, I need a better camera, and a better hand :P. C is a coefficient, check out the third vid too see it all again, should make it clearer, else, just shoot me a message. thx!

  • He's gonna use the kalman filter to track the quail XD

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